# NewSpace Market — MRD (machine-readable datasheets), full dump # Typed spacecraft component specifications extracted from vendor datasheets. # 2486 products, 19011 values, generated 2026-08-30. # Units are canonical (converted by code). A property that is absent is NOT published # by the vendor — never assume a value. "@" marks the measurement condition. # License: CC BY 4.0, attribution "NewSpace Market". # Live API and MCP connector: https://newspacemarket.com/mrd-connect/ ## RW222 — AAC Clyde Space [reaction-wheels] https://newspacemarket.com/products/aac-rw222/ Angular momentum storage: 0.003 N·m·s Angular momentum storage: 0.006 N·m·s @ (variant 2) Max torque: 2 mN·m Data interface: I²C Envelope (L×W×H): 25 x 25 x 15mm Wheel speed: 10000-15000 @ To be tested Envelope (L×W×H): 25 x 25 x15 @ Outer dimensions Operating temperature: -20-60 Supply voltage: 3.25-3.5 @ Supply voltage Mass: 100 g @ as published, mode unspecified Power consumption: 1 W @ as published, mode unspecified ## VRW-B-02 Reaction Wheel — VECTRONIC Aerospace GmbH [reaction-wheels] https://newspacemarket.com/products/vectronic-vrw-b-02/ Envelope (L×W×H): 70 mm x 70 mm x 48 mm Mass: 1000 g Angular momentum storage: 0.2 N·m·s @ nominal Power consumption: 1.1 W (max) @ steady state, no speed Power consumption: 4.5 W (max) @ steady state, max. speed Power consumption: 45 W (max) @ max. speed, max. torque Static imbalance: 1 (max) Dynamic imbalance: 80 (max) Data interface: RS-422 Data interface: RS-485 @ (variant 2) Data interface: CAN @ (variant 3) Flight heritage: 100 years of in-orbit flight experience Wheel speed: -6000-6000 (max) Max torque: 20 mN·m (max) Design lifetime: 5.1 (nominal) @ in-orbit (converted from hours) Radiation tolerance (TID): 20 krad @ as published, mode unspecified Supply voltage: 9-36 V @ as published, mode unspecified Operating temperature: -20-70 °C @ as published, mode unspecified Design lifetime: 5.1 @ nominal in-orbit (converted from hours) Design lifetime: 5.1 years (from hour @ nominal in-orbit ## 1 Nms Microsatellite Reaction Wheel — Sinclair Interplanetary (Rocket Lab) [reaction-wheels] https://newspacemarket.com/products/sinclair-1-nms-microsatellite-reaction-wheel/ Angular momentum storage: 1 N·m·s @ Nominal Max torque: 50 mN·m @ at 1 Nms (at 28 V supply) Data interface: RS-485 Data interface: CAN @ (variant 2) Envelope (L×W×H): 150 mm x 140 mm x 42 mm Mass: 970 g Supply voltage: 24 (min) @ Nominal Supply voltage: 34 (max) @ Nominal Supply voltage: 50 (max) Power consumption: 46.7 W @ @ 1.0 Nms, +40 mNm Power consumption: 15.1 W @ @ 1.0 Nms, steady state Power consumption: 2.4 W @ @ 0.2 Nms, steady state Power consumption: -29.1 W @ @ 1.0 Nms, -100 mNm regenerative braking Operating temperature: -40 °C (min) Operating temperature: 70 °C (max) Radiation tolerance (TID): 20 krad Bearing type: ball Flight heritage: 52 Units on-orbit. First launch June 2016. Angular momentum storage: 1 N·m·s (nominal) Supply voltage: 24-34 (nominal) Supply voltage: 50 Operating temperature: -40-70 @ operating Random vibration: 14 Radiation tolerance (TID): 20 krad @ dose Data interface: RS-485 @ Two RS-485 plus one CAN Data interface: CAN @ Two RS-485 plus one CAN (variant 2) ## Microsat Reaction Wheel — SSBV Aerospace & Technology [reaction-wheels] https://newspacemarket.com/products/ssbv-microsat-reaction-wheel/ Max torque: 20 mN·m (max) Angular momentum storage: 0.65 N·m·s (max) Wheel speed: -9000 (min) Wheel speed: 9000 (max) Mass: 1550 g Envelope (L×W×H): 102 x 102 x 105 mm Static imbalance: 5 (max) Operating temperature: -30 °C (min) Operating temperature: 60 °C (max) Supply voltage: 28 (nominal) @ unregulated Data interface: RS-422 Flight heritage: SUNSAT and TUBSAT Satellites, Orbcomm 2nd Generation constellation Wheel speed: -9000-9000 Operating temperature: -30-60 Supply voltage: 28 @ unregulated ## NanoTorque GSW-600 Reaction Wheels — GomSpace [reaction-wheels] https://newspacemarket.com/products/gomspace-nanotorque-gsw-600-reaction-wheels/ Design lifetime: 3 years @ design, in-orbit operations Design lifetime: 3 years @ design Max torque: 2 mN·m Angular momentum storage: 0.019 N·m·s @ storage Bearing type: hybrid Data interface: SPI Data interface: I2C @ (variant 2) Connector: Molex PicoBlade right angle, 053261-1371 Operating temperature: -40 °C (min) Operating temperature: 80 °C (max) Survival temperature: -40 °C (min) Survival temperature: 85 °C (max) Max torque: -1.5 mN·m (min) @ Continuous Max torque: 1.5 mN·m (max) @ Continuous Max torque: -0.015 mN·m (min) @ Minimum torque, Torque control Max torque: 0.015 mN·m (max) @ Minimum torque, Torque control Wheel speed: -6000 (min) @ Maximum Wheel speed: 6000 (max) @ Maximum Wheel speed: -3500 (min) @ At max torque Wheel speed: 3500 (max) @ At max torque Angular momentum storage: 0.019 N·m·s @ At max speed Supply voltage: 4.9 (min) Supply voltage: 5 (nominal) Supply voltage: 5.1 (max) Mass: 180 g @ One Wheel Envelope (L×W×H): 44.0 x 44.0 x 27.0 @ One Wheel Max torque: 0.015 mN·m (min) @ Torque control Wheel speed: -6000-6000 (max) Wheel speed: -3500-3500 @ At max torque Angular momentum storage: 0.019 N·m·s (typical) @ At max speed Supply voltage: 4.9-5.1 Data interface: 100-130 @ SPI speed Data interface: 100-400 @ I2C speed Connector: Molex PicoBlade right angle, 053261-1371 @ Main connector H2 Design lifetime: 3 years @ in-orbit operations Flight heritage: Flight-proven ## Zyra Reaction Wheel — arcsec [reaction-wheels] https://newspacemarket.com/products/zyra-reaction-wheel/ Angular momentum storage: 0.0275 N·m·s Max torque: 1.5 mN·m Envelope (L×W×H): 40x40x24.5 mm Static imbalance: G0.4 Balancing grade (Static and dynamic) Dynamic imbalance: G0.4 Balancing grade (Static and dynamic) Data interface: RS-485 Supply voltage: 5 (min) Supply voltage: 12 (max) Mass: 165 g Static imbalance: 0.4 @ Balancing grade Dynamic imbalance: 0.4 @ Balancing grade Supply voltage: 5-12 ## Reaction Wheels — Blue Canyon Technologies [reaction-wheels] https://newspacemarket.com/products/rwp100-reaction-wheel/ Angular momentum storage: 1 N·m·s (max) Max torque: 60 mN·m (max) Static imbalance: 3 (max) @ STANDARD Dynamic imbalance: 90 (max) @ STANDARD Static imbalance: 1 (max) @ FINE BALANCE Dynamic imbalance: 10 (max) @ FINE BALANCE Mass: 1100 g Envelope (L×W×H): 112 x 112 x 55 mm Supply voltage: 22-34 Power consumption: 14 (max) @ AT MAX MOMENTUM Power consumption: 100 @ PEAK POWER Power consumption: 4 @ AT ZERO MOMENTUM Power consumption: 42 @ PEAK REGENERATED POWER Connector: 21 pin: M83513/13-C01NW Data interface: RS-422 Operating temperature: -20-60 Survival temperature: -30-70 Flight heritage: longest unit on-orbit 3.3 years ## W18 Reaction Wheel — Bradford Space [reaction-wheels] https://newspacemarket.com/products/bradford-w18-reaction-wheel/ Max torque: 265 mN·m (max) @ gross torque Power consumption: 168 W @ as published, mode unspecified Angular momentum storage: 18 N·m·s Wheel speed: 4000 (max) Static imbalance: 0.5 Dynamic imbalance: 5 Envelope (L×W×H): Ø295×125 Mass: 5200 g Power consumption: 168 W @ Peak Power Consumption at max. torque and speed Power consumption: 29 W @ Steady State Consumption at max. constant speed Power consumption: 7.6 W @ Quiescent Power Consumption Supply voltage: 28 (nominal) Supply voltage: 50 (nominal) @ (variant 2) Data interface: MIL-STD-1553 Data interface: other @ analogue Operating temperature: -15 °C (min) @ RWA Operating temperature: 60 °C (max) @ RWA Flight heritage: SOHO, RadarSat, Seastar, Olympus, INTEGRAL, XMM, Rosetta, Aeolus, BepiColombo ## Reaction Wheel — Pyxis Space [reaction-wheels] https://newspacemarket.com/products/pyxis-reaction-wheel/ Wheel speed: 5000-10000 Angular momentum storage: 0.005 N·m·s @ nominal Max torque: 2 mN·m (max) Data interface: CAN @ 2.0B Supply voltage: 4.5-5.5 Power consumption: 2.5 W (max) Mass: 100 g Envelope (L×W×H): 32 x 32 x 32 mm3 Operating temperature: -40-80 °C Radiation tolerance (TID): 10 krad Bearing type: other @ vacuum bearings Flight heritage: since 2024 Data interface: I2C @ option Data interface: UART @ option (variant 2) Wheel speed: 5000 (nominal) Wheel speed: 10000 (max) Angular momentum storage: 0.005 N·m·s (nominal) Data interface: CAN Bearing type: vacuum ## Reaction Wheel RW1 — EXA (Astro-und Feinwerktechnik) [reaction-wheels] https://newspacemarket.com/products/rw1-reaction-wheel-2/ Angular momentum storage: 0.0006 N·m·s @ @8000rpm Wheel speed: 8000 @ Nominal Wheel speed: 16380 @ Maximum Max torque: 0.023 mN·m @ Nominal Mass: 24 g (max) Envelope (L×W×H): 21mm*21mm*12 mm Operating temperature: -20 °C @ min Operating temperature: 50 °C @ max Design lifetime: 1 years Wheel speed: 8000-16380 Max torque: 23 mN·m (nominal) Operating temperature: -20-50 Design lifetime: 1 @ Hardware Power consumption: 0.25 W @ as published, mode unspecified Supply voltage: 5-5 V @ as published, mode unspecified ## RSI 4-75/60 Momentum and Reaction Wheel — Collins Aerospace [reaction-wheels] https://newspacemarket.com/products/collins-rsi-4-75-60-momentum-reaction-wheel/ Design lifetime: 15 years @ >, in orbit Wheel speed: -6000-6000 @ Operational Envelope (L×W×H): 222 mm x 85 mm @ Diameter x Height Supply voltage: 24-51 Operating temperature: -10-55 @ mineral oil Operating temperature: -25-75 @ synthetic oil Operating temperature: -5-50 @ mineral oil (variant 2) Operating temperature: -20-70 @ synthetic oil (variant 2) Survival temperature: -20-60 @ mineral oil Survival temperature: -40-75 @ synthetic oil Flight heritage: Part of TELDIX wheel family with 40+ years heritage, 7,300+ cumulative in-orbit years Angular momentum storage: 4 N·m·s @ at nominal speed Max torque: 75 mN·m @ at nominal speed Mass: 3700 g (max) Power consumption: 20 W (max) @ Steady state at nominal speed Power consumption: 90 W (max) @ Maximum torque at nominal speed Design lifetime: 15 years @ in orbit ## CubeSat Reaction Wheels Module SXC-FW4-02 — SPUTNIX [reaction-wheels] https://newspacemarket.com/products/sputnix-sxc-fw4-02-reaction-wheels/ Max torque: 8.8 mN·m @ as published, mode unspecified Mass: 580 g @ as published, mode unspecified Supply voltage: 5-12 V @ as published, mode unspecified Envelope (L×W×H): 97.5 × 97.5 × 80 mm ## Reaction Wheels Block — Glavkosmos [reaction-wheels] https://newspacemarket.com/products/reaction-wheels-block/ Mass: 450 g @ as published, mode unspecified Power consumption: 3 W @ as published, mode unspecified Design lifetime: 1 years @ as published, mode unspecified Lead time: 5 months @ as published, mode unspecified Supply voltage: 4-15 V @ as published, mode unspecified Envelope (L×W×H): 97 × 97 × 63 mm ## RW400 — AAC Clyde Space [reaction-wheels] https://newspacemarket.com/products/aac-rw400/ Max torque: 8 mN·m @ as published, mode unspecified Radiation tolerance (TID): 36 krad Wheel speed: 5000 Envelope (L×W×H): 50 x 50 x 27 mm Operating temperature: -40-60 °C Supply voltage: 3.3-5.1 Power consumption: 0.751 W Power consumption: 1 W @ (variant 2) ## VRW Reaction Wheels — VECTRONIC Aerospace GmbH [reaction-wheels] https://newspacemarket.com/products/vectronic-vrw-a-1/ Angular momentum storage: 8 N·m·s @ as published, mode unspecified Max torque: 50 mN·m @ as published, mode unspecified Mass: 1000 g @ as published, mode unspecified Power consumption: 1.1 W @ as published, mode unspecified Radiation tolerance (TID): 20 krad @ as published, mode unspecified Supply voltage: 9-36 V @ as published, mode unspecified Operating temperature: -20-70 °C @ as published, mode unspecified Envelope (L×W×H): 70 mm x 70 mm x 48 mm Connector: MDM-9 / MDM-25 Wheel speed: 0.1 Envelope (L×W×H): 96 mm x 96 mm x 52 mm @ (variant 2) Connector: MDM-25 @ (variant 2) Wheel speed: 0.1 @ (variant 2) Envelope (L×W×H): 140 mm x 140 mm x 60 mm @ (variant 3) Connector: MDM-25 @ (variant 3) Wheel speed: 0.1 @ (variant 3) Envelope (L×W×H): 180 mm x 180 mm x 60 mm @ (variant 4) Connector: MDM-25 @ (variant 4) ## RW40 — Comat [reaction-wheels] https://newspacemarket.com/products/comat-rw40/ Max torque: 4 mN·m @ as published, mode unspecified Mass: 230 g @ as published, mode unspecified Power consumption: 0.9 W @ as published, mode unspecified Operating temperature: -30-50 °C @ as published, mode unspecified Angular momentum storage: 0.04 N·m·s Design lifetime: 8 years Flight heritage: 100+ units on the Kinéis satellite constellation ## 1 Nms GEO Reaction Wheel — Sinclair Interplanetary (Rocket Lab) [reaction-wheels] https://newspacemarket.com/products/sinclair-1-nms-geo-reaction-wheel/ Angular momentum storage: 1 N·m·s @ as published, mode unspecified ## 30 mNms Nanosatellite Reaction Wheel — Sinclair Interplanetary (Rocket Lab) [reaction-wheels] https://newspacemarket.com/products/sinclair-30-mnms-nanosatellite-reaction-wheel/ Angular momentum storage: 0.03 N·m·s @ as published, mode unspecified Max torque: 2 mN·m @ as published, mode unspecified Radiation tolerance (TID): 20 krad Angular momentum storage: 0.03 N·m·s @ Nominal Angular momentum storage: 0.04 N·m·s @ Peak, at 5 V supply Max torque: 2 mN·m @ at 0.02 Nms Max torque: 0.5 mN·m @ at 0.04 Nms (at 5 V supply) Mass: 185 g Envelope (L×W×H): 50 mm x 50 mm x 40 mm Supply voltage: 3.4-6 @ Nominal Supply voltage: 8 @ maximum Power consumption: 1.8 W @ @ 0.02 Nms, +2 mNm Power consumption: 0.3 W @ @ 0.04 Nms, steady state Power consumption: 0.1 W @ @ 0.01 Nms, steady state Operating temperature: -40-70 °C Radiation tolerance (TID): 20 krad @ dose Bearing type: ball @ Diamond coated hybrid ball bearings Data interface: UART Data interface: I2C @ (variant 2) Data interface: other @ SMBus Flight heritage: 55 Units total on-orbit, on 20 satellites Flight heritage: First launch April 28, 2008, design essentially unchanged @ (variant 2) Flight heritage: Demonstrated 12 arc-sec RMS pointing on 7 kg satellite @ (variant 3) ## 400 mNms Microsatellite Reaction Wheel — Sinclair Interplanetary (Rocket Lab) [reaction-wheels] https://newspacemarket.com/products/sinclair-400-mnms-microsatellite-reaction-wheel/ Angular momentum storage: 0.4 N·m·s @ as published, mode unspecified Max torque: 100 mN·m @ as published, mode unspecified Radiation tolerance (TID): 60 krad @ Total Dose, with LDRS testing Angular momentum storage: 0.4 N·m·s @ heavy rotor Max torque: 100 mN·m @ at nominal momentum Mass: 770 g @ heavy rotor Envelope (L×W×H): 110 mm dia x 48 mm high Supply voltage: 24 (min) @ Nominal Supply voltage: 34 (max) @ Nominal Operating temperature: -40 °C (min) Operating temperature: 70 °C (max) Radiation tolerance (TID): 60 krad (min) @ Total Dose Flight heritage: Mechanical design from RW3-1.0, with 52 Units on-orbit. ## Reaction wheels module — SPUTNIX [reaction-wheels] https://newspacemarket.com/products/reaction-wheels-module/ Mass: 580 g @ as published, mode unspecified Power consumption: 0.8 W @ as published, mode unspecified Supply voltage: 5-12 V @ as published, mode unspecified Operating temperature: -30-50 °C @ as published, mode unspecified Envelope (L×W×H): 97.5 x 97.5 x 80 mm (±1 mm) Wheel speed: 10 (max) ## Reaction wheel — SPUTNIX [reaction-wheels] https://newspacemarket.com/products/reaction-wheel/ Max torque: 50 mN·m @ as published, mode unspecified Mass: 3200 g @ as published, mode unspecified Supply voltage: 22-34 V @ as published, mode unspecified Envelope (L×W×H): 160 x 160 x 80 (without fasteners) mm ## ASPINA Reaction Wheels for Small Space Satellites — ASPINA [reaction-wheels] https://newspacemarket.com/products/aspina-space-blower/ Angular momentum storage: 2 N·m·s @ family value (4 models in card), pairing across fields may not exist Max torque: 100 mN·m @ family value (3 models in card), pairing across fields may not exist Mass: 71 g @ as published, mode unspecified Power consumption: 0.6 W @ as published, mode unspecified Design lifetime: 5 years @ as published, mode unspecified Radiation tolerance (TID): 30 krad @ as published, mode unspecified Supply voltage: 9-12 V @ as published, mode unspecified TRL: 8 Flight heritage: 1st units launched: Jan 2025 Wheel speed: 6000 Envelope (L×W×H): 30 x 30 x 30 mm Random vibration: 14.1 TRL: 8 @ (variant 2) Flight heritage: 1st Launch: Middle of 2026 @ (variant 2) Wheel speed: 6000 @ (variant 2) Envelope (L×W×H): 100 x 100 x 58.5 mm @ (variant 2) Random vibration: 20 @ (variant 2) TRL: 8 @ (variant 3) Flight heritage: 1st Launch: Jun 2026 @ (variant 3) Wheel speed: 7000 @ (variant 3) Envelope (L×W×H): 138 x 138 x 50 mm @ (variant 3) Random vibration: 20.8 @ (variant 3) TRL: 8 @ (variant 4) Flight heritage: 1st Launch: Jun 2026 @ (variant 4) Wheel speed: 7000 @ (variant 4) Envelope (L×W×H): 138 x 138 x 68 mm @ (variant 4) ## Reaction Wheel — Space Inventor ApS [reaction-wheels] https://newspacemarket.com/products/reaction-wheel-2/ Design lifetime: 5 years @ as published, mode unspecified ## Reaction Wheel CW0017 — CubeSpace ADCS [reaction-wheels] https://newspacemarket.com/products/reaction-wheel-cw0017/ Lead time: 2.7616 months @ as published, mode unspecified ## Reaction Wheel CW2500 (0.25 Nms) — CubeSpace ADCS [reaction-wheels] https://newspacemarket.com/products/reaction-wheel-cw2500-0-25-nms/ Lead time: 2.7616 months @ as published, mode unspecified ## Reaction Wheel CW0057 — CubeSpace ADCS [reaction-wheels] https://newspacemarket.com/products/reaction-wheel-cw0057/ Lead time: 2.7616 months @ as published, mode unspecified ## Reaction Wheel CW0162 — CubeSpace ADCS [reaction-wheels] https://newspacemarket.com/products/reaction-wheel-cw0162/ Lead time: 2.7616 months @ as published, mode unspecified ## Reaction Wheel CW0500 — CubeSpace ADCS [reaction-wheels] https://newspacemarket.com/products/reaction-wheel-cw0500/ Lead time: 2.7616 months @ as published, mode unspecified ## Reaction Wheel CW1200 (0.12 Nms) — CubeSpace ADCS [reaction-wheels] https://newspacemarket.com/products/reaction-wheel-cw1200-0-12-nms/ Lead time: 2.7616 months @ as published, mode unspecified ## Reaction Wheel CW5000 (0.5 Nms) — CubeSpace ADCS [reaction-wheels] https://newspacemarket.com/products/reaction-wheel-cw5000-0-5-nms/ Lead time: 2.7616 months @ as published, mode unspecified ## Reaction Wheel CW10k (1 Nms) — CubeSpace ADCS [reaction-wheels] https://newspacemarket.com/products/reaction-wheel-cw10k-1-nms/ Lead time: 2.7616 months @ as published, mode unspecified ## Reaction Wheel (CW40K) (4Nms) — CubeSpace ADCS [reaction-wheels] https://newspacemarket.com/products/reaction-wheel-cw40k-4nms/ Lead time: 2.7616 months @ as published, mode unspecified ## Reaction wheel — ASPINA [reaction-wheels] https://newspacemarket.com/products/arw-3m-reaction-wheel/ Angular momentum storage: 2 N·m·s @ family value (4 models in card), pairing across fields may not exist Max torque: 100 mN·m @ family value (3 models in card), pairing across fields may not exist Mass: 71 g @ as published, mode unspecified Power consumption: 0.6 W @ as published, mode unspecified Design lifetime: 5 years @ as published, mode unspecified Radiation tolerance (TID): 30 krad @ as published, mode unspecified Supply voltage: 9-12 V @ as published, mode unspecified Operating temperature: -30-70 °C @ as published, mode unspecified TRL: 8 Flight heritage: 1st units launched: Jan 2025 Wheel speed: 6000 Envelope (L×W×H): 30 x 30 x 30 mm Random vibration: 14.1 TRL: 8 @ (variant 2) Flight heritage: 1st Launch: Middle of 2026 @ (variant 2) Wheel speed: 6000 @ (variant 2) Envelope (L×W×H): 100 x 100 x 58.5 mm @ (variant 2) Random vibration: 20 @ (variant 2) TRL: 8 @ (variant 3) Flight heritage: 1st Launch: Jun 2026 @ (variant 3) Wheel speed: 7000 @ (variant 3) Envelope (L×W×H): 138 x 138 x 50 mm @ (variant 3) Random vibration: 20.8 @ (variant 3) TRL: 8 @ (variant 4) Flight heritage: 1st Launch: Jun 2026 @ (variant 4) Wheel speed: 7000 @ (variant 4) Envelope (L×W×H): 138 x 138 x 68 mm @ (variant 4) ## Small Sat Reaction Wheels — Comat [reaction-wheels] https://newspacemarket.com/products/comat-reaction-wheel-60/ Mass: 270 g @ as published, mode unspecified Design lifetime: 10 years @ as published, mode unspecified Radiation tolerance (TID): 20 krad @ as published, mode unspecified Supply voltage: 14-28 V @ as published, mode unspecified Operating temperature: -30-60 °C @ as published, mode unspecified ## HR04, HC7 & HC9 Reaction Wheel Assemblies — Honeywell Aerospace [reaction-wheels] https://newspacemarket.com/products/honeywell-hc7-reaction-wheel-assembly/ Power consumption: 5 W @ as published, mode unspecified Operating temperature: -10-50 °C @ as published, mode unspecified ## W18E Reaction Wheel — Bradford Space [reaction-wheels] https://newspacemarket.com/products/bradford-w18e-reaction-wheel/ Angular momentum storage: 22 N·m·s Max torque: 265 mN·m (max) Static imbalance: 0.5 Dynamic imbalance: 5 Envelope (L×W×H): Ø295×125 Mass: 5650 g Flight heritage: SOHO, RadarSat, Seastar, Olympus, INTEGRAL, XMM, Rosetta, Aeolus, BepiColombo Angular momentum storage: 22 N·m·s @ as published, mode unspecified Max torque: 248 mN·m @ as published, mode unspecified Mass: 5560 g @ as published, mode unspecified Power consumption: 168 W @ as published, mode unspecified Wheel speed: 4000 Operating temperature: -15 °C ## W18ES Reaction Wheel — Bradford Space [reaction-wheels] https://newspacemarket.com/products/bradford-w18es-reaction-wheel/ Angular momentum storage: 25 N·m·s @ as published, mode unspecified Mass: 6020 g @ as published, mode unspecified Power consumption: 168 W @ as published, mode unspecified Operating temperature: -15 °C Angular momentum storage: 25 N·m·s Wheel speed: 4000 (max) @ Operational Static imbalance: 0.5 Dynamic imbalance: 5 Envelope (L×W×H): Ø295×125 @ RWA Mass: 6020 g @ RWA Envelope (L×W×H): 258×181×143 @ 2-channel WDE Mass: 4670 g @ 2-channel WDE Power consumption: 168 W @ Peak at max. torque and speed Power consumption: 29 W @ Steady State at max. constant speed Power consumption: 7.6 W @ Quiescent Supply voltage: 28 (nominal) Supply voltage: 50 (nominal) @ (variant 2) Data interface: MIL-STD-1553 Data interface: other @ analogue Flight heritage: SOHO, RadarSat, Seastar, Olympus, INTEGRAL, XMM, Rosetta, Aeolus, BepiColombo ## W45 Reaction Wheel — Bradford Space [reaction-wheels] https://newspacemarket.com/products/bradford-w45-reaction-wheel/ Angular momentum storage: 40 N·m·s Static imbalance: 0.5 Dynamic imbalance: 5 Envelope (L×W×H): Ø365×125 Mass: 6700 g Data interface: MIL-STD-1553 Data interface: other @ analogue Flight heritage: SOHO, RadarSat, Seastar, Olympus, INTEGRAL, XMM, Rosetta, Aeolus, BepiColombo Angular momentum storage: 40 N·m·s @ as published, mode unspecified Max torque: 265 mN·m @ as published, mode unspecified Mass: 6700 g @ as published, mode unspecified Power consumption: 168 W @ as published, mode unspecified Wheel speed: 4000 Supply voltage: 28 Operating temperature: -15 °C ## W45E Reaction Wheel — Bradford Space [reaction-wheels] https://newspacemarket.com/products/bradford-w45e-reaction-wheel/ Angular momentum storage: 45 N·m·s @ as published, mode unspecified Max torque: 248 mN·m @ as published, mode unspecified Mass: 7450 g @ as published, mode unspecified Power consumption: 168 W @ as published, mode unspecified Angular momentum storage: 45 N·m·s Max torque: 248 mN·m (max) Wheel speed: 4000 (max) @ Operational Static imbalance: 0.5 Dynamic imbalance: 5 Envelope (L×W×H): Ø365×125 @ RWA Mass: 7450 g @ RWA Power consumption: 168 W @ Peak Power Consumption at max. torque and speed Power consumption: 29 W @ Steady State Consumption at max. constant speed Power consumption: 7.6 W @ Quiescent Power Consumption Supply voltage: 28 (nominal) Supply voltage: 50 (nominal) @ (variant 2) Data interface: MIL-STD-1553 Data interface: other @ analogue Operating temperature: -15 °C (min) @ RWA Operating temperature: 60 °C (max) @ RWA Flight heritage: SOHO, RadarSat, Seastar, Olympus, INTEGRAL, XMM, Rosetta, Aeolus, BepiColombo ## CubeSat Reaction Wheels Control System (SatBus 4RW) — NanoAvionics [reaction-wheels] https://newspacemarket.com/products/nanoavionics-rw0-4rw0-reaction-wheels/ Mass: 137 g @ as published, mode unspecified Operating temperature: -40-85 °C @ as published, mode unspecified ## Microsatellite Reaction Wheel SX-SBOX-RWH-50-2.0-01 — SPUTNIX [reaction-wheels] https://newspacemarket.com/products/sputnix-sx-sbox-rwh-50-reaction-wheel/ Max torque: 50 mN·m @ as published, mode unspecified Mass: 3200 g @ as published, mode unspecified Supply voltage: 22-34 V @ as published, mode unspecified Envelope (L×W×H): 160 × 160 × 80 mm ## AAC Clyde Space RW210 Reaction Wheel — AAC Clyde Space [reaction-wheels] https://newspacemarket.com/products/aac-clyde-rw210-reaction-wheel/ Max torque: 0.1 mN·m @ as published, mode unspecified Mass: 21 g @ as published, mode unspecified Power consumption: 0.8 W @ as published, mode unspecified Radiation tolerance (TID): 36 krad @ as published, mode unspecified Supply voltage: 3.25-3.5 V @ as published, mode unspecified Operating temperature: -20-60 °C @ as published, mode unspecified Angular momentum storage: 0.0015 N·m·s Angular momentum storage: 0.003 N·m·s @ (variant 2) Angular momentum storage: 0.006 N·m·s @ (variant 3) Max torque: 0.1 mN·m (max) Wheel speed: 10000 (max) Wheel speed: 15000 (max) @ (variant 2) Mass: 21 g Mass: 32 g @ (variant 2) Mass: 48 g @ (variant 3) Envelope (L×W×H): 25 x 25 x 15mm Supply voltage: 3.25 (min) Supply voltage: 3.5 (max) Power consumption: 0.075 W (max) @ Idle Power consumption: 0.63 W (max) @ Nominal Power consumption: 0.8 W (max) @ Peak Operating temperature: -20 °C (min) Operating temperature: 60 °C (max) Radiation tolerance (TID): 36 krad Flight heritage: first flight in 2017 ## Reaction Wheel RW25 — EXA (Astro-und Feinwerktechnik) [reaction-wheels] https://newspacemarket.com/products/rw25-reaction-wheel/ Angular momentum storage: 0.03 N·m·s @ as published, mode unspecified Max torque: 2 mN·m @ as published, mode unspecified Mass: 200 g @ as published, mode unspecified Power consumption: 2.8 W @ as published, mode unspecified Supply voltage: 5-5 V @ as published, mode unspecified Design lifetime: 2 years Angular momentum storage: 0.03 N·m·s @ @5000rpm Wheel speed: 5000 (nominal) Wheel speed: 5500 (max) Max torque: 2 mN·m @ Nominal Mass: 200 g (max) Envelope (L×W×H): 50mm*50mm*25mm Operating temperature: -20 °C (min) Operating temperature: 50 °C (max) ## Reaction Wheel RW35 — EXA (Astro-und Feinwerktechnik) [reaction-wheels] https://newspacemarket.com/products/rw35-reaction-wheel/ Angular momentum storage: 0.1 N·m·s @ @5000rpm Wheel speed: 5000-5000 Max torque: 5 mN·m @ Nominal Mass: 500 g (max) Envelope (L×W×H): 102mm*102mm*58mm Operating temperature: -20-50 °C Design lifetime: 5 years @ Hardware Angular momentum storage: 0.1 N·m·s @ as published, mode unspecified Max torque: 5 mN·m @ as published, mode unspecified Mass: 500 g @ as published, mode unspecified Power consumption: 9 W @ as published, mode unspecified Design lifetime: 5 years @ as published, mode unspecified Radiation tolerance (TID): 2 krad @ as published, mode unspecified Supply voltage: 18-18 V @ as published, mode unspecified ## Reaction Wheel RW90 — EXA (Astro-und Feinwerktechnik) [reaction-wheels] https://newspacemarket.com/products/rw90-reaction-wheel/ Angular momentum storage: 0.35 N·m·s @ as published, mode unspecified Max torque: 15 mN·m @ as published, mode unspecified Power consumption: 1.8 W @ as published, mode unspecified Design lifetime: 7 years @ as published, mode unspecified Survival temperature: -40 °C Angular momentum storage: 0.35 N·m·s @ @7800rpm Wheel speed: 6000 (nominal) Wheel speed: 7800 (max) Max torque: 15 mN·m (nominal) Mass: 900 g (max) Envelope (L×W×H): 103mm*101*80m Operating temperature: -20 °C (min) Operating temperature: 50 °C (max) Design lifetime: 7 years ## Reaction Wheel RW100 — EXA (Astro-und Feinwerktechnik) [reaction-wheels] https://newspacemarket.com/products/rw100-reaction-wheel/ Angular momentum storage: 0.4 N·m·s @ as published, mode unspecified Max torque: 20 mN·m @ as published, mode unspecified Mass: 800 g @ as published, mode unspecified Power consumption: 2 W @ as published, mode unspecified Design lifetime: 7 years @ as published, mode unspecified Supply voltage: 18-34 V @ as published, mode unspecified Survival temperature: -40 °C Angular momentum storage: 0.4 N·m·s @ @6000rpm Wheel speed: 6000 @ Nominal Rotation Speed Max torque: 20 mN·m @ Nominal Torque Mass: 800 g (max) Envelope (L×W×H): 100mm*100mm*60mm Design lifetime: 7 years ## Reaction Wheel RW150 — EXA (Astro-und Feinwerktechnik) [reaction-wheels] https://newspacemarket.com/products/rw150-reaction-wheel/ Angular momentum storage: 1 N·m·s @ @6000rpm Max torque: 30 mN·m @ Nominal Torque Mass: 1300 g (max) Design lifetime: 7 years Angular momentum storage: 1 N·m·s @ as published, mode unspecified Max torque: 30 mN·m @ as published, mode unspecified Mass: 1300 g @ as published, mode unspecified Power consumption: 2 W @ as published, mode unspecified Design lifetime: 7 years @ as published, mode unspecified Supply voltage: 18-34 V @ as published, mode unspecified Wheel speed: 6000 Envelope (L×W×H): 150 mm x 150 mm x 60 mm Survival temperature: -40 °C ## Reaction Wheel RW250 — EXA (Astro-und Feinwerktechnik) [reaction-wheels] https://newspacemarket.com/products/rw250-reaction-wheel/ Angular momentum storage: 4 N·m·s @ @5000rpm Wheel speed: 5000 @ Nominal Rotation Speed Wheel speed: 5000 @ Maximum Rotation Speed Max torque: 100 mN·m @ Nominal Mass: 2700 g (max) Envelope (L×W×H): 180mm*180mm*82mm Operating temperature: -20 °C (min) Operating temperature: 50 °C (max) Design lifetime: 7 years Angular momentum storage: 4 N·m·s @ as published, mode unspecified Max torque: 100 mN·m @ as published, mode unspecified Mass: 2700 g @ as published, mode unspecified Power consumption: 2.5 W @ as published, mode unspecified Design lifetime: 7 years @ as published, mode unspecified Supply voltage: 23-34 V @ as published, mode unspecified Survival temperature: -40 °C ## Reaction Wheel RWT250 — EXA (Astro-und Feinwerktechnik) [reaction-wheels] https://newspacemarket.com/products/rwt250-reaction-wheel/ Angular momentum storage: 4 N·m·s @ as published, mode unspecified Max torque: 300 mN·m @ as published, mode unspecified Mass: 3000 g @ as published, mode unspecified Power consumption: 3 W @ as published, mode unspecified Design lifetime: 7 years @ as published, mode unspecified Supply voltage: 23-34 V @ as published, mode unspecified Survival temperature: -30 °C Angular momentum storage: 4 N·m·s @ @5000rpm Wheel speed: 5000 (nominal) Wheel speed: 5000 (max) Max torque: 300 mN·m (nominal) Mass: 3000 g (max) Envelope (L×W×H): 200mm*200mm*100mm Design lifetime: 7 years ## Reaction Wheel RW800 — EXA (Astro-und Feinwerktechnik) [reaction-wheels] https://newspacemarket.com/products/rw800-reaction-wheel/ Angular momentum storage: 12 N·m·s @ at 3600rpm Wheel speed: 3600 (nominal) Max torque: 200 mN·m (nominal) Mass: 6000 g (max) Envelope (L×W×H): 250mm*250mm*100mm Operating temperature: -20 °C (min) Operating temperature: 60 °C (max) Design lifetime: 15 years Angular momentum storage: 12 N·m·s @ as published, mode unspecified Max torque: 200 mN·m @ as published, mode unspecified Mass: 6000 g @ as published, mode unspecified Power consumption: 2.5 W @ as published, mode unspecified Design lifetime: 15.5 years @ as published, mode unspecified Supply voltage: 23-34 V @ as published, mode unspecified Survival temperature: -30 °C ## Reaction Wheel RW1500 — EXA (Astro-und Feinwerktechnik) [reaction-wheels] https://newspacemarket.com/products/rw1500-reaction-wheel/ Angular momentum storage: 25 N·m·s @ as published, mode unspecified Max torque: 200 mN·m @ as published, mode unspecified Mass: 6000 g @ as published, mode unspecified Power consumption: 2.5 W @ as published, mode unspecified Design lifetime: 15.5 years @ as published, mode unspecified Supply voltage: 22-37 V @ as published, mode unspecified Survival temperature: -40 °C Angular momentum storage: 25 N·m·s @ @4000rpm Wheel speed: 4000 (nominal) Max torque: 200 mN·m (nominal) Mass: 6000 g (max) Envelope (L×W×H): 320mm*320mm*120mm Operating temperature: -20 °C (min) Operating temperature: 60 °C (max) Design lifetime: 15 years ## Reaction Wheel RW3000 — EXA (Astro-und Feinwerktechnik) [reaction-wheels] https://newspacemarket.com/products/rw3000-reaction-wheel/ Angular momentum storage: 50 N·m·s @ @4000rpm Wheel speed: 4000 @ Nominal Rotation Speed Max torque: 200 mN·m @ Nominal Torque Mass: 9000 g (max) Envelope (L×W×H): 370mm*370mm*120mm Operating temperature: -20 °C (min) Operating temperature: 60 °C (max) Design lifetime: 15 years Angular momentum storage: 50 N·m·s @ as published, mode unspecified Max torque: 200 mN·m @ as published, mode unspecified Mass: 9000 g @ as published, mode unspecified Power consumption: 2.5 W @ as published, mode unspecified Design lifetime: 15.5 years @ as published, mode unspecified Supply voltage: 22-37 V @ as published, mode unspecified Survival temperature: -40 °C ## Reaction Wheel RW6000 — EXA (Astro-und Feinwerktechnik) [reaction-wheels] https://newspacemarket.com/products/rw6000-reaction-wheel/ Angular momentum storage: 100 N·m·s @ as published, mode unspecified Max torque: 200 mN·m @ as published, mode unspecified Mass: 12500 g @ as published, mode unspecified Power consumption: 5 W @ as published, mode unspecified Design lifetime: 15.5 years @ as published, mode unspecified Supply voltage: 23-34 V @ as published, mode unspecified Envelope (L×W×H): 446 x 442 x 149 mm3 Survival temperature: 0 °C Angular momentum storage: 100 N·m·s @ @4200rpm Wheel speed: 4200 (nominal) Max torque: 200 mN·m (nominal) Mass: 12500 g (max) Operating temperature: 0 °C (min) Operating temperature: 60 °C (max) Design lifetime: 15 years ## Reaction Wheels (RW25) — Serenum Space [reaction-wheels] https://newspacemarket.com/products/serenum-reaction-wheels/ Max torque: 0.2 mN·m @ as published, mode unspecified Mass: 40 g @ as published, mode unspecified Power consumption: 0.075 W @ as published, mode unspecified Radiation tolerance (TID): 36 krad @ as published, mode unspecified Supply voltage: 5-8 V @ as published, mode unspecified Envelope (L×W×H): 25 x 25 x 25 mm Static imbalance: 0.003 (max) Dynamic imbalance: 0.006 (max) Angular momentum storage: 0.0006 N·m·s ## TELDIX RSI 12 Momentum and Reaction Wheels — Collins Aerospace [reaction-wheels] https://newspacemarket.com/products/collins-teldix-rsi-12-reaction-wheel/ Angular momentum storage: 12 N·m·s @ as published, mode unspecified Design lifetime: 15 years @ as published, mode unspecified Flight heritage: 7,300+ years cumulative in-orbit operational time ## TELDIX RSI 45 Momentum and Reaction Wheels — Collins Aerospace [reaction-wheels] https://newspacemarket.com/products/collins-teldix-rsi-45-reaction-wheel/ Angular momentum storage: 45 N·m·s @ as published, mode unspecified Design lifetime: 15 years @ as published, mode unspecified Flight heritage: 7,300+ years cumulative in-orbit operational time ## TELDIX RSI 68 Momentum and Reaction Wheels — Collins Aerospace [reaction-wheels] https://newspacemarket.com/products/collins-teldix-rsi-68-reaction-wheel/ Angular momentum storage: 68 N·m·s @ as published, mode unspecified Design lifetime: 15 years @ as published, mode unspecified Flight heritage: 7,300+ years cumulative in-orbit operational time ## High Motor Torque Momentum and Reaction Wheels — Collins Aerospace [reaction-wheels] https://newspacemarket.com/products/collins-rsi-25-220-45-momentum-reaction-wheel/ Angular momentum storage: 68 N·m·s @ as published, mode unspecified Mass: 7150 g @ as published, mode unspecified Power consumption: 20 W @ as published, mode unspecified Design lifetime: 15 years @ as published, mode unspecified ## Teldix High Motor Torque Momentum and Reaction Wheels — Collins Aerospace [reaction-wheels] https://newspacemarket.com/products/collins-rsi-30-280-30-momentum-reaction-wheel/ Angular momentum storage: 68 N·m·s @ as published, mode unspecified Design lifetime: 15 years @ as published, mode unspecified Angular momentum storage: 68 N·m·s @ at nominal speed Max torque: 170 mN·m @ at nominal speed Wheel speed: 6000 (max) Wheel speed: -6000 (min) Mass: 8900 g (max) Envelope (L×W×H): 347 mm (Diameter) x 124 mm (Height) Supply voltage: 98 (min) Supply voltage: 102 (max) Power consumption: 20 W (max) @ Steady state at nominal speed Power consumption: 150 W (max) @ Maximum torque at nominal speed Operating temperature: -20 °C (min) Operating temperature: 70 °C (max) Survival temperature: -40 °C (min) Survival temperature: 70 °C (max) Design lifetime: 15 years @ in orbit Design lifetime: 15 years @ >, in orbit ## Reaction Wheels — Comat [reaction-wheels] https://newspacemarket.com/products/reaction-wheels/ Angular momentum storage: 50 N·m·s @ as published, mode unspecified Design lifetime: 8 years @ as published, mode unspecified ## Twinkle Star Tracker — arcsec [star-trackers] https://newspacemarket.com/products/arcsec-twinkle/ Attitude accuracy (cross-boresight): 3 @ 1 sigma, Cross-boresight accuracy Accuracy around boresight (roll): 30 @ 1 sigma, Around boresight accuracy Envelope (L×W×H): 20 x 20 x 40 mm Attitude accuracy (cross-boresight): 3 Accuracy around boresight (roll): 30 Limiting star magnitude: 7 Update rate: 10 Hz Field of view: 10.6 Power consumption: 1 W @ Nominal Data interface: RS485 Supply voltage: 5 Mass: 35 g ## SpectraTRAC Star Tracker — Adcole Space (Redwire) [star-trackers] https://newspacemarket.com/products/adcole-spectratrac-star-tracker/ Attitude accuracy (cross-boresight): 10 @ test capability Attitude accuracy (cross-boresight): 6 @ < Attitude accuracy (cross-boresight): 10 @ Cross Axis Accuracy around boresight (roll): 27 @ Boresight Update rate: 4 Hz Update rate: 4 Hz @ (variant 2) Max tracking slew rate: 2 @ maximum tracking rate > Max tracking slew rate: 2 @ Max Tracking Rate > Sun exclusion angle: 45 @ w/ Baffle Field of view: 19° x 14° Lost-in-space acquisition time: 0.23 s @ LIS, TYPICAL Lost-in-space acquisition time: 0.17 s @ TRACK, TYPICAL Limiting star magnitude: 6 Mass: 475 g @ baffle & star tracker Mass: 475 g @ w/Baffle Mass: 475 g @ including baffle, and star tracker Envelope (L×W×H): 120 X 61 X 61 mm w/Baffle Envelope (L×W×H): 120 x 61 x 61 mm @ (variant 2) Supply voltage: 5 @ DC Power consumption: 2.5 W @ Average Power consumption: 2.5 W @ < Data interface: RS-422 Operating temperature: -30 °C @ TO 55° Design lifetime: 5 years @ > in Low Earth Orbit (LEO) Attitude accuracy (cross-boresight): 6 @ <, test capability Max tracking slew rate: 2 @ > Lost-in-space acquisition time: 0.23 s @ LIS (Lost in Space), typical Envelope (L×W×H): 120 X 61 X 61 mm @ w/Baffle Power consumption: 2.5 W @ <, low power consumption Design lifetime: 5 @ >, design life in Low Earth Orbit (LEO) Flight heritage: decades of flight heritage combined with the agile and innovative culture of a commercial space platform Radiation tolerance (TID): 75 krad @ as published, mode unspecified Cycles / reuses: 5 @ Typical design life, based on each specific mission, 25% duty cycle ## VST-68M, VST-41M Star Trackers — VECTRONIC Aerospace GmbH [star-trackers] https://newspacemarket.com/products/vectronic-vst-68m/ Envelope (L×W×H): 60mm x 60mm x 138 mm @ with baffle Random vibration: 20 @ random 3 axis Radiation tolerance (TID): 20 krad @ > Attitude accuracy (cross-boresight): 5 Supply voltage: 9-40 V @ as published, mode unspecified Operating temperature: -20-65 °C @ as published, mode unspecified Envelope (L×W×H): 60mm x 60mm x 138 mm Mass: 470 g Radiation tolerance (TID): 20 krad @ gt Power consumption: 3 W Data interface: RS-422 Data interface: CAN @ (variant 2) Connector: MDM 25 male Attitude accuracy (cross-boresight): 5 @ x,y axis Accuracy around boresight (roll): 30 Update rate: 5 Hz Max tracking slew rate: 3 Field of view: 14° x 14° Lost-in-space acquisition time: 1 s @ Typ. Flight heritage: The predecessors of this sensor, the VST-41M series, have been successfully used in various small satellite missions. ## HYDRA Star Tracker — Sodern [star-trackers] https://newspacemarket.com/products/sodern-hydra-star-tracker/ Design lifetime: 10 years @ LEO Design lifetime: 18 years @ GEO Export status: ITAR Free Attitude accuracy (cross-boresight): 0.6 @ 3 sigma, Low Frequency Spatial Error (XY) Accuracy around boresight (roll): 4.6 @ 3 sigma, Low Frequency Spatial Error (Z) Attitude accuracy (cross-boresight): 3.4 @ 3 sigma, High Frequency Spatial Error (XY) Accuracy around boresight (roll): 27 @ 3 sigma, High Frequency Spatial Error (Z) Attitude accuracy (cross-boresight): 2.3 @ 3 sigma, Temporal noise (XY) Accuracy around boresight (roll): 18 @ 3 sigma, Temporal noise (Z) Max tracking slew rate: 6 @ in Acquisition Max tracking slew rate: 8 @ in Tracking Lost-in-space acquisition time: 2.2 s (typical) @ from lost-in-space Supply voltage: 5-5.5 Power consumption: 0.7 W (typical) @ OH, TEC OFF, @ 30°C, 5V Data interface: SpaceWire @ MIL 1355 wording in datasheet Operating temperature: -30-60 Survival temperature: -40-70 Random vibration: 30 @ OH Mass: 1400 g Attitude accuracy (cross-boresight): 3.4 @ High Frequency Spatial Error Accuracy around boresight (roll): 27 @ High Frequency Spatial Error Max tracking slew rate: 8 @ Tracking Lost-in-space acquisition time: 2.2 s @ typ Sun exclusion angle: 26 Envelope (L×W×H): 283 MM x 147 MM Supply voltage: 5 (nominal) Power consumption: 0.7 W @ OH, TEC OFF, typ Data interface: SpaceWire Update rate: 8 Hz Flight heritage: Flight-proven (TRL9) since 2014 ## MIST Miniature Integrated Star Tracker — Voyager Technologies [star-trackers] https://newspacemarket.com/products/mist-miniature-integrated-star-tracker/ Lost-in-space acquisition time: 1 s (max) @ Lost-in-space acquisition time Attitude accuracy (cross-boresight): 5 (typical) @ Attitude Knowledge Error, 1 sigma Random vibration: 14 @ Acceptance Random vibration: 20 @ Qualification Operating temperature: -24-61 °C @ as published, mode unspecified Lost-in-space acquisition time: 1 s (max) Limiting star magnitude: 6.5 Attitude accuracy (cross-boresight): 5 @ 1 sigma Max tracking slew rate: 1 @ no degradation Max tracking slew rate: 5 @ with degradation Update rate: 10 Hz Data interface: SpaceWire Data interface: RS-422 @ (variant 2) Field of view: 14 Sun exclusion angle: 45 Operating temperature: -24 °C (min) Operating temperature: 61 °C (max) Design lifetime: 10 years @ LEO Design lifetime: 18 years @ GEO Design lifetime: 12 years @ MEO Mass: 550 g @ with baffle Power consumption: 3.8 W @ Maximum Supply voltage: 5 Envelope (L×W×H): 10cm x 10cm x 5cm ## Redwire SpectraTRAC Star Tracker — Redwire Corporation [star-trackers] https://newspacemarket.com/products/redwire-spectratrac-star-tracker/ Design lifetime: 5 years @ >, LEO Attitude accuracy (cross-boresight): 10 @ cross-axis Attitude accuracy (cross-boresight): 6 @ cross-axis, < Max tracking slew rate: 2 @ max tracking rate Lost-in-space acquisition time: 0.23 s @ LIS (Lost-in-Space) Lost-in-space acquisition time: 0.17 s @ Track (Typical) Mass: 475 g @ baffle & star tracker Envelope (L×W×H): 120 X 61 X 61 @ L x W x H (mm) w/Baffle Supply voltage: 5 @ DC Voltage Power consumption: 2.5 W @ Average power consumption Power consumption: 2.5 W @ <, Low power consumption Design lifetime: 5 @ > , in Low Earth Orbit (LEO) Operating temperature: -30-55 °C @ as published, mode unspecified Design lifetime: 5 years @ LEO Cycles / reuses: 5 @ Typical design life, 25% duty cycle Design lifetime: 5 years @ >, Low Earth Orbit (LEO) Export status: This product is controlled for export from the United States. Contact Redwire for details. Field of view: 19 Attitude accuracy (cross-boresight): 10 @ Cross Axis Accuracy around boresight (roll): 27 @ Boresight Update rate: 4 Hz Max tracking slew rate: 2 (max) Sun exclusion angle: 45 @ w/ Baffle Lost-in-space acquisition time: 0.23 s @ LIS, TYPICAL Limiting star magnitude: 6 Mass: 475 g @ w/Baffle Supply voltage: 5 @ DC Power consumption: 2.5 W @ Average Operating temperature: -30 °C (min) Operating temperature: 55 °C (max) ## ARGO 1.0 Star Tracker — Hipparcos S.r.l. [star-trackers] https://newspacemarket.com/products/hipparcos-argo-1-0-star-tracker/ Field of view: 22.4 Update rate: 10 Hz Lost-in-space acquisition time: 3 s (max) @ from Lost in Space (up to 3°/s) Attitude accuracy (cross-boresight): 3 @ Systematic Error (BRF) - EOL - @1°/s, 1 OH (XY) Attitude accuracy (cross-boresight): 2 @ Systematic Error (BRF) - EOL - @1°/s, 2 OH (XYZ) Attitude accuracy (cross-boresight): 1 @ Systematic Error (BRF) - EOL - @1°/s, 3 OH (XYZ) Attitude accuracy (cross-boresight): 15 @ NEA (3σ) (BRF) - EOL - @1°/s, 1 OH (XY) Attitude accuracy (cross-boresight): 9 @ NEA (3σ) (BRF) - EOL - @1°/s, 2 OH (XYZ) Attitude accuracy (cross-boresight): 6 @ NEA (3σ) (BRF) - EOL - @1°/s, 3 OH (XYZ) Max tracking slew rate: 10 @ Max tracking rate, 1 OH Max tracking slew rate: 10 @ Max tracking rate, 2 OH Max tracking slew rate: 10 @ Max tracking rate, 3 OH Design lifetime: 5 years @ in LEO Radiation tolerance (TID): 30 krad @ Optical assembly Envelope (L×W×H): 73 x 91 x h79 @ Camera, incl. mounting feet Envelope (L×W×H): 106 x 91 x h39 @ RPCU, incl. mounting feet Mass: 385 g @ Camera Mass: 355 g @ RPCU Supply voltage: 9 (min) Supply voltage: 60 (max) Power consumption: 2.7 W @ Camera Power consumption: 1.1 W @ RPCU Data interface: Spacewire @ RPCU vs Spacecraft Data interface: RS-422 @ RPCU vs Spacecraft (variant 2) Data interface: CAN @ RPCU vs Spacecraft (variant 3) Operating temperature: -30 °C (min) Operating temperature: 60 °C (max) Survival temperature: -40 °C (min) Survival temperature: 70 °C (max) Flight heritage: since 2021 Field of view: 22.4 @ ± 11,2° implies a total FOV of 22.4 degrees Lost-in-space acquisition time: 3 s @ <, from Lost in Space (up to 3°/s) Attitude accuracy (cross-boresight): 15 @ 3 sigma, NEA (BRF) - EOL - @1°/s, 1 OH (XY) Attitude accuracy (cross-boresight): 9 @ 3 sigma, NEA (BRF) - EOL - @1°/s, 2 OH (XYZ) Attitude accuracy (cross-boresight): 6 @ 3 sigma, NEA (BRF) - EOL - @1°/s, 3 OH (XYZ) Max tracking slew rate: 10 Envelope (L×W×H): 106 x 91 x h39 @ RPCU Supply voltage: 9-60 Data interface: RPCU vs Spacecraft Data interface: RPCU vs Spacecraft @ (variant 2) Data interface: RPCU vs Spacecraft @ (variant 3) Operating temperature: -30-60 Survival temperature: -40-70 Random vibration: 17.38 @ Random vibration levels ## HST-A1 Star Tracker — TY-Space Technology [star-trackers] https://newspacemarket.com/products/ty-space-hst-a1-star-tracker/ Attitude accuracy (cross-boresight): 0.3 @ @0.1°/s, Pointing, 3σ Accuracy around boresight (roll): 3 @ @0.1°/s, Roll, 3σ Attitude accuracy (cross-boresight): 1 @ @0.5°/s, Pointing, 3σ Accuracy around boresight (roll): 15 @ @0.5°/s, Roll, 3σ Attitude accuracy (cross-boresight): 1.5 @ @1.0°/s, Pointing, 3σ Accuracy around boresight (roll): 20 @ @1.0°/s, Roll, 3σ Max tracking slew rate: 1.5 @ Trackable Field of view: 5.5 @ ≥5.5°×5.5° Lost-in-space acquisition time: 5 s @ Better than Sun exclusion angle: 30 @ Sun Design lifetime: 7 years @ @LEO Orbit Mass: 4200 g @ Device Weight (excluding baffle) Mass: 730 g @ Baffle Weight Operating temperature: -30 °C @ Operating Temperature Range (min) Operating temperature: 40 °C @ Operating Temperature Range (max) Operating temperature: 20 °C @ Best Operating Temperature Range (nominal) Survival temperature: -10 °C @ Storage Temperature Range (min) Survival temperature: 30 °C @ Storage Temperature Range (max) Power consumption: 3.5 W @ Operating State Supply voltage: 28 @ nominal Power consumption: 3.5 W Data interface: CAN Data interface: RS-422 @ (variant 2) Connector: J30J-15ZKNP8-J @ X1 Connector: J30J-15ZKNP8-J @ X2 Supply voltage: 26 @ min Supply voltage: 32 @ max Data interface: LVDS @ (variant 3) Connector: 12226-1150-00FR @ X3 Connector: 12226-1150-00FR @ X4 Data interface: other @ (variant 4) Attitude accuracy (cross-boresight): 0.3 (typical) Accuracy around boresight (roll): 3 (typical) Attitude accuracy (cross-boresight): 0.3 (typical) @ Pointing, 3σ, @0.1°/s Accuracy around boresight (roll): 3 (typical) @ Roll, 3σ, @0.1°/s Attitude accuracy (cross-boresight): 1 (typical) @ Pointing, 3σ, @0.5°/s Accuracy around boresight (roll): 15 (typical) @ Roll, 3σ, @0.5°/s Attitude accuracy (cross-boresight): 1.5 (typical) @ Pointing, 3σ, @1.0°/s Accuracy around boresight (roll): 20 (typical) @ Roll, 3σ, @1.0°/s Max tracking slew rate: 1.5 (max) @ Trackable Field of view: ≥5.5°×5.5° @ Field of View Update rate: 10 Hz (min) Sun exclusion angle: 30 @ better than, Sun exclusion Mass: 4200 g @ ±0.3, Device Weight (body) Envelope (L×W×H): 140±1×130±1 Height: 223±5 mm @ Envelope Size (body) Mass: 730 g @ ±0.05, Device Weight (baffle) Envelope (L×W×H): 155±2 Height: 297±5 mm @ Envelope Size (baffle) Power consumption: 3.5 W @ ±0.5, Operating State Supply voltage: 28 @ Supply voltage Power consumption: 3.5 W @ ±0.5, Power Consumption (Long Term Operating Mode) Connector: J30J-15ZKNP8-J @ X1 Electrical Connector Connector: J30J-15ZKNP8-J @ X2 Electrical Connector Connector: 12226-1150-00FR @ X3 Electrical Connector Connector: 12226-1150-00FR @ X4 Electrical Connector Design lifetime: 7 @ LEO Orbit Radiation tolerance (TID): 50 krad @ as published, mode unspecified Operating temperature: -10-30 °C @ as published, mode unspecified Attitude accuracy (cross-boresight): 0.3 Accuracy around boresight (roll): 3 Update rate: 10 Hz ## Sinclair Star Tracker (ST-16RT2) — Sinclair Interplanetary (Rocket Lab) [star-trackers] https://newspacemarket.com/products/sinclair-star-tracker-st-16rt2/ Attitude accuracy (cross-boresight): 5 @ cross-boresight Accuracy around boresight (roll): 55 @ around boresight Max tracking slew rate: 3 Update rate: 2 Hz Data interface: RS-485 @ Two half-duplex Supply voltage: 9 (min) Supply voltage: 34 (max) Power consumption: 0.5 W (max) @ Average Power consumption: 1 W @ Peak Operating temperature: -40 °C (min) Operating temperature: 50 °C (max) Survival temperature: -40 °C (min) Survival temperature: 95 °C (max) Design lifetime: 13 years @ LEO (800 km) Design lifetime: 9 years @ GEO Flight heritage: 13 first generation units on-orbit, first launch November 2013; 40 second generation units on-orbit, first launch June 2016 Field of view: 7.5° x 10° half-angle @ No Baffle Field of view: 8° half-angle @ Short Baffle Field of view: 7.5° x 10° half-angle @ Large Baffle Sun exclusion angle: 34 @ Short Baffle Sun exclusion angle: 22 @ Large Baffle Envelope (L×W×H): 62 x 56 x 38 mm @ No Baffle Envelope (L×W×H): 62 x 56 x 68 mm @ Short Baffle Envelope (L×W×H): 99 Ø x 120 mm @ Large Baffle Mass: 158 g @ No Baffle Mass: 185 g @ Short Baffle Mass: 235 g @ Large Baffle Flight heritage: 30 units on-orbit with customer-designed baffles; 13 units on-orbit; 10 units on-orbit @ (variant 2) Attitude accuracy (cross-boresight): 5 @ rms, cross-boresight Accuracy around boresight (roll): 55 @ rms, around boresight Update rate: 2 Hz @ attitude quaternion and angular rates Sun exclusion angle: 34 @ sun-to-boresight, Short Baffle Sun exclusion angle: 22 @ sun-to-boresight, Large Baffle Supply voltage: 9-34 Power consumption: 0.5 W @ <, Average Data interface: RS-485 @ two half-duplex, ±70 V fault tolerant Operating temperature: -40-50 @ operating Survival temperature: -40-95 @ survival Random vibration: 29.6 @ > Flight heritage: 30 units on-orbit with customer-designed baffles @ No Baffle Flight heritage: 13 units on-orbit @ Short Baffle Flight heritage: 10 units on-orbit @ Large Baffle Design lifetime: 13 years @ LEO ## Compact Star Tracker — Glavkosmos [star-trackers] https://newspacemarket.com/products/%d1%81ompact-star-tracker/ Mass: 193 g @ as published, mode unspecified Power consumption: 0.5 W @ as published, mode unspecified Design lifetime: 3 years @ as published, mode unspecified Lead time: 6 months @ as published, mode unspecified Supply voltage: 5-5 V @ as published, mode unspecified Attitude accuracy (cross-boresight): 5 Envelope (L×W×H): 56 × 60 × 93 mm ## Star Tracker GEO — Glavkosmos [star-trackers] https://newspacemarket.com/products/star-tracker-geo/ Mass: 800 g @ as published, mode unspecified Power consumption: 5 W @ as published, mode unspecified Design lifetime: 5 years @ as published, mode unspecified Lead time: 6 months @ as published, mode unspecified Supply voltage: 10-32 V @ as published, mode unspecified Operating temperature: -40-50 °C @ as published, mode unspecified Attitude accuracy (cross-boresight): 1.5 Attitude accuracy (cross-boresight): 1 @ (variant 2) Envelope (L×W×H): 149 × 100 × 137 mm Sun exclusion angle: 30 ## Star Tracker LEO — Glavkosmos [star-trackers] https://newspacemarket.com/products/star-tracker-leo/ Mass: 500 g @ as published, mode unspecified Power consumption: 5 W @ as published, mode unspecified Design lifetime: 5 years @ as published, mode unspecified Lead time: 6 months @ as published, mode unspecified Supply voltage: 10-32 V @ as published, mode unspecified Operating temperature: -40-50 °C @ as published, mode unspecified Attitude accuracy (cross-boresight): 1.5 Attitude accuracy (cross-boresight): 1 @ (variant 2) Envelope (L×W×H): 149 × 100 × 137 mm Sun exclusion angle: 30 ## Sagitta Star Tracker — arcsec [star-trackers] https://newspacemarket.com/products/arcsec-sagitta/ Power consumption: 1.5 W @ as published, mode unspecified Supply voltage: 5-5 V @ as published, mode unspecified Attitude accuracy (cross-boresight): 2 Attitude accuracy (cross-boresight): 10 @ (variant 2) Envelope (L×W×H): 44 x 50 x 95 mm ## Scorpio Star Tracker — arcsec [star-trackers] https://newspacemarket.com/products/arcsec-scorpio/ Limiting star magnitude: 6.2 Update rate: 7 Hz Field of view: 24.8 Sun exclusion angle: 30 @ baffle Power consumption: 2 W @ Nominal Data interface: RS485 Supply voltage: 5 Mass: 450 g Mass: 450 g @ as published, mode unspecified Power consumption: 2 W @ as published, mode unspecified Supply voltage: 5-5 V @ as published, mode unspecified Attitude accuracy (cross-boresight): 2 Accuracy around boresight (roll): 10 Envelope (L×W×H): 72 x 72 x 162 mm ## ARGO-2 High Performance Star Tracker System (HSTS-2) — Tsd-space [star-trackers] https://newspacemarket.com/products/tsd-space-argo-2-star-tracker/ Mass: 250 g @ as published, mode unspecified Power consumption: 3 W @ as published, mode unspecified Radiation tolerance (TID): 20 krad @ as published, mode unspecified Supply voltage: 5-5 V @ as published, mode unspecified Envelope (L×W×H): 95 mm x 94 mm x 22 mm ## PST4S-H1 Star Tracker — TY-Space Technology [star-trackers] https://newspacemarket.com/products/ty-space-pst4s-h1-star-tracker/ Mass: 310 g @ as published, mode unspecified Power consumption: 0.9 W @ as published, mode unspecified Design lifetime: 5 years @ as published, mode unspecified Radiation tolerance (TID): 30 krad @ as published, mode unspecified Supply voltage: 5-5 V @ as published, mode unspecified Operating temperature: -40-40 °C @ as published, mode unspecified Envelope (L×W×H): 57x57x141 mm3 Attitude accuracy (cross-boresight): 3 @ Pointing Accuracy around boresight (roll): 30 @ Roll Max tracking slew rate: 0.1 @ Pointing Attitude accuracy (cross-boresight): 3 @ @0.1°/s Pointing Accuracy around boresight (roll): 30 @ @0.1°/s Roll Max tracking slew rate: 0.5 @ Pointing (variant 2) Attitude accuracy (cross-boresight): 5 @ @0.5°/s Pointing Accuracy around boresight (roll): 50 @ @0.5°/s Roll Max tracking slew rate: 1 @ Pointing (variant 3) Attitude accuracy (cross-boresight): 10 @ @1.0°/s Pointing Accuracy around boresight (roll): 100 @ @1.0°/s Roll Max tracking slew rate: 3 @ Trackable Update rate: 10 Hz (min) Lost-in-space acquisition time: 2 s (max) @ Lost-in-space acquisition Sun exclusion angle: 35 @ Sun Mass: 310 g Operating temperature: -30 °C (min) Operating temperature: 40 °C (max) Survival temperature: -30 °C (min) Survival temperature: 40 °C (max) Power consumption: 0.9 W @ Operating Supply voltage: 5 Supply voltage: 4.8 (min) @ Safe Operating Voltage Supply voltage: 5.4 (max) @ Safe Operating Voltage Design lifetime: 7 years ## PST3S-H4 Star Tracker — TY-Space Technology [star-trackers] https://newspacemarket.com/products/ty-space-pst3s-h4-star-tracker/ Attitude accuracy (cross-boresight): 5 @ Pointing Accuracy around boresight (roll): 50 Attitude accuracy (cross-boresight): 5 @ @0.1°/s Pointing Accuracy around boresight (roll): 50 @ @0.1°/s Attitude accuracy (cross-boresight): 8 @ @0.5°/s Pointing Accuracy around boresight (roll): 60 @ @0.5°/s Attitude accuracy (cross-boresight): 15 @ @1.0°/s Pointing Accuracy around boresight (roll): 120 @ @1.0°/s Max tracking slew rate: 3 @ Trackable Update rate: 10 Hz Lost-in-space acquisition time: 2 s @ Max Sun exclusion angle: 35 @ Sun Field of view: 80 @ cone from the top of the baffle Mass: 95 g Envelope (L×W×H): Φ64, Height: 98±2 Supply voltage: 5 @ Nominal Supply voltage: 4.8 @ Safe Operating (min) Supply voltage: 5.4 @ Safe Operating (max) Power consumption: 1 W @ Operating State Data interface: RS-422 Connector: J70A-2F2-037-431-TH Operating temperature: -30 °C @ Min Operating temperature: 40 °C @ Max Survival temperature: -30 °C @ Min Survival temperature: 40 °C @ Max Design lifetime: 3 years @ @500km Orbit Mass: 95 g @ as published, mode unspecified Power consumption: 1 W @ as published, mode unspecified Design lifetime: 5 years @ as published, mode unspecified Radiation tolerance (TID): 30 krad @ as published, mode unspecified Supply voltage: 5-5 V @ as published, mode unspecified Operating temperature: -40-40 °C @ as published, mode unspecified ## PST3S-H5 Star Tracker — TY-Space Technology [star-trackers] https://newspacemarket.com/products/ty-space-pst3s-h5-star-tracker/ Mass: 130 g @ as published, mode unspecified Power consumption: 1 W @ as published, mode unspecified Design lifetime: 5 years @ as published, mode unspecified Radiation tolerance (TID): 50 krad @ as published, mode unspecified Supply voltage: 5-5 V @ as published, mode unspecified Operating temperature: -40-40 °C @ as published, mode unspecified Attitude accuracy (cross-boresight): 3 @ Pointing Accuracy around boresight (roll): 30 Attitude accuracy (cross-boresight): 5 @ Pointing @0.1°/s Accuracy around boresight (roll): 50 @ @0.1°/s Attitude accuracy (cross-boresight): 8 @ Pointing @0.5°/s Accuracy around boresight (roll): 60 @ @0.5°/s Attitude accuracy (cross-boresight): 15 @ Pointing @1.0°/s Accuracy around boresight (roll): 120 @ @1.0°/s Update rate: 10 Hz (min) Max tracking slew rate: 3 @ Trackable Lost-in-space acquisition time: 2 s (max) Sun exclusion angle: 35 @ Sun Sun exclusion angle: 25 @ Earth Mass: 130 g Envelope (L×W×H): <Φ64, Height: 134±2 Power consumption: 1 W @ Operating State Data interface: RS-422 Connector: J70A-2F2-037-431-TH Design lifetime: 5 years @ 500km Orbit ## PST3S-K4 Star Tracker — TY-Space Technology [star-trackers] https://newspacemarket.com/products/ty-space-pst3s-k4-star-tracker/ Attitude accuracy (cross-boresight): 5 @ 3σ, Pointing @0.1°/s Accuracy around boresight (roll): 50 @ 3σ, Rolling @0.1°/s Attitude accuracy (cross-boresight): 8 @ 3σ, Pointing @0.5°/s Accuracy around boresight (roll): 80 @ 3σ, Rolling @0.5°/s Attitude accuracy (cross-boresight): 10 @ 3σ, Pointing @1.0°/s Accuracy around boresight (roll): 100 @ 3σ, Rolling @1.0°/s Max tracking slew rate: 2 @ Trackable Lost-in-space acquisition time: 2 s (max) Sun exclusion angle: 35 @ Sun Mass: 60 g @ ±10g Power consumption: 0.8 W @ ±0.1, Operating State Power consumption: 0.8 W @ ±0.1, Long Term Operating Mode Supply voltage: 5 Data interface: RS-422 Data interface: CAN @ (variant 2) Design lifetime: 5 years @ @500km Orbit Mass: 60 g @ as published, mode unspecified Power consumption: 0.9 W @ as published, mode unspecified Design lifetime: 5 years @ as published, mode unspecified Radiation tolerance (TID): 30 krad @ as published, mode unspecified Supply voltage: 5-5 V @ as published, mode unspecified Operating temperature: -40-40 °C @ as published, mode unspecified Attitude accuracy (cross-boresight): 5 Accuracy around boresight (roll): 50 Update rate: 10 Hz Envelope (L×W×H): Baffle Folded: 40×40×34.6 (mm³) Envelope (L×W×H): Baffle Deployed: 40×40×75.7 (mm³) @ (variant 2) ## NST10-G1 Star Tracker — TY-Space Technology [star-trackers] https://newspacemarket.com/products/ty-space-nst10-g1-star-tracker/ Mass: 90 g @ as published, mode unspecified Power consumption: 1.2 W @ as published, mode unspecified Design lifetime: 3 years @ as published, mode unspecified Radiation tolerance (TID): 30 krad @ as published, mode unspecified Supply voltage: 5-5 V @ as published, mode unspecified Operating temperature: -30-40 °C @ as published, mode unspecified Attitude accuracy (cross-boresight): 5 Accuracy around boresight (roll): 50 Max tracking slew rate: 10 Field of view: 18°×18° Update rate: 10 Hz @ Min. Lost-in-space acquisition time: 2 s @ Max. Acquisition Sun exclusion angle: 35 @ Sun Sun exclusion angle: 25 @ Earth or other stray light Design lifetime: 5 years @ @500Km Orbit Design lifetime: 3 years @ @1000Km Orbit Mass: 500 g Envelope (L×W×H): 90mm×90mm×200±2mm Operating temperature: -40 °C (min) Operating temperature: 45 °C (max) Survival temperature: -40 °C (min) Survival temperature: 45 °C (max) Power consumption: 2 W @ Operating state Supply voltage: 5 Power consumption: 2 W Data interface: RS-422 Data interface: LVDS @ (variant 2) Connector: J30J-37ZKN-J @ X1 Communication Connector: J30J-15ZKN-J @ X2 Power ## NST20-G2 Star Tracker — TY-Space Technology [star-trackers] https://newspacemarket.com/products/ty-space-nst20-g2-star-tracker/ Attitude accuracy (cross-boresight): 3 @ Pointing Accuracy around boresight (roll): 30 Max tracking slew rate: 20 Attitude accuracy (cross-boresight): 20 @ @20°/s Pointing Accuracy around boresight (roll): 200 @ @20°/s Roll Update rate: 20 Hz (min) Lost-in-space acquisition time: 2 s (max) Sun exclusion angle: 25 Design lifetime: 7 years @ 500km Orbit Design lifetime: 5 years @ 1,000km Orbit Mass: 1200 g Envelope (L×W×H): 140×120×268 Operating temperature: -40 °C (min) Operating temperature: 45 °C (max) Survival temperature: -40 °C (min) Survival temperature: 45 °C (max) Power consumption: 3.5 W @ Operating State Supply voltage: 21 (min) Supply voltage: 29.5 (max) Data interface: RS-422 Connector: J30J-37ZKN-J @ X1 Communication Interface Connector: J30J-15ZKN-J @ X2 Power Interface Mass: 1200 g @ as published, mode unspecified Power consumption: 4 W @ as published, mode unspecified Design lifetime: 7 years @ as published, mode unspecified Radiation tolerance (TID): 100 krad @ as published, mode unspecified Supply voltage: 28-28 V @ as published, mode unspecified Operating temperature: -30-50 °C @ as published, mode unspecified ## NST20-G3 Star Tracker — TY-Space Technology [star-trackers] https://newspacemarket.com/products/ty-space-nst20-g3-star-tracker/ Mass: 1200 g @ as published, mode unspecified Power consumption: 4 W @ as published, mode unspecified Design lifetime: 7 years @ as published, mode unspecified Radiation tolerance (TID): 100 krad @ as published, mode unspecified Supply voltage: 28-28 V @ as published, mode unspecified Operating temperature: -30-50 °C @ as published, mode unspecified Attitude accuracy (cross-boresight): 1 Accuracy around boresight (roll): 6 Attitude accuracy (cross-boresight): 2 @ 3σ, @0.1°/s-0.5% (Pointing) Attitude accuracy (cross-boresight): 5 @ 3σ, @0.5°/s-1.2% (Pointing) Accuracy around boresight (roll): 16 @ 3σ, @0.1°/s-0.5% (Roll) Accuracy around boresight (roll): 30 @ 3σ, @0.5°/s-1.2% (Roll) Update rate: 10 Hz Sun exclusion angle: 30 @ Sun Lost-in-space acquisition time: 2 s @ Max. Mass: 1200 g (nominal) Envelope (L×W×H): L: 140±0.5 B: 120±0.2 H: 272±2 Supply voltage: 28 (nominal) Supply voltage: 27 (min) Supply voltage: 29 (max) Power consumption: 4 W (nominal) @ Operating State Power consumption: 4 W (nominal) @ Operating Mode Data interface: RS-422 Connector: J30J-37ZKN-J @ X1 Communication Interface Connector: J30J-15ZKN-J @ X2 Power Interface Operating temperature: -30 °C (min) @ Operating Temperature Range Operating temperature: 40 °C (max) @ Operating Temperature Range Survival temperature: -30 °C (min) @ Storage Temperature Range Survival temperature: 40 °C (max) @ Storage Temperature Range Design lifetime: 7 years @ 1000km Orbit ## NST4S-A2 Star Tracker — TY-Space Technology [star-trackers] https://newspacemarket.com/products/ty-space-nst4s-a2-star-tracker/ Attitude accuracy (cross-boresight): 3 @ Pointing Accuracy around boresight (roll): 30 @ Roll Attitude accuracy (cross-boresight): 3 @ @0.1°/s Accuracy around boresight (roll): 30 @ @0.1°/s Attitude accuracy (cross-boresight): 5 @ @0.5°/s Accuracy around boresight (roll): 50 @ @0.5°/s Attitude accuracy (cross-boresight): 10 @ @1.0°/s Accuracy around boresight (roll): 100 @ @1.0°/s Update rate: 10 Hz (min) Max tracking slew rate: 3 @ Trackable Lost-in-space acquisition time: 2 s (max) @ Acquisition Sun exclusion angle: 25 @ Sun Field of view: 80 @ cone Mass: 370 g Envelope (L×W×H): Φ100±1 x 182±2 Supply voltage: 5 @ Nominal Supply voltage: 4.8-5.4 @ Safe Operating Power consumption: 0.9 W @ Operating State Power consumption: 0.9 W @ Long Term Operating Connector: J30J-31ZKWP3-J Operating temperature: -30-40 °C Survival temperature: -30-40 °C Design lifetime: 7 years @ @1200km Orbit Mass: 370 g @ as published, mode unspecified Power consumption: 0.9 W @ as published, mode unspecified Design lifetime: 7 years @ as published, mode unspecified Radiation tolerance (TID): 50 krad @ as published, mode unspecified Supply voltage: 5-5 V @ as published, mode unspecified Operating temperature: -40-40 °C @ as published, mode unspecified Flight heritage: More than 50 sets of NST4S-A2 are work well on orbit. ## NST5S-A1 Star Tracker — TY-Space Technology [star-trackers] https://newspacemarket.com/products/ty-space-nst5s-a1-star-tracker/ Mass: 380 g @ as published, mode unspecified Power consumption: 1.5 W @ as published, mode unspecified Design lifetime: 7 years @ as published, mode unspecified Radiation tolerance (TID): 50 krad @ as published, mode unspecified Supply voltage: 5-5 V @ as published, mode unspecified Operating temperature: -40-40 °C @ as published, mode unspecified Attitude accuracy (cross-boresight): 1 Accuracy around boresight (roll): 10 Attitude accuracy (cross-boresight): 2 @ @0.1°/s, Pointing, 3σ Accuracy around boresight (roll): 15 @ @0.1°/s, Roll, 3σ Attitude accuracy (cross-boresight): 5 @ @0.5°/s, Pointing, 3σ Accuracy around boresight (roll): 35 @ @0.5°/s, Roll, 3σ Attitude accuracy (cross-boresight): 7 @ @1.0°/s, Pointing, 3σ Accuracy around boresight (roll): 50 @ @1.0°/s, Roll, 3σ Max tracking slew rate: 3 @ Trackable Update rate: 10 Hz (min) Lost-in-space acquisition time: 2 s (max) Sun exclusion angle: 35 @ Sun Data interface: RS-422 Design lifetime: 7 years Mass: 420 g Envelope (L×W×H): (78.2±1)×(78±1) Height: 168±2 Power consumption: 1.5 W @ Operating State Connector: J30J-31ZKNP30-J ## HORUS Star Tracker — Sodern [star-trackers] https://newspacemarket.com/products/sodern-horus-star-tracker/ Design lifetime: 10 years @ LEO Design lifetime: 18 years @ GEO Mass: 1600 g Sun exclusion angle: 24 @ Baffle Sun Exclusion Angle Lost-in-space acquisition time: 2.9 s @ typ Max tracking slew rate: 6 @ in Acquisition Max tracking slew rate: 8 @ in Tracking Envelope (L×W×H): 141 X 141 MM Envelope (L×W×H): 250 MM @ baffle length Operating temperature: -30 °C (min) Operating temperature: 50 °C (max) Survival temperature: -40 °C (min) Survival temperature: 70 °C (max) Design lifetime: 10 years @ in LEO Design lifetime: 18 years @ in GEO Supply voltage: 70 (min) Supply voltage: 105 (max) Supply voltage: 24 (min) @ (variant 2) Supply voltage: 50 (max) @ (variant 2) Power consumption: 7 W (max) @ typ, TEC OFF Data interface: MIL-STD-1553 Update rate: 8 Hz Update rate: 10 Hz @ (variant 2) Mass: 1600 g @ as published, mode unspecified Design lifetime: 18 years @ as published, mode unspecified Supply voltage: 24-50 V @ as published, mode unspecified Attitude accuracy (cross-boresight): 3.5 (max) Accuracy around boresight (roll): 25 (max) ## uSTAR-250 Star Tracker — Voyager Technologies [star-trackers] https://newspacemarket.com/products/ustar-250-star-tracker/ Mass: 750 g @ as published, mode unspecified Operating temperature: -30-50 °C @ as published, mode unspecified ## NST-3 Nano Star Tracker — TY-Space Technology [star-trackers] https://newspacemarket.com/products/nst-3-nano-star-tracker/ Mass: 165 g @ as published, mode unspecified ## Star Tracker – CubeStar — CubeSpace ADCS [star-trackers] https://newspacemarket.com/products/star-tracker-cubestar/ Lead time: 3.6822 months @ as published, mode unspecified ## Blue Canyon Technologies nano star tracker (NST) — Blue Canyon Technologies [star-trackers] https://newspacemarket.com/products/bct-cubesat-battery-packs/ Design lifetime: 5 years @ as published, mode unspecified ## ASTRO CL Star Tracker — Jena-Optronik [star-trackers] https://newspacemarket.com/products/jena-optronik-astro-cl/ Mass: 320 g @ as published, mode unspecified Power consumption: 1.2 W @ as published, mode unspecified Radiation tolerance (TID): 15 krad @ as published, mode unspecified Supply voltage: 4.2-5.5 V @ as published, mode unspecified Operating temperature: -35-50 °C @ as published, mode unspecified Update rate: 5 Hz Max tracking slew rate: 3 (min) Limiting star magnitude: 5.8 Envelope (L×W×H): 60 x 60 x 129 mm Sun exclusion angle: 26 ## ASTRO APS Autonomous Star Sensor — Jena-Optronik [star-trackers] https://newspacemarket.com/products/jena-optronik-astro-aps/ Mass: 2000 g @ as published, mode unspecified Power consumption: 6 W @ as published, mode unspecified Design lifetime: 18 years @ as published, mode unspecified Supply voltage: 28-28 V @ as published, mode unspecified Operating temperature: -30-60 °C @ as published, mode unspecified Field of view: 20 Envelope (L×W×H): 154 x 154 x 237 mm (incl. baffle) Sun exclusion angle: 26 ## ASTRO APS3 Autonomous Star Sensor — Jena-Optronik [star-trackers] https://newspacemarket.com/products/jena-optronik-astro-aps3/ Mass: 1800 g @ as published, mode unspecified Power consumption: 6 W @ as published, mode unspecified Radiation tolerance (TID): 15 krad @ as published, mode unspecified Supply voltage: 5-5 V @ as published, mode unspecified Operating temperature: -30-60 °C @ as published, mode unspecified Max tracking slew rate: 6 (max) Limiting star magnitude: 7 Envelope (L×W×H): 148 x 142 x 210 mm (incl. baffle) Sun exclusion angle: 26 ## ASTRO XP High Accuracy Star Tracker — Jena-Optronik [star-trackers] https://newspacemarket.com/products/jena-optronik-astro-xp/ Mass: 2500 g @ as published, mode unspecified Power consumption: 1.5 W @ as published, mode unspecified Radiation tolerance (TID): 65 krad @ as published, mode unspecified Supply voltage: 28-100 V @ as published, mode unspecified Operating temperature: -40-30 °C @ as published, mode unspecified Field of view: 3.3 Update rate: 2 Hz Attitude accuracy (cross-boresight): 3.5 (max) Lost-in-space acquisition time: 1 s (max) Envelope (L×W×H): 215 x 215 x 321 mm Envelope (L×W×H): 137 x 146 x 60 mm @ (variant 2) Sun exclusion angle: 30 ## AURIGA CP Star Tracker — Sodern [star-trackers] https://newspacemarket.com/products/sodern-auriga-cp-star-tracker/ Design lifetime: 10 years @ in LEO orbit (400-1200 km) Design lifetime: 15 years @ in GEO orbit Flight heritage: FLIGHT PROVEN SINCE 2019, OVER 1500 UNITS LAUNCHED Sun exclusion angle: 35 @ standard Attitude accuracy (cross-boresight): 9 @ 3sigma, Low Frequency spatial (FOV) error XY Accuracy around boresight (roll): 51 @ 3sigma, Low Frequency spatial (FOV) error Z Attitude accuracy (cross-boresight): 6.6 @ 3sigma, High Frequency spatial (Pixel) error XY Accuracy around boresight (roll): 38 @ 3sigma, High Frequency spatial (Pixel) error Z Max tracking slew rate: 0.3 @ in Acquisition, baseline Max tracking slew rate: 2 @ in Acquisition, up to Max tracking slew rate: 3 @ in Tracking, up to Sun exclusion angle: 26 @ baffle add-on Max tracking slew rate: 4 @ in Acquisition, with Auriga-gyro software option, up to Max tracking slew rate: 10 @ in Tracking, with Auriga-gyro software option, up to Update rate: 10 Hz @ Software operating frequency, up to Operating temperature: -20 °C (min) @ Optical head (OH) Operating temperature: 40 °C (max) @ Optical head (OH) Survival temperature: -30 °C (min) @ Optical head (OH) & Electronic Unit (EU) Survival temperature: 70 °C (max) @ Optical head (OH) & Electronic Unit (EU) Envelope (L×W×H): 66 x 59 x 94 (height, including baffle) @ Optical head (OH) Mass: 225 g @ Optical head (OH), including baffle Envelope (L×W×H): 91 x 117 x 25 (height) @ Electronic Unit (EU) Mass: 315 g @ Electronic Unit (EU) Design lifetime: 10 years @ in LEO 400-1200km Design lifetime: 15 years @ in GEO with EOR Supply voltage: 5 @ Optical head (OH) Supply voltage: 4.75 (min) @ Electronic Unit (EU) Supply voltage: 5.5 (max) @ Electronic Unit (EU) Power consumption: 0.8 W @ Optical head (OH), typical Power consumption: 1 W @ Optical head (OH), max Power consumption: 2.1 W @ Electronic Unit (EU), typical Power consumption: 3.4 W @ Electronic Unit (EU), max Data interface: SpaceWire @ Optical head (OH) Data interface: RS422 @ Electronic Unit (EU) Data interface: UART @ Electronic Unit (EU) (variant 2) Data interface: CAN @ Electronic Unit (EU) (variant 3) Update rate: 8 Hz @ Optical head (OH) Update rate: 10 Hz @ Optical head (OH) (variant 2) Update rate: 5 Hz @ Optical head (OH), possible to relax CPU load Update rate: 8 Hz @ Electronic Unit (EU) Update rate: 10 Hz @ Electronic Unit (EU) (variant 2) Lost-in-space acquisition time: 3.8 s @ typical from lost-in-space Sun exclusion angle: 35 @ Baffle Sun Exclusion Angle Design lifetime: 15 years @ as published, mode unspecified Envelope (L×W×H): 6U and above ## A-STR Autonomous Star Tracker — Leonardo SpA (Space Division) [star-trackers] https://newspacemarket.com/products/leonardo-a-str-autonomous-star-tracker/ Mass: 3550 g @ as published, mode unspecified Power consumption: 8.9 W @ as published, mode unspecified Design lifetime: 18 years @ as published, mode unspecified Supply voltage: 20-50 V @ as published, mode unspecified Operating temperature: -30-60 °C @ as published, mode unspecified Field of view: 16.4 Lost-in-space acquisition time: 6 s (max) Update rate: 10 Hz Envelope (L×W×H): 195 x 175 x 290.5 mm (40 deg SEA baffle) ## AA-STR Autonomous Star Tracker — Leonardo SpA (Space Division) [star-trackers] https://newspacemarket.com/products/leonardo-aa-str-autonomous-star-tracker/ Mass: 2600 g @ as published, mode unspecified Power consumption: 5.6 W @ as published, mode unspecified Design lifetime: 18 years @ as published, mode unspecified Supply voltage: 60-110 V @ as published, mode unspecified Operating temperature: -30-60 °C @ as published, mode unspecified Field of view: 20 Lost-in-space acquisition time: 9 s (max) Update rate: 10 Hz Envelope (L×W×H): 164 x 156 x 348 mm (25 deg SEA baffle) ## Nano Star Trackers (NST) — Blue Canyon Technologies [star-trackers] https://newspacemarket.com/products/bct-mid-extension-nst-star-tracker/ Mass: 350 g @ as published, mode unspecified Envelope (L×W×H): 10 x 5 x 5.5 cm Attitude accuracy (cross-boresight): 6 Attitude accuracy (cross-boresight): 40 @ (variant 2) Envelope (L×W×H): 17 x 8.5 x 7 cm @ (variant 2) Attitude accuracy (cross-boresight): 1 @ (variant 3) Attitude accuracy (cross-boresight): 10 @ (variant 4) Envelope (L×W×H): 25 x 10 x 10 cm @ (variant 3) Attitude accuracy (cross-boresight): 1 @ (variant 5) Attitude accuracy (cross-boresight): 10 @ (variant 6) ## Nano Star Trackers — Blue Canyon Technologies [star-trackers] https://newspacemarket.com/products/bct-full-extension-nst-star-tracker/ Mass: 35000 g @ as published, mode unspecified Envelope (L×W×H): 10 x 5 x 5.5 cm Attitude accuracy (cross-boresight): 6 Attitude accuracy (cross-boresight): 40 @ (variant 2) Envelope (L×W×H): 17 x 8.5 x 7 cm @ (variant 2) Attitude accuracy (cross-boresight): 1 @ (variant 3) Attitude accuracy (cross-boresight): 10 @ (variant 4) Envelope (L×W×H): 25 x 10 x 10 cm @ (variant 3) Attitude accuracy (cross-boresight): 1 @ (variant 5) Attitude accuracy (cross-boresight): 10 @ (variant 6) ## Star Tracker — HEX20 [star-trackers] https://newspacemarket.com/products/hex20-star-tracker/ Mass: 325 g @ as published, mode unspecified Power consumption: 5 W @ as published, mode unspecified Field of view: 10 Update rate: 5 Hz Envelope (L×W×H): 95x85x85 mm Sun exclusion angle: 30 TRL: 5 ## T3 Star Tracker — Terma [star-trackers] https://newspacemarket.com/products/terma-t3-star-tracker/ Mass: 350 g @ as published, mode unspecified Power consumption: 2 W @ as published, mode unspecified Design lifetime: 5 years @ as published, mode unspecified Supply voltage: 5-12 V @ as published, mode unspecified Operating temperature: -40-30 °C @ as published, mode unspecified Envelope (L×W×H): 100 × 60 × 60 mm Field of view: 20 Sun exclusion angle: 37.5 Update rate: 5 Hz (max) ## T1 Star Tracker — Terma [star-trackers] https://newspacemarket.com/products/terma-t1-star-tracker/ Mass: 1530 g @ as published, mode unspecified Power consumption: 3.25 W @ as published, mode unspecified Radiation tolerance (TID): 15 krad @ as published, mode unspecified Operating temperature: -40-30 °C @ as published, mode unspecified Envelope (L×W×H): 100 × 100 × 40 mm Field of view: 20 ## n-ART ST 1U Star Tracker — Gumush [star-trackers] https://newspacemarket.com/products/gumush-n-art-st-1u/ Mass: 100 g @ as published, mode unspecified ## n-ART ST 2U Star Tracker — Gumush [star-trackers] https://newspacemarket.com/products/gumush-n-art-st-2u/ Mass: 200 g @ as published, mode unspecified ## n-ART ST 3U Star Tracker — Gumush [star-trackers] https://newspacemarket.com/products/gumush-n-art-st-3u/ Mass: 300 g @ as published, mode unspecified ## OBC — Dragonfly Aerospace [obc-computers] https://newspacemarket.com/products/obc-2/ Design lifetime: 8 years @ LEO Data interface: RS-422 Operating temperature: -10 °C Envelope (L×W×H): 160 x 117 x 30.5 mm Mass: 350 g Design lifetime: 8 years (max) @ LEO Power consumption: 5 W Processor: Dual Core ARM-A9 CPU clock: 766 MHz RAM: 256 MB @ Dual Storage: 32 GB @ Dual SD Card Storage: 0.125 GB @ Dual Flash Data interface: other @ DCL (Direct Command Line) Operating system: Linux 4.14 build for Xiphos Q7S Design lifetime: 8 years @ up to, LEO Export status: ITAR-Free ## HYDROS-C Water Electrolysis Thruster — Tethers Unlimited, Inc. (AMERGINT) [propulsion] https://newspacemarket.com/products/tethers-unlimited-hydros-c-thruster/ Propulsion type: water @ derived from product name/propellant Propulsion type: water Flight heritage: Proven capability on-orbit Specific impulse: 310 (min) Thrust: 1200 mN (min) @ max Thrust: 2.2 mN @ Orbit-Averaged Total impulse: 1.75 N·s (min) @ per Thrust Event Total impulse: 2151 N·s (min) @ Delivered Propellant: water Propellant mass: 500 g Mass: 2200 g @ Dry Mass: 2700 g @ Wet Envelope (L×W×H): 190 x 130 x 92mm Power consumption: 5-25 W @ MAX W/ Heaters Power consumption: 16 W @ Nominal MAX Power consumption: 3.5 W @ Standby ## T6 Ion Thruster — QinetiQ Space [propulsion] https://newspacemarket.com/products/qinetiq-t6-ion-thruster/ Propulsion type: electric @ derived from product name/propellant Power consumption: 4.5 W Flight heritage: ESA BepiColombo (launched 2018), AlphaSat TDP#4 Propulsion type: electric Thrust: 30 mN (min) Thrust: 230 mN (max) Thrust: 75 mN (min) @ qualified for BepiColombo Thrust: 145 mN (max) @ qualified for BepiColombo Specific impulse: 4250 @ BOL, at 70mN Specific impulse: 3650 @ BOL, at 150mN Specific impulse: 4300 @ Kaufman thruster, at 1850V beam voltage, -265V accel voltage Specific impulse: 3200 @ Ring Cusp thruster, at 1000V beam voltage, -1115V accel voltage Propellant: xenon Feed/tank pressure: 2.5 bar (min) Feed/tank pressure: 3.5 bar (max) Power at thrust: 5000 W @ at 145mN thrust Power at thrust: 10000 W @ two thrusters, 290mN total thrust Power at thrust: 15000 W @ three thrusters, 435mN total thrust Power at thrust: 20000 W @ four thrusters, 580mN total thrust Supply voltage: 100 @ PPU input ## ENPULSION NANO Thruster (IFM Nano Thruster) — ENPULSION GmbH [propulsion] https://newspacemarket.com/products/enpulsion-nano-thruster/ Propulsion type: electric @ derived from product name/propellant Propulsion type: electric Thrust: 0.01 mN (min) @ dynamic thrust range Thrust: 0.4 mN (max) @ dynamic thrust range Thrust: 0.35 mN @ nominal thrust Specific impulse: 2000 (min) Specific impulse: 6000 (max) Total impulse: 5000 N·s (min) Propellant: indium Propellant mass: 230 g Power at thrust: 40 W @ at nominal thrust, incl. neutralizer Mass: 670 g @ dry Mass: 900 g @ wet Envelope (L×W×H): 100.0 x 100.0 x 82.5 mm Supply voltage: 12 Supply voltage: 28 @ (variant 2) Supply voltage: OTHER VOLTAGES UPON REQUEST @ (variant 3) Power consumption: 8 W (min) @ total system power, to operate thruster Power consumption: 40 W (max) @ total system power Power consumption: 3.5 W @ hot standby power Data interface: RS-422 Data interface: RS-485 @ (variant 2) Survival temperature: -40 °C (min) @ non-operational temperature envelope Survival temperature: 105 °C (max) @ non-operational temperature envelope Operating temperature: -20 °C (min) @ operational temperature envelope Operating temperature: 40 °C (max) @ operational temperature envelope Flight heritage: Successfully tested in orbit on a customer spacecraft in early 2018 ## SPS-100 Propulsion System — Space Electric Thruster Systems (SETS) [propulsion] https://newspacemarket.com/products/sets-sps-100-propulsion-system/ Propulsion type: electric @ derived from product name/propellant TRL: 4 Propulsion type: electric @ Hall-effect thruster Power at thrust: 1000 W @ Total power consumption Power at thrust: 1750 W @ Total power consumption (variant 2) Thrust: 95 mN (max) Specific impulse: 1900 (max) Total impulse: 3000 N·s (max) @ one thruster configuration Propellant: Xenon Propellant: Krypton @ (variant 2) Mass: 20000 g (max) @ Dry mass (without tank) ## SIRIUS-OBC-LEON3FT — AAC Clyde Space [obc-computers] https://newspacemarket.com/products/aac-smallsat-sirius-obc-leon3ft/ Data interface: UARTs Data interface: UARTs @ (variant 2) Operating temperature: -30-60 °C Supply voltage: 4.5 Processor: 32-bit LEON3FT (IEEE-1754 SPARC v8) fault-tolerant processor CPU clock: 50 MHz RAM: 64 MB @ post-EDAC Storage: 2 GB @ Nonvolatile System Memory Nand Flash, post-EDAC Operating system: RTEMS real-time operating system (RTOS) Mass: 130 g Envelope (L×W×H): 95.89 mm x 90.17 mm x 17.20 mm Power consumption: 1.3 W @ Nominal Data interface: SpaceWire @ 50 Mbps Data interface: RS-422 @ UARTs Data interface: RS-485 @ UARTs (variant 2) Data interface: CAN @ Implemented on optional daughter board Radiation tolerance (TID): 20 krad @ qualified >30 kRAD, Si Design lifetime: 5 years @ in LEO Flight heritage: over a decade of design heritage ## VACCO Thruster Valves — VACCO Industries [propulsion] https://newspacemarket.com/products/vacco-thruster-valves/ Thrust: 8896.44 mN Cycles / reuses: 150000 @ Operating Cycles Random vibration: 6.28 Propulsion type: cold-gas Feed/tank pressure: 17.9264 bar @ Operating Pressure Feed/tank pressure: 43.437 bar @ Proof Pressure Feed/tank pressure: 57.916 bar @ Burst Pressure Time to thrust: 7 s @ Opening @ 16.8 VDC, 230 psig Time to thrust: 4 s @ Closing @ 230 psig Propellant: GN2 Power consumption: 20 W @ at 17 VDC Supply voltage: 12-21 @ Operating Voltage Operating temperature: -20-150 °C Flight heritage: Space Shuttle Manned Maneuvering Unit ## FoX NavRIX GEO GNSS Receiver — Beyond Gravity (ex-RUAG Space) [gnss-receivers] https://newspacemarket.com/products/beyond-gravity-fox-navrix-geo-gnss-receiver/ Data interface: RS-422 Position accuracy: 10 m @ 3D typ. Velocity accuracy: 0.01 m/s @ 3D rms Time to first fix (cold): 900 s @ Warm start typ. (GEO) Constellations: GPS L1 C/A Constellations: Galileo E1 B/C @ (variant 2) Mass: 4000 g @ 2 GNSSR, 2 antennas, 2 LNAs Envelope (L×W×H): 217x148x131mm3 @ box incl. feet Supply voltage: 28 (nominal) @ unregulated Power consumption: 10 W (max) Data interface: UART @ RS-422 Data interface: RS-422 @ PPS outputs Operating temperature: -30 °C (min) Operating temperature: 70 °C (max) Radiation tolerance (TID): 36 krad Design lifetime: 10 years @ in GEO Flight heritage: TEMPO (NASA) Flight heritage: SWARM (ESA) @ (variant 2) Flight heritage: Sentinel-1, Sentinel-2 and Sentinel-3 A/B (Copernicus) @ (variant 3) Flight heritage: Sentinel-1, Sentinel-2 and Sentinel-3 C/D @ (variant 4) Flight heritage: Sentinel-6/Michael Freilich A/B (NASA/ESA) @ (variant 5) Flight heritage: EarthCare (ESA/JAXA) @ (variant 6) Flight heritage: ICESat-2 (NASA) @ (variant 7) Flight heritage: PACE (NASA) @ (variant 8) Flight heritage: OSAM-1 (NASA) @ (variant 9) Flight heritage: Biomass (ESA) @ (variant 10) Flight heritage: FLEX (ESA) @ (variant 11) Flight heritage: KOMPSAT-6,-7 (KARI) @ (variant 12) Flight heritage: CAS-500 (KARI/KAI) @ (variant 13) Flight heritage: WSF-M (BAE) @ (variant 14) ## Canisterized Satellite Dispenser (CSD) — Planetary Systems Corp (Rocket Lab) [deployers] https://newspacemarket.com/products/psc-rocket-lab-canisterized-satellite-dispenser/ Cycles / reuses: 50 @ Allowable number of door closures by customer before refurbishment is required Envelope (L×W×H): 3U, 6U, 12U Separation velocity: 1 m/s Mass: 3320 g (min) @ 3U, Empty. ±3% Mass: 4500 g (min) @ 6U, Empty. ±3% Mass: 5650 g (min) @ 12U, Empty. ±3% Capacity: 3 @ 3U Capacity: 6 @ 6U Capacity: 12 @ 12U Actuation: motor Supply voltage: 22 (min) @ Power to pins 1 & 2, return from pins 3 & 4 Open Door Supply voltage: 34 (max) @ Power to pins 1 & 2, return from pins 3 & 4 Open Door Operating temperature: -34 °C (min) @ Qualification limits Operating temperature: 80 °C (max) @ Qualification limits Survival temperature: -50 °C (min) @ Qualification limits Survival temperature: 90 °C (max) @ Qualification limits Flight heritage: Attained TRL 9 with flight heritage in 2013. Flight heritage: A 3U CSD flew aboard the inaugural Falcon 9 v1.1 flight on September 2013 and released the 7-piece POPACS payload in orbit. @ (variant 2) ## VACCO Latch Valves / Isolation Valves — VACCO Industries [tanks-valves] https://newspacemarket.com/products/vacco-latch-valves-isolation-valves/ Cycles / reuses: 25000 @ Cycle Life Flight heritage: In production since 1988 Flight heritage: Boeing HS601/HS702, Astrium Eurostar 3000, Mitsubishi DS2000, ATV, HTV, Cygnus @ (variant 2) Supply voltage: 20-54 Operating pressure (MEOP): 137.8952 bar Material: Titanium Mass: 340 g ## nanoST — Solar MEMS Technologies [star-trackers] https://newspacemarket.com/products/solar-mems-nanost/ Design lifetime: 5 years @ >, LEO Design lifetime: 8 years @ up to, LEO, without additional shielding Attitude accuracy (cross-boresight): 30 Accuracy around boresight (roll): 200 Export status: ITAR FREE Random vibration: 20 Random vibration: 20.1 @ (variant 2) Random vibration: 1500 @ (variant 3) Field of view: 15 @ Full Lost-in-space acquisition time: 3 s @ max Max tracking slew rate: 0.2 @ Nominal Max tracking slew rate: 1 @ Max. Update rate: 1.5 Hz @ min Limiting star magnitude: 6.2 Envelope (L×W×H): 90 x 52 x 39 mm Sun exclusion angle: 45 @ Cubesat Sun exclusion angle: 30 @ Cubesat (on demand) Mass: 150 g Supply voltage: 5 Power consumption: 1.2 W Operating temperature: -20 °C (min) @ Nominal performance Operating temperature: 50 °C (max) @ Nominal performance Survival temperature: -45 °C (min) Survival temperature: 85 °C (max) Design lifetime: 5 years @ in LEO Design lifetime: 8 years @ in LEO without additional shielding ## MicroST — Solar MEMS Technologies [star-trackers] https://newspacemarket.com/products/solar-mems-microst/ Lost-in-space acquisition time: 2 s @ <, from LiS Max tracking slew rate: 0.5 @ Nominal Max tracking slew rate: 2.5 @ Without LiS Max tracking slew rate: 3.5 @ Max Update rate: 5 Hz Update rate: 10 Hz @ (variant 2) Sun exclusion angle: 36 @ < Limiting star magnitude: 6.5 @ 6.5 - 7 Limiting star magnitude: 7 @ 6.5 - 7 (variant 2) Operating temperature: -30 °C @ Operating temperature Operating temperature: 50 °C @ Operating temperature (variant 2) Survival temperature: -40 °C @ Qualification temperature Survival temperature: 60 °C @ Qualification temperature (variant 2) Radiation tolerance (TID): 30 krad Design lifetime: 12 years @ >, LEO Data interface: RS422 @ upon request Data interface: CAN @ upon request (variant 2) Data interface: Ethernet @ upon request (variant 3) Supply voltage: 5 Power consumption: 3.5 W Envelope (L×W×H): 70 x 70 x 150 mm Mass: 600 g Attitude accuracy (cross-boresight): 6 Accuracy around boresight (roll): 48 Random vibration: 20 Random vibration: 20.1 @ (variant 2) Random vibration: 1500 @ (variant 3) ## Hydra — Sodern [star-trackers] https://newspacemarket.com/products/sodern-hydra-access-star-tracker/ Update rate: 8 Hz Max tracking slew rate: 6 (max) @ in Acquisition Max tracking slew rate: 8 (max) @ in Tracking Sun exclusion angle: 26 @ Sun Exclusion Angle Lost-in-space acquisition time: 2.2 s @ lost-in-space Mass: 1400 g Supply voltage: 5 Power consumption: 0.7 W @ OH, typ, TEC OFF, @ 30°C, 5V Operating temperature: -30 °C @ min Operating temperature: 60 °C @ max Survival temperature: -40 °C @ min Survival temperature: 70 °C @ max Attitude accuracy (cross-boresight): 3.4 Accuracy around boresight (roll): 27 Flight heritage: More than 245 units launched, flight-proven since 2012, over ten million hours in operation Design lifetime: 10 years @ LEO Design lifetime: 18 years @ GEO ## ST400 — Berlin Space Technologies [star-trackers] https://newspacemarket.com/products/bst-st400-star-tracker/ Attitude accuracy (cross-boresight): 5 Accuracy around boresight (roll): 40 Limiting star magnitude: 6 Data interface: RS-422 Supply voltage: 3.7-5 Power consumption: 0.67 W @ @ 3.7V Envelope (L×W×H): 48x57x89mm³ @ ST400D Envelope (L×W×H): 74x74x146mm³ @ with Baffle 40° Sun Exclusion Mass: 270 g @ ST400D Mass: 350 g @ with Baffle 40° Sun Exclusion Operating temperature: -20-40 °C Update rate: 5 Hz (max) Max tracking slew rate: 0.3 @ nominal conditions (pitch, yaw) Max tracking slew rate: 1 @ nominal conditions (pure roll) Radiation tolerance (TID): 11 krad @ Proton 130 MeV Design lifetime: 5 years @ LEO Sun exclusion angle: 40 @ Baffle Flight heritage: space heritage ## Hydra — Safran Electronics Defense Space [star-trackers] https://newspacemarket.com/products/safran-sodern-hydra-star-tracker/ Attitude accuracy (cross-boresight): 3.4 Accuracy around boresight (roll): 27 Lead time: 8 Attitude accuracy (cross-boresight): 4.1 @ sigma, XY Accuracy around boresight (roll): 32 @ sigma, Z Max tracking slew rate: 6 (max) @ acquisition Max tracking slew rate: 8 (max) @ tracking Sun exclusion angle: 26 @ optical head Lost-in-space acquisition time: 2.2 s (typical) @ lost-in-space Max tracking slew rate: 6 (max) @ acquisition (variant 2) Max tracking slew rate: 8 (max) @ tracking (variant 2) Sun exclusion angle: 26 @ Sun Exclusion Angle (SEA) Sun exclusion angle: 18.5 @ Earth Exclusion Angle (EEA) Supply voltage: 5 @ Access-CP Supply voltage: 21 @ EU-LEO min Supply voltage: 52 @ EU-LEO max Supply voltage: 23 @ EU-GEO min Supply voltage: 55 @ EU-GEO max Supply voltage: 23 @ EU-TC min Supply voltage: 55 @ EU-TC max Power consumption: 0.7 W (typical) @ Access-CP (TEC OFF) Power consumption: 7.7 W (typical) @ EU-LEO (TEC OFF) Power consumption: 9.3 W (typical) @ EU-GEO (TEC OFF) Power consumption: 9.3 W (typical) @ EU-TC (TEC OFF) Data interface: SpaceWire @ Access-CP Data interface: MIL-STD-1553B @ EU-LEO Data interface: RS422 @ EU-LEO (AS/CS16) Data interface: MIL-STD-1553B @ EU-GEO Data interface: RS422 @ EU-GEO (AS/CS16) Data interface: MIL-STD-1553B @ EU-TC Data interface: RS422 @ EU-TC (AS/CS16) Update rate: 8 Hz @ Access-CP Update rate: 10 Hz @ Access-CP (variant 2) Update rate: 8 Hz @ EU Update rate: 10 Hz @ EU (variant 2) Update rate: 12 Hz @ EU (variant 3) Update rate: 16 Hz @ EU (variant 4) Update rate: 20 Hz @ EU (variant 5) Update rate: 30 Hz @ EU (variant 6) Envelope (L×W×H): Ø 147 x 283 mm @ Optical Head Envelope (L×W×H): 170 x 146 x 103 mm @ EU-LEO Envelope (L×W×H): 177 x 158 x 109 mm @ EU-GEO Envelope (L×W×H): 194 x 166 x 159 mm @ EU-TC Mass: 1400 g @ Optical Head Mass: 1800 g @ EU-LEO Mass: 2600 g @ EU-GEO Mass: 3900 g @ EU-TC Operating temperature: -30 °C @ min Operating temperature: 60 °C @ max Survival temperature: -40 °C @ min Survival temperature: 70 °C @ max Design lifetime: 10 years @ LEO Design lifetime: 18 years @ GEO Flight heritage: Flight-proven algorithm: more than eight millions hours of successfull operation ## Redwire Coarse Sun Sensor – Pyramid — Redwire Corporation [sun-sensors] https://newspacemarket.com/products/redwire-coarse-sun-sensor-pyramid/ Field of view: 360 Envelope (L×W×H): 2.3″×2.3″ (58×58) MM @ mounting base Envelope (L×W×H): 3.5″×3.5″×1.7″ (89×89×43 MM) @ with baffles Accuracy: 1 ° @ at null (typically) Accuracy: 5 ° @ throughout linear range Mass: 130 g @ nominal Radiation tolerance (TID): 100 krad Flight heritage: MAVEN Flight heritage: SMAP @ (variant 2) Flight heritage: DSCS @ (variant 3) Flight heritage: UARS @ (variant 4) Flight heritage: EUVE @ (variant 5) Flight heritage: GPS IIR @ (variant 6) Flight heritage: GPS IIF @ (variant 7) Flight heritage: LANDSAT @ (variant 8) Flight heritage: MARS SURVEYOR @ (variant 9) Flight heritage: MARS ODYSSEY @ (variant 10) Flight heritage: STARDUST @ (variant 11) Flight heritage: ODIN/CYCLOPS @ (variant 12) Flight heritage: AMOS-1 @ (variant 13) Flight heritage: AMOS-2 @ (variant 14) Flight heritage: SPACEBUS 4000 @ (variant 15) Flight heritage: TDRS @ (variant 16) Flight heritage: GOES @ (variant 17) Flight heritage: CLASSIFIED PROGRAMS @ (variant 18) ## Magmeter-2 — Bartington Instruments [magnetometers] https://newspacemarket.com/products/magmeter-2/ Measurement range: 100 µT @ up to ±100µT Measurement range: 1000 µT @ up to ±1000µT Resolution: 10 nT @ for ranges up to ±100µT Resolution: 100 nT @ for ranges up to ±1000µT Operating temperature: 0 °C (min) Operating temperature: 50 °C (max) Operating temperature: 40 °C (max) @ for charging Survival temperature: 5 °C (min) @ long term Survival temperature: 30 °C (max) @ long term Survival temperature: -10 °C (min) @ short term Survival temperature: 50 °C (max) @ short term Survival temperature: -20 °C (min) @ without batteries Survival temperature: 65 °C (max) @ without batteries Envelope (L×W×H): 106 x 63 x 148mm Mass: 630 g @ battery included Connector: Hirose RM15TRD-10P (mating connector – RM15TPD-10S) @ Sensor connector Connector: 3 off BNC connectors (X, Y and Z) @ Output connectors Connector: 2.1mm socket @ Battery charger inlet Design lifetime: 8 @ Battery life ## 3-Axis Magnetorquer NanoTorque GST-600 — GomSpace [magnetorquers] https://newspacemarket.com/products/gomspace-nanotorque-gst-600-magnetorquer/ Magnetic dipole moment: 0.23 A·m² (min) Magnetic dipole moment: 0.4 A·m² (typical) Power consumption: 0.003 W (typical) Power consumption: 0.5 W Power consumption: 0.625 W (max) Flight heritage: Flight-proven Supply voltage: 3.6 (max) @ Maximum supply voltage and logic voltage for TMP100 temperature sensor Operating temperature: -35 °C (min) Operating temperature: 70 °C (max) Survival temperature: -35 °C (min) Survival temperature: 70 °C (max) Mass: 180 g (typical) Envelope (L×W×H): 90.5 x 96.9 x 17.2 Data interface: I2C @ TMP100 sensor Connector: Molex PicoBlade 53398-0671 @ J1 - Magnetorquer Z-Axis Connector: Molex PicoBlade 53398-0471 @ J2 - Communication Connector: Molex PicoBlade 53398-0471 @ J3 - Communication Connector: Molex PicoLock 503763-0291 @ J4 - Magnetorquer X-Axis Connector: Molex PicoLock 503763-0291 @ J5 - Magnetorquer Y-Axis ## NanoTorque GST-600 — GomSpace [magnetorquers] https://newspacemarket.com/products/gomspace-nanotorque-gst-600-mk2-magnetorquer/ Magnetic dipole moment: 0.4 A·m² Power consumption: 0.5 W Flight heritage: Flight-proven GomSpace product line Envelope (L×W×H): 90.5 x 96.9 x 17.2 mm Mass: 180 g Operating temperature: -35 °C (min) Operating temperature: 70 °C (max) Survival temperature: -35 °C (min) Survival temperature: 70 °C (max) ## Halcyon — Benchmark Space Systems [propulsion] https://newspacemarket.com/products/benchmark-space-systems-halcyon/ Propellant mass: 660 g Propulsion type: chemical Total impulse: 1000 N·s (min) Total impulse: 500000 N·s (max) Propellant: HTP @ catalytic monopropellant Propellant: HTP + FUEL INJECTION @ dual-mode bipropellant Thrust: 250 mN @ catalytic monopropellant Thrust: 1000 mN @ catalytic monopropellant (variant 2) Thrust: 5000 mN @ catalytic monopropellant (variant 3) Thrust: 10000 mN @ catalytic monopropellant (variant 4) Thrust: 2000 mN @ dual-mode bipropellant Thrust: 10000 mN @ dual-mode bipropellant (variant 2) Thrust: 22000 mN @ dual-mode bipropellant (variant 3) Specific impulse: 150 (min) @ catalytic monopropellant Specific impulse: 170 (max) @ catalytic monopropellant Specific impulse: 290 (min) @ dual-mode bipropellant Specific impulse: 310 (max) @ dual-mode bipropellant Min impulse bit: 10 mN·s (max) @ catalytic monopropellant Min impulse bit: 35 mN·s (max) @ dual-mode bipropellant Survival temperature: -30 °C (min) Survival temperature: 60 °C (max) Operating temperature: -5 °C (min) @ propellant on-orbit Operating temperature: 25 °C (max) @ propellant on-orbit Power consumption: 4 W (max) @ idle Power consumption: 15 W (max) @ firing Supply voltage: 12 @ catalytic monopropellant Supply voltage: 24 (min) @ catalytic monopropellant Supply voltage: 32 (max) @ catalytic monopropellant Supply voltage: 24 (min) @ dual-mode bipropellant Supply voltage: 32 (max) @ dual-mode bipropellant Data interface: RS-422 Data interface: RS-485 @ (variant 2) Flight heritage: June 2021 @ catalytic monopropellant ## BHT-100 — Busek Co. [propulsion] https://newspacemarket.com/products/busek-bht-100-hall-effect-thruster/ Design lifetime: 1.1 years (from hour @ Predicted Lifetime Power consumption: 100 W Propulsion type: electric Power at thrust: 100 W @ Discharge Power Mass: 1160 g Supply voltage: 200 (nominal) Envelope (L×W×H): 8 cm Diameter, 5.5 cm Length Thrust: 7 mN Specific impulse: 1000 Total impulse: 45360 N·s @ Demonstrated Impulse Total impulse: 250000 N·s (min) @ Predicted Total Impulse Propellant: Xenon, Iodine ## Warlock — Magdrive [propulsion] https://newspacemarket.com/products/magdrive-warlock/ Thrust: 40000 mN Specific impulse: 5000 Propellant: 2.5 kg Power consumption: 2-100 W Propulsion type: electric Thrust: 100 mN @ nominal Thrust: 50000 mN @ max Specific impulse: 1500 @ nominal Specific impulse: 1500 @ max Total impulse: 3000 N·s (min) @ nominal Total impulse: 50000 N·s (min) @ max Mass: 3000 g @ nominal Mass: 3000 g @ max Envelope (L×W×H): 20x10x10 @ nominal Envelope (L×W×H): 20x10x10 @ max Thrust: 4000 mN @ ECO Thrust: 10000 mN @ SPORT Specific impulse: 4500 @ ECO Specific impulse: 1800 @ SPORT Power at thrust: 150 W @ ECO Power at thrust: 150 W @ SPORT ## 30kN Hybrid Engine — Nammo [propulsion] https://newspacemarket.com/products/30kn-hybrid-engine-3131/ Specific impulse: 270 Propulsion type: hybrid Thrust: 30000000 mN @ in vacuum Total impulse: 1000000 N·s (min) Propellant: 87.5% H2O2, and HTPB Mass: 165000 g @ including fuel cartridge Envelope (L×W×H): 356mm [14 inch] Diameter, 1.7m Length Flight heritage: TRL8, flown on Nucleus Sounding Rocket ## Intelligent Protected Lithium Battery Module with SoC Reporting (BM2) — Pumpkin, Inc. [batteries] https://newspacemarket.com/products/pumpkin-bm2-battery-module/ Cycles / reuses: 500 Connector: 2 x 14-pin Connector: User-provided captive harness (+$1000) @ (variant 2) Capacity: 72 Wh (min) Capacity: 100 Wh (max) Capacity (charge): 3.5 Ah @ standard cell LG INR18650 MJ1 Mass: 700 g (max) Mass: 692 g @ Eight 18650 cells, with optional SUPERNOVA-compatible heatsink / mounting brackets Mass: 710 g (max) @ Eight 18650 cells, with optional SUPERNOVA-compatible heatsink / mounting brackets Mass: 542 g @ Eight 18650 cells, without SUPERNOVA-compatible heatsink / mounting brackets Mass: 560 g (max) @ Eight 18650 cells, without SUPERNOVA-compatible heatsink / mounting brackets Supply voltage: 8.4 (nominal) @ 2S4P configuration Supply voltage: 12.6 (nominal) @ 3S2P configuration Supply voltage: 16.8 (nominal) @ 4S2P configuration Supply voltage: 6 (min) @ 2S4P configuration Supply voltage: 8.4 (max) @ 2S4P configuration Supply voltage: 9 (min) @ 3S2P configuration Supply voltage: 12.6 (max) @ 3S2P configuration Supply voltage: 12 (min) @ 4S2P configuration Supply voltage: 16.8 (max) @ 4S2P configuration Power consumption: 84 W (max) @ peak power Power consumption: 168 W (max) @ peak power (variant 2) Power consumption: 1 W (max) Power consumption: 84 W @ Nominal Power, 2S4P configuration Power consumption: 126 W @ Nominal Power, 3S2P configuration Power consumption: 168 W @ Nominal Power, 4S2P configuration Operating temperature: -40 °C (min) @ Discharge Operating temperature: 75 °C (max) @ Discharge Operating temperature: -40 °C (min) @ Charge Operating temperature: 50 °C (max) @ Charge ## ANT-GPS Series — AAC Clyde Space [antennas] https://newspacemarket.com/products/aac-ant-gps/ Frequency: 1575.42 MHz (nominal) Polarization: RHCP Antenna type: patch Mass: 80 g Envelope (L×W×H): 21.03 mm x 50.8 mm x 50.8 mm Connector: SMA Female Operating temperature: -55-85 °C Flight heritage: 15 years of successful on-orbit flight operations heritage on our AAC SpaceQuest spacecraft as well as being deployed for a global clientele. More than 18 in Operation on Orbit Frequency band: L Gain: -2.3 Supply voltage: 3.3 Radiation tolerance (TID): 10 krad TRL: 9 Survival temperature: -55 °C ## Chameleon SWIR — Dragonfly Aerospace [cameras] https://newspacemarket.com/products/dragonfly-chameleon-swir/ Ground sample distance: 8.7 m @ at 500 km Swath width: 11.2 km @ at 500 km Mass: 1600 g Envelope (L×W×H): 100 x 100 x 215 mm with rear-mounted nCCM Data interface: LVDS Data interface: SpaceWire @ (variant 2) Data interface: SPI @ TMTC Interface Data interface: I2C @ TMTC Interface (variant 2) Data interface: CAN @ TMTC Interface (variant 3) Data interface: RS422 @ TMTC Interface (variant 4) Data interface: RS485 @ TMTC Interface (variant 5) Power consumption: 7 W (max) @ Imaging mode (est) Power consumption: 5 W (max) @ Readout mode Supply voltage: 5 Operating temperature: 10-30 °C Survival temperature: -20-55 °C Spectral bands: 4 TRL: 8 ## IRIS 4Mpx Space Camera System — 3D Plus (HEICO) [cameras] https://newspacemarket.com/products/3d-plus-iris-4mpx-space-camera/ Radiation tolerance (TID): 30 krad @ > Radiation tolerance (TID): 40 krad @ > (variant 2) Radiation tolerance (TID): 40 krad @ > (variant 3) Focal length: 25 Spectral bands: 450 (min) Spectral bands: 700 (max) Mass: 400 g (max) Envelope (L×W×H): 86x72x80 mm³ Supply voltage: 4.5 (min) Supply voltage: 9 (max) Power consumption: 1.5 W @ Average Power Consumption (25°C) Operating temperature: -40 °C (min) Operating temperature: 55 °C (max) Data interface: Space Wire ## piPATCH-S-UL — SkyFox Labs s.r.o. [antennas] https://newspacemarket.com/products/skyfox-labs-pipatch-s-ul/ Export status: controlled @ Dual Use goods, needs special Export License approved by the Ministry of Industry and Trade of t Export status: controlled and needs special Export License approved by the Ministry of Industry and Trade of the Czech Republic (the local control entity), if exported outside EU-member states territory. The request for the Export License has to be submitted by the manu Export status: controlled @ needs special Export License approved by the Ministry of Industry and Trade of the Czech Republi Frequency band: S Antenna type: ZeroCore Patch Antenna Polarization: RHCP @ standard Polarization: linear @ on request Gain: 5.55 @ Circular Mode (RHCP), average band gain, front lobe Frequency: 2025-2110 MHz Power consumption: 10 W @ CW @ 25°C, open space radiation Mass: 60 g @ ± X/Y side mount Mass: 65 g @ ± Z side mount Envelope (L×W×H): 98×82.6×+6/-8 mm @ ± X/Y side mount Envelope (L×W×H): 98×98×+6/-8 mm @ ± Z side mount Operating temperature: -40-85 °C Connector: MCX-F @ standard Connector: SMA-F @ on request Operating temperature: -40-85 °C @ (variant 2) Survival temperature: -55-100 °C ## Redwire FALCCON High Gain Broadband Space Antenna — Redwire Corporation [antennas] https://newspacemarket.com/products/redwire-falccon-antenna/ Frequency band: L Gain: 21 @ high gain Gain: 18.5 @ intermediate gain Envelope (L×W×H): 80 cm x 80 cm x 38 cm @ high gain Envelope (L×W×H): 60 cm x 60 cm x 38 cm @ intermediate gain Mass: 10000 g (max) Connector: PSM Connector: TNC @ (variant 2) Design lifetime: 5 years (min) Design lifetime: 5 years @ gt, Greater than Export status: ECCN 7A104 Design lifetime: 5 years @ gt ## TPOD (Third Planet Orbital Deployer) — Third Planet Orbital [deployers] https://newspacemarket.com/products/third-planet-orbital-tpod-deployer/ model_used: TPOD-12XL Mass: 6750 g (max) Envelope (L×W×H): 226.3±0.1 x 226.3±0.1 x 366±0.3 @ Satellite Size Max payload mass: 27400 g Connector: D-Sub (DE-9) Plug Supply voltage: 18 (min) @ Release Pulse Supply voltage: 36 (max) @ Release Pulse Actuation: pulse @ Release Pulse Export status: ITAR Free @ Componentry... Capacity: 27.4 Separation velocity: 2 m/s ## ISIPOD — Innovative Space Logistics [deployers] https://newspacemarket.com/products/isispace-isipod/ Export status: FAR/ITAR free design @ ISIPOD product line Export status: FAR/ITAR free design @ QUADPACK product line Export status: FAR/ITAR free design @ ISIPOD Export status: FAR/ITAR free design @ QUADPACK Export status: FAR/ITAR free design Export status: FAR/ITAR free design @ (variant 2) Envelope (L×W×H): 1U, 2U, 3U (and combinations) Flight heritage: Since 2013, on PSLV, Antares, Soyuz, Dnepr, LM-2D, Atlas V, LM-11, Vega, Falcon 9 Capacity: 1 @ 1-Unit ISIPOD Capacity: 2 @ 2-Unit ISIPOD Capacity: 3 @ 3-Unit ISIPOD Max payload mass: 2000 g @ 1-Unit ISIPOD Max payload mass: 4000 g @ 2-Unit ISIPOD Max payload mass: 6000 g @ 3-Unit ISIPOD Actuation: other @ redundant deployment signals Mass: 1500 g @ 1-Unit ISIPOD Mass: 1750 g @ 2-Unit ISIPOD Mass: 2000 g @ 3-Unit ISIPOD Flight heritage: since 2013 Vega @ 1-Unit ISIPOD Flight heritage: since 2015 PSLV @ 2-Unit ISIPOD Flight heritage: since 2013 PSLV, Antares, Soyuz, Dnepr, LM-2D, Atlas V @ 3-Unit ISIPOD ## Constellation On Board Computer (cOBC) — Beyond Gravity (ex-RUAG Space) [obc-computers] https://newspacemarket.com/products/beyond-gravity-cobc-constellation-on-board-computer/ Processor: e500Core CPU clock: 800 MHz RAM: 1024 MB Storage: 2.7 GB Operating system: VxWorks Operating system: RTEMS @ (variant 2) Operating system: Linux @ (variant 3) Mass: 5400 g Envelope (L×W×H): 300 x 119 x 239 mm³ @ excluding feet Power consumption: 26 W @ nominal Data interface: RS-422 @ TM Encoder Data interface: RS-422 @ TC Decoder Data interface: Ethernet Data interface: SpaceWire @ (variant 2) Data interface: CAN @ (variant 3) Data interface: RS-422 @ (variant 4) Data interface: RS-485 @ (variant 5) Data interface: UART @ (variant 6) Data interface: other @ GPIO Data interface: other @ Sync Pulse output Data interface: other @ Separation strap inputs Data interface: other @ External alarm inputs Data interface: other @ External Cryptographic Unit Operating temperature: -20-60 °C Design lifetime: 10 years Design lifetime: 10 years @ LEO Design lifetime: 10 years @ LEO, MEO and GEO Random vibration: 15 ## U7790 – High-Performance Satellite MESH Modem — SpaceBridge Inc. [sdr-modems] https://newspacemarket.com/products/u7790/ Protocols / waveforms: DVB-S2/S2X ACM @ forward link Protocols / waveforms: MF-TDMA and WaveSwitch @ return link Modulation: QPSK to 256APSK @ forward link Modulation: SS-BPSK, QPSK, 8PSK, 16QAM, 32QAM, 64QAM @ return link Frequency: 950-2150 MHz @ RX L-band Frequency: 950-2400 MHz @ TX L-band TX power: 0-0.001 W Data rate: 100000 kbps @ download Data rate: 25000 kbps @ upload Data interface: Ethernet @ U7790-60/SA/ODU, user Data interface: Ethernet @ U7790-60/SA/ODU, management Data interface: Ethernet @ U7790-120, user Data interface: Ethernet @ U7790-120, management Envelope (L×W×H): 482.6 x 153.4 x 44.4 mm @ U7790-60 Mass: 3400 g (max) Power consumption: 60 W @ U7790-60, AC PS Power consumption: 40 W @ U7790-60, to power RF/BUC Power consumption: 120 W @ U7790-120, AC PS Power consumption: 100 W @ U7790-120, to power RF/BUC Supply voltage: 90-260 Operating temperature: 0-50 °C Survival temperature: -40-85 °C Export status: export controlled @ encryption up to AES256 ## pqADSB-NG — SkyFox Labs s.r.o. [antennas] https://newspacemarket.com/products/skyfox-labs-pqadsb-ng/ Frequency: 1090 MHz @ L-band Frequency band: L Frequency: 1090 MHz @ L-band (variant 2) Frequency band: L @ (variant 2) Polarization: RHCP Antenna type: Patch Antenna system Antenna type: RHCP ceramic patch antenna @ (variant 2) Mass: 55 g Envelope (L×W×H): 50×50×12.5 mm Power consumption: 0.26 W @ typical Power consumption: 0.26 W @ typical (variant 2) Data interface: UART Data interface: UART @ (variant 2) Connector: PicoBlade™ 6P connector Connector: MOLEX 6 pin connector @ (variant 2) Export status: regulated (Dual Use) goods, the export is controlled and needs special Export License approved by the Ministry of Industry and Trade of the Czech Republic (the local control entity). Operating temperature: -40-85 °C Export status: controlled @ regulated (Dual Use) goods, the export is controlled and needs special Export License approved b ## Oxford Space Systems Deployable Helical Antenna for IoT applications — Oxford Space Systems [antennas] https://newspacemarket.com/products/oxford-space-systems-deployable-helical-antenna-for-iot-applications/ Export status: ITAR-free Antenna type: helical Flight heritage: Flight heritage Frequency band: VHF Frequency band: S @ (variant 2) ## SpaceCam 5MP — Voyager Technologies [cameras] https://newspacemarket.com/products/spacecam-5mp/ Sensor resolution: 2560 (H) x 2160 (V) Supply voltage: 5 (nominal) Supply voltage: 28 (nominal) @ optional Data interface: SpaceWire @ at 80 Mbps Data interface: other @ CameraLink Operating temperature: -20 °C (min) @ Operational Operating temperature: 50 °C (max) @ Operational Survival temperature: -30 °C (min) @ Non-operational Survival temperature: 85 °C (max) @ Non-operational Design lifetime: 15 years (max) @ LEO and GEO Envelope (L×W×H): 10.7 cm L x 8.4 cm W x 23.8 cm H @ with baffle Mass: 1000 g (min) @ Dependent on optic configuration Mass: 2500 g (max) @ Dependent on optic configuration Power consumption: 6.5 W @ nominal Power consumption: 7.5 W @ maximum Radiation tolerance (TID): 100 krad Design lifetime: 15 years @ up to, LEO and GEO ## Redwire SpectraCAM High Resolution Flight Camera — Redwire Corporation [cameras] https://newspacemarket.com/products/redwire-spectracam-flight-camera/ Export status: controlled @ High Resolution Space Cameras are export controlled through an ECCN (Export Control Classificati Envelope (L×W×H): 50 x 50 x 47 mm Export status: export controlled through an ECCN (Export Control Classification Number) issued by the United States Department of Commerce. Export shipment requires successful application for an export license (under ECCN7A004 for Redwire SpectraCAM Flight Cameras). Mass: 180 g (max) @ without optics Supply voltage: 5 @ nominal Sensor resolution: 5 @ monochrome Operating temperature: -30 °C (min) Operating temperature: 55 °C (max) ## Owl 640 T — Raptor Photonics [cameras] https://newspacemarket.com/products/raptor-photonics-owl-640-t/ Export status: This product is under the export control of the UK goverment and may be subject to a single individual export license before shipment. Sensor resolution: 640 x 512 Spectral bands: VIS-SWIR (0.6μm to 1.7μm) Sensor resolution: 640 x 512 @ (variant 2) Data interface: other @ 12 bit Camera Link (Base Configuration / SDR) Power consumption: 4 W @ with TEC ON, NUC ON Envelope (L×W×H): 68mm x 50.00mm x 50.00mm @ excluding standard mounting Mass: 245 g Supply voltage: 12 (nominal) Connector: C Mount @ Optical Interface ## GPS-110 — Berlin Space Technologies [gnss-receivers] https://newspacemarket.com/products/gps-110-gnss-receiver/ Export status: ITAR free @ EU dual use Design lifetime: 5 years Flight heritage: since 2023 Supply voltage: 12 Power consumption: 0.3 W @ both GPS receivers switched off Power consumption: 3 W @ both GPS receivers switched on Position accuracy: 10 m (max) Velocity accuracy: 0.1 m/s Time to first fix (cold): 40 s @ cold start Constellations: GPS only, Galileo and others on demand Data interface: RS-422 Mass: 285 g Envelope (L×W×H): 91 x 84 x 41 mm Operating temperature: -40-85 °C Export status: EU dual use, ITAR free ## Control Moment Gyroscopes (CMG 15-45S / 40-60S / 75-75S) — Airbus Defence and Space [imus-gyros] https://newspacemarket.com/products/airbus-cmg-15-45/ Design lifetime: 10 years Flight heritage: Airbus CMG products have cumulated over 1 millon hours on orbit, without failure Mass: 69000 g @ total Mass: 61000 g @ mechanism Mass: 8000 g @ electronics channel Envelope (L×W×H): mechanism 550mm x 500mm x 570mm @ mechanism Envelope (L×W×H): electronics 390mm x 250mm x 175mm (per box for 2 CMG channels) @ electronics Power consumption: 57 W @ quasi-static, @75Nms per CMG Power consumption: 145 W @ max maneuver per CMG Radiation tolerance (TID): compatible with typical 10 years LEO @ total dose Data interface: MIL 1553 data bus interface Design lifetime: 10 years @ LEO Operating temperature: -20 °C Survival temperature: -30 °C Envelope (L×W×H): mechanism 550 mm x 500 mm x 570 mm, electronics 390 mm x 250 mm x 175 mm ## NanoTorque GSW-600 — GomSpace [reaction-wheels] https://newspacemarket.com/products/gomspace-nanotorque-gsw-600/ Design lifetime: 3 years @ design lifetime Max torque: 2 mN·m Angular momentum storage: 0.019 N·m·s @ storage Bearing type: hybrid Data interface: SPI Data interface: I2C @ (variant 2) Connector: Molex PicoBlade right angle, 053261-1371 Angular momentum storage: 0.019 N·m·s @ At max speed Data interface: SPI @ SPI speed Data interface: I2C @ I2C speed Mass: 180 g Envelope (L×W×H): 44.0 x 44.0 x 27.0 mm Dynamic imbalance: 300 @ Flywheel inertia Design lifetime: 3 years @ design, in-orbit operations Design lifetime: 3 years @ in-orbit operations Wheel speed: 6000 ## Sodern Auriga CP — Sodern [star-trackers] https://newspacemarket.com/products/sodern-auriga-cp/ Design lifetime: 10 years @ LEO Design lifetime: 15 years @ GEO with EOR Design lifetime: 10 years @ LEO 400-1200km Design lifetime: 15 years @ GEO with EOR (variant 2) Design lifetime: 10 years @ LEO and 15 years in GEO orbit with EOR Envelope (L×W×H): 66 x 56 x 94 mm (height) Envelope (L×W×H): No Electronic Unit, centralized software @ (variant 2) Field of view: 9 Update rate: 10 Hz Mass: 225 g @ OH, including baffle Design lifetime: 10 years @ in LEO 400-1200km Design lifetime: 15 years @ in GEO with EOR Power consumption: 0.8 W @ OH, typ Power consumption: 1.1 W @ OH, max Lost-in-space acquisition time: 3.8 s @ lost-in-space, typ Max tracking slew rate: 0.3 @ Acquisition, baseline Max tracking slew rate: 2 (max) @ Acquisition Max tracking slew rate: 3 (max) @ Tracking Sun exclusion angle: 35 ## ABSL CM520 8s9p Li-ion Space Battery (28 V, 18 Ah) — EnerSys / ABSL Space Products [batteries] https://newspacemarket.com/products/absl-cm520-8s9p-space-battery/ Cell chemistry: Li-ion Supply voltage: 28 (nominal) Supply voltage: 33.6 (max) Supply voltage: 24 (min) Capacity (charge): 18 Ah Capacity: 532.8 Wh Envelope (L×W×H): 209 x 190 mm (Footprint) Envelope (L×W×H): 117 mm (Height) @ (variant 2) Mass: 4300 g Flight heritage: variety of missions in a variety of ESA LEO missions, lunar landers and launch vehicles Flight heritage: over 5.5 billion cell hours of in-orbit heritage using ABSL™ Li-ion cell technology @ (variant 2) Connector: single keyed circular or D-type connector Operating temperature: 0 °C (min) @ Thermal chamber only Operating temperature: 40 °C (max) @ Thermal chamber only Survival temperature: -20 °C (min) @ Cell Level Qual only Survival temperature: 60 °C (max) @ Cell Level Qual only Radiation tolerance (TID): 10000 krad @ cell level ## Q8J Computer-on-Module — Xiphos Technologies [sdr-modems] https://newspacemarket.com/products/xiphos-q8j/ Envelope (L×W×H): 80 mm x 80 mm x 11.2 mm Power consumption: 5 W @ as little as Data interface: Ethernet @ Gigabit Ethernet networking through its RJ45 connector Connector: RJ45 Data interface: USB @ USB 2.0/USB 3.1 Gen 1 Host port Data interface: RS-232 @ factory-selectable RS-232/422/485 Data interface: RS-422 @ factory-selectable RS-232/422/485 (variant 2) Data interface: RS-485 @ factory-selectable RS-232/422/485 (variant 3) Data interface: CAN @ PIM Data interface: RS-232 @ PIM (variant 2) Data interface: RS-422 @ PIM (variant 3) Data interface: RS-485 @ PIM (variant 4) Power consumption: 5 W @ typical Supply voltage: 9 Envelope (L×W×H): 80 mm x 80 mm x 11.2 mm @ (variant 2) Mass: 56 g @ without connectors Data interface: Ethernet @ Gigabit Ethernet (RJ45 on adapter) Data interface: USB @ USB Type-C Host port (USB 2.0 & USB 3.1 Gen 1) Data interface: CAN @ CAN Bus & PCIe controllers (in logic) Data interface: RS-232 @ factory selectable RS-232/422/485 (Mezzanine connector) Data interface: RS-422 @ factory selectable RS-232/422/485 (Mezzanine connector) (variant 2) Data interface: RS-485 @ factory selectable RS-232/422/485 (Mezzanine connector) (variant 3) Flight heritage: The Q8JS, the Flight Model (FM) version of the Q8J, has been flying since September 2023 Data interface: Gigabit Ethernet networking through its RJ45 connector Data interface: USB 2.0/USB 3.1 Gen 1 Host port @ (variant 2) Data interface: Gigabit Ethernet (RJ45 on adapter) @ (variant 3) Data interface: USB Type-C Host port (USB 2.0 & USB 3.1 Gen 1) @ (variant 4) Data interface: CAN Bus & PCIe controllers (in logic) @ (variant 5) Radiation tolerance (TID): 30 krad ## SRS-4 — Satlab A/S [radios] https://newspacemarket.com/products/satlab-srs-4/ Data interface: CAN-bus bitrate Up to 1 Mbit/s Data interface: RS-422 bitrate Up to 12.5 Mbit/s, full-duplex @ (variant 2) Data interface: Ethernet bitrate 100 Mbit/s, full-duplex @ (variant 3) Flight heritage: since 2021 TRL: 9 Frequency band: S Frequency: 2200-2290 MHz @ Transmit Frequency: 2025-2110 MHz @ Receive TX power: 0.1-1.995 W RX sensitivity: -122 @ <1 % PER, 100 kBd BPSK Modulation: BPSK/QPSK/8PSK @ Transmit Modulation: BPSK/QPSK @ Receive Mass: 253 g Envelope (L×W×H): 93.0 mm × 87.2 mm × 18.0 mm Supply voltage: 5.1-28.8 Power consumption: 1.5 W @ RX (5 MBd), 6 V input, 20 °C Power consumption: 10.8 W @ TX (5 MBd, 33 dBm output), 6 V input, 20 °C Data interface: CAN @ CAN-bus bitrate Up to 1 Mbit/s Data interface: RS-422 @ RS-422 bitrate Up to 12.5 Mbit/s, full-duplex Data interface: Ethernet @ Ethernet bitrate 100 Mbit/s, full-duplex Operating temperature: -40-85 °C @ Operating temperature RX Operating temperature: -40-70 °C @ Operating temperature TX Survival temperature: -40-85 °C @ Storage Power consumption: 1.5 W @ Input power (Idle) Power consumption: 1.5 W @ Input power (RX) Power consumption: 10.8 W @ Input power (TX, 33 dBm output power) Power consumption: 10.8 W @ Input power (RX+TX, 33 dBm output power) Power consumption: 0.16 W @ Additional input power for Ethernet enabled Power consumption: 0.06 W @ Additional input power for RS-422 enabled ## NanoCom AX100 — GomSpace [radios] https://newspacemarket.com/products/nanocom-ax100/ Frequency: 430-440 MHz Frequency band: UHF @ AX100U Frequency band: UHF @ AX100UL Frequency band: VHF @ AX100V Modulation: GFSK/GMSK TX power: 0.251-1 W @ adjustable output power TX power: 0.794-1.259 W @ at RF connector Data rate: 0.1-38.4 kbps Data rate: 0.5-19.2 kbps @ TX, within 25 kHz BW Data rate: 0.5-38.4 kbps @ TX, capable Data rate: 0.1-38.4 kbps @ RX RX sensitivity: -137 @ at 100 bps with FEC RX sensitivity: -132 @ 600 baud w/ FEC RX sensitivity: -122 @ 5000 baud w/ FEC RX sensitivity: -111 @ 50000 baud w/ FEC Mass: 24.5 g Envelope (L×W×H): 65 mm x 40 mm x 6.5 mm Supply voltage: 3.3-3.4 Supply voltage: 3.3 @ typ. Power consumption: 0.1815 W @ RX (typ. 55mA at 3.3V) Power consumption: 0.396 W @ RX (max. 120mA at 3.3V) Power consumption: 2.475 W @ TX, max PCL, nominal temperature +25C (typ. 750mA at 3.3V) Power consumption: 2.64 W @ TX, max PCL, nominal temperature +25C (typ. 800mA at 3.3V) Power consumption: 2.805 W @ TX, max PCL, nominal temperature +25C (max. 850mA at 3.3V) Power consumption: 1.98 W @ TX, max PCL, extreme temperature -30C to +85C (min. 600mA at 3.3V) Power consumption: 3.3 W @ TX, max PCL, extreme temperature -30C to +85C (max. 1000mA at 3.3V) Data interface: I2C Data interface: UART @ (variant 2) Data interface: CAN @ (variant 3) Connector: 20-position hard-gold plated FSI one-piece connector Connector: MCX antenna connector @ (variant 2) Connector: Picoblade Connector (JTAG) @ (variant 3) Connector: Picoblade USART (debug) Connector @ (variant 4) Operating temperature: -30-85 °C Operating temperature: -30-85 °C @ (variant 2) Survival temperature: -30-85 °C Flight heritage: The AX100 has flown on several satellites and performed perfectly. ## PULSAR-SANT — AAC Clyde Space [antennas] https://newspacemarket.com/products/aac-pulsar-sant/ Design lifetime: 2 years @ >, LEO Frequency band: S Gain: 7 (min) Gain: 7 Beamwidth: 60 Beamwidth: 60 @ (variant 2) Polarization: circular @ Left or right hand Antenna type: patch Mass: 50 g (max) Connector: SMA female Design lifetime: 2 years (min) @ in LEO Flight heritage: UKube-1 mission Operating temperature: -40-85 °C ## piPATCH-S-DL — SkyFox Labs s.r.o. [antennas] https://newspacemarket.com/products/skyfox-labs-pipatch-s-dl/ Frequency band: S Antenna type: patch Polarization: RHCP Gain: 5.55 @ RHCP Polarization: linear @ on request Mass: 60 g @ X/Y side mount Mass: 65 g @ Z side mount Envelope (L×W×H): 98x82.6x+6/-8 mm @ X/Y side mount Envelope (L×W×H): 98x98x+6/-8 mm @ Z side mount Connector: MCX-F @ standard Connector: SMA-F @ on request Power consumption: 10 W @ CW continuous wave Export status: Since the country of origin of this product (the Czech Republic) is a valid participating member of the Wassennaar Agreement ( http://www.wassenaar.org ) and agrees with the Missile Technology Control Regime ( http://www.mtcr.info ) and the piPATCH-S-DL/F Operating temperature: -40-85 °C ## Oxford Space Systems Deployable Yagi Antenna for AIS and VDES applications — Oxford Space Systems [antennas] https://newspacemarket.com/products/oxford-space-systems-deployable-yagi-antenna-for-ais-and-vdes-applications/ Export status: ITAR-free Antenna type: Yagi Flight heritage: Yes (3-element configuration) ## Multiband GNSS Module with Antenna M-GNSSB-ANT-RX — Arralis [antennas] https://newspacemarket.com/products/arralis-m-gnssb-ant-rx-multiband-gnss-module-with-antenna/ Gain: 2-3 Frequency band: L Frequency band: S @ (variant 2) Supply voltage: 3.3 Supply voltage: 3.3 (nominal) Supply voltage: 5 @ RS485 option Envelope (L×W×H): 58mm x 58mm Connector: SMA connector - DC - 18GHz Data interface: RS-485 Data interface: UART @ (variant 2) ## K-Band Flat Panel Passive Antenna PAN-8498-64-K — ReliaSat [antennas] https://newspacemarket.com/products/arralis-pan-8498-64-k-k-band-flat-panel-antenna/ Gain: 20 (min) Power consumption: 5 W Frequency band: Ku Frequency: 17000 MHz Frequency: 21000 MHz (max) Beamwidth: 9 Beamwidth: 11 (max) Polarization: LHCP Polarization: RHCP @ (variant 2) Antenna type: Flat Panel Array Mass: 50 g (max) Envelope (L×W×H): 84 x 98 mm Connector: K (rear mounted) ## S-Band Flat Panel Antenna PAN-185185-4-S — ReliaSat [antennas] https://newspacemarket.com/products/arralis-pan-185185-4-s-s-band-flat-panel-antenna/ Frequency band: S Frequency: 1950000-2250000 MHz Beamwidth: 35-40 Polarization: RHCP Polarization: LHCP @ (variant 2) Antenna type: Flat Panel Array Antenna Envelope (L×W×H): 190 x 190 x 12 mm Connector: SMA Gain: 10 (min) ## ThinAir Commercial IFC Antennas — ThinKom Solutions, Inc. [antennas] https://newspacemarket.com/products/thinkom-thinair-nexus/ Antenna type: High-torque brushless DC motors Frequency band: Ka Beamwidth: 1.8 @ Tx Beamwidth: 2.4 @ Rx Polarization: circular @ switchable (co/orthogonal) Polarization: dual @ simultaneous dual-pol mode Mass: 63500 g Envelope (L×W×H): 1.0m x 0.8m x 0.1m Power consumption: 228 W @ Average Power ## IAA.01 Iridium Automotive Magnetic Mount Antenna — Taoglas [antennas] https://newspacemarket.com/products/taoglas-iaa01-iridium-magnetic-mount-antenna/ Frequency: 1616-1626.5 MHz Gain: 3.7 @ With Ground plane(30x30cm) Polarization: RHCP Antenna type: magnetic mount antenna Envelope (L×W×H): 40.5 x 38 x 12.3mm Connector: SMA Male Straight Operating temperature: -40-85 °C Survival temperature: -40-85 °C Mass: 43.5 g ## Small Antenna Module (SAM) — Spacemanic s.r.o. [antennas] https://newspacemarket.com/products/spacemanic-sam-antenna/ Lead time: 12 Antenna type: dipole Antenna type: cross dipole (turnstile) @ (variant 2) Antenna type: V-dipole @ (variant 3) Flight heritage: Flight heritage on multiple missions (e.g. LASARsat, CroCube, GRBBeta and external customers). Operating temperature: -40-85 °C Envelope (L×W×H): 98 x 98 x 6.2 Envelope (L×W×H): 98 x 98 x 10,1 (incl. components) @ (variant 2) Supply voltage: 5 (nominal) Mass: 55 g (nominal) Power consumption: 0.075 W @ average Power consumption: 1.5 W @ deployment mode (peak) Frequency band: VHF Frequency: 133-150 MHz Frequency band: UHF @ (variant 2) Frequency: 380-450 MHz @ (variant 2) Gain: 2.3 @ VHF dipole antenna Gain: 2.6 @ UHF dipole antenna Gain: 2.6 @ UHF turnstile antenna Data interface: I2C Data interface: RS-485 @ (variant 2) Connector: Molex PicoBlade 53261-0971 Data interface: UART @ (variant 3) Connector: Molex PicoLock 503763-0691 @ (variant 2) Connector: Molex MMCX 73415-1000 @ (variant 3) ## SBAF120UL3 1.2m Lower Ku-Band Tx/Rx SFL Class I Antenna System — SpaceBridge Inc. [antennas] https://newspacemarket.com/products/sbaf120ul3-1-2m-lower-ku-band-tx-rx-sfl-class-i-antenna-system/ Antenna type: offset feed prime focus Mass: 16000 g @ excluding mast Frequency band: Ku Polarization: linear @ orthogonal (co-pol optional) Connector: WR75 @ Tx Connector: WR75 @ Rx Operating temperature: -50 °C Gain: 42.2 Gain: 41.1 @ (variant 2) ## 1.2 Meter Auto Flyaway Antenna (FA120-AK) — ALL-SEEING TECHNOLOGY CO., LTD [antennas] https://newspacemarket.com/products/ast-fa120-ak-flyaway-antenna/ Frequency band: C Frequency band: X @ (variant 2) Frequency band: Ku @ (variant 3) Frequency band: Ka @ (variant 4) Antenna type: Offset antenna Mass: 24000 g Operating temperature: -15 °C (min) Operating temperature: 60 °C (max) Polarization: 35 (min) ## 1.2 Meter Motorized Vehicle Mount Antenna (PS120) — ALL-SEEING TECHNOLOGY CO., LTD [antennas] https://newspacemarket.com/products/ast-ps120-vehicle-mount-antenna/ Antenna type: Single Offset Frequency band: Ku Frequency: 13750 MHz (min) @ Tx Frequency: 14500 MHz (max) @ Tx Frequency: 10700 MHz (min) @ Rx Frequency: 12750 MHz (max) @ Rx Gain: 43.4 @ Tx Gain: 41.7 @ Rx Polarization: linear Mass: 85000 g (max) @ BUC and packages have not included Envelope (L×W×H): 1755mm×1250mm×420mm (L×W×H) Supply voltage: 100 (min) @ AC Supply voltage: 240 (max) @ AC Power consumption: 350 W (max) @ System consumption (BUC not include) Operating temperature: -40 °C (min) Operating temperature: 60 °C (max) Survival temperature: -50 °C (min) Survival temperature: 70 °C (max) ## AstroMesh Unfurlable Mesh Antenna Reflector — Northrop Grumman Space Systems [antennas] https://newspacemarket.com/products/ngc-astromesh-reflector/ Antenna type: Unfurlable Mesh Antenna Reflector Frequency band: UHF Frequency band: Ka @ (variant 2) Flight heritage: >150 years collective on-orbit success, 11+ successful deployments ## Blade Antennas — Haigh Farr [antennas] https://newspacemarket.com/products/haigh-farr-blade-antenna/ Antenna type: Blade Frequency band: UHF Frequency band: C @ (variant 2) Power consumption: 25 W (min) @ CW, standard, with sufficient airflow Power consumption: 30 W (max) @ CW, standard, with sufficient airflow Power consumption: 80 W @ CW, high powered Frequency: 380 MHz (min) Frequency: 470 MHz (max) Operating temperature: -50 °C (min) Operating temperature: -123.1 °C (max) Survival temperature: 26.9 °C (max) @ transient Polarization: linear @ predominately vertical Connector: SMA Standard Connector: TNC Optional (50 Ω) @ (variant 2) Flight heritage: Over 30 years in airborne applications ## Wraparound™ Antennas — Haigh Farr [antennas] https://newspacemarket.com/products/haigh-farr-omnislot-antenna/ Flight heritage: Flown on all types of vehicles from subsurface sea to space, including high Mach kinetic kill weapons, high G projectiles Frequency: 300 MHz (min) Frequency: 13000 MHz (max) Power consumption: 40 W @ cw Connector: SMA standard Antenna type: omnidirectional ## RF Antennas (LYRA range) — NewSpace Systems (NSS) [antennas] https://newspacemarket.com/products/nss-lyra-rf-antennas/ Beamwidth: 70 Beamwidth: 80 @ (variant 2) Beamwidth: 18 @ (variant 3) Beamwidth: 10 @ (variant 4) Frequency: 1575.42 MHz Gain: 16 @ @ Zenith Polarization: RHCP Envelope (L×W×H): 54 mm x 54 mm x 14.1 mm Connector: 50 Ω SMA female ## UHF Deployable Monopole Antenna — Plan-S (Connecta) [antennas] https://newspacemarket.com/products/uhf-deployable-monopole-antenna-4217/ Frequency band: UHF Frequency: 400-403 MHz Gain: 0 Polarization: linear Antenna type: Deployable Monopole Envelope (L×W×H): 22x150x25 mm (Stowed Length) Envelope (L×W×H): 22x330x25 mm (Deployable Length) @ (variant 2) Supply voltage: 5 Connector: 1x SMA Female Flight heritage: Flight heritage demonstrated on 1 Satellite Operating temperature: -40 °C ## Connecta IoT Module and Dual-Band Antenna — Plan-S (Connecta) [antennas] https://newspacemarket.com/products/connecta-iot-module-and-dual-band-antenna-4217/ Envelope (L×W×H): 17 x 17.5 x 2.15 mm (max) Operating temperature: -30 °C (min) Operating temperature: 85 °C (max) Data interface: UART Data interface: other @ (variant 2) Gain: 3.3 Antenna type: UFL coaxial cable or SMA connector Mass: 25 g (max) Envelope (L×W×H): 80 × 80 × 13.65 mm @ (variant 2) ## S-Band Launcher Antenna — Anywaves [antennas] https://newspacemarket.com/products/s-band-launcher-antenna/ Frequency band: S Antenna type: patch Frequency: 2025 MHz (min) Frequency: 2120 MHz (max) Gain: 5 (min) Gain: 10 (max) Polarization: circular Beamwidth: 30 (min) Beamwidth: 80 (max) Mass: 60 g Envelope (L×W×H): 90 x 90 x 20 mm TRL: 8 Connector: Antenna: 136 g ± 3 g Flat mechanical bracket: 166 g Thermal shield: 60 g ## PULSAR-XANT-PLUS — AAC Clyde Space [antennas] https://newspacemarket.com/products/aac-pulsar-xant/ Power consumption: 2 W Power consumption: 5 W @ (variant 2) Frequency band: X Frequency: 8.025 GHz – 8.45 GHz Gain: 11.5 dBi ± 0.5 dB Polarization: LHCP / RHCP Antenna type: patch Mass: 29 g (max) Envelope (L×W×H): 58 mm x 58 mm x 4.7 mm Connector: Straight SMP Operating temperature: -40°C to +85°C Design lifetime: 2 years @ in LEO ## ANT-100 — AAC Clyde Space [antennas] https://newspacemarket.com/products/aac-ant-100/ TRL: 9 Antenna type: static whip antenna Frequency band: VHF Frequency band: UHF @ (variant 2) Mass: 10 g (min) Mass: 100 g (max) Envelope (L×W×H): 5” - 20” (Frequency Dependent) Operating temperature: -40 °C (min) Operating temperature: 80 °C (max) Survival temperature: -50 °C (min) Survival temperature: 100 °C (max) Flight heritage: 15 years of successful on-orbit flight operations heritage Connector: SMA RF Output ## SBMP090 0.9m Manpack — SpaceBridge Inc. [antennas] https://newspacemarket.com/products/sbmp090-manpack/ Frequency band: X @ SBMP090X Frequency band: Ku @ SBMP090UL Frequency band: Ka @ SBMP090A Frequency: 7900-8400 MHz @ Tx Freq. (SBMP090X) Frequency: 7250-7750 MHz @ Rx Freq. (SBMP090X) Frequency: 12750-13250 MHz @ Tx Freq. (SBMP090UL) Frequency: 10700-11700 MHz @ Rx Freq. (SBMP090UL) Frequency: 13750-14500 MHz @ Tx Freq. (SBMP090UX) Frequency: 10700-12750 MHz @ Rx Freq. (SBMP090UX) Frequency: 27500-31000 MHz @ Tx Freq. (SBMP090A) Frequency: 18300-20200 MHz @ Rx Freq. (SBMP090A) Polarization: Circular @ SBMP090X Polarization: Linear @ SBMP090UL Polarization: Linear @ SBMP090UX Polarization: Circular @ SBMP090A Gain: 35.5 (min) @ Tx Gain mid-band (SBMP090X) Gain: 35.1 (min) @ Rx Gain mid-band (SBMP090X) Gain: 39.3 (min) @ Tx Gain mid-band (SBMP090UL) Gain: 38.5 (min) @ Rx Gain mid-band (SBMP090UL) Gain: 40 (min) @ Tx Gain mid-band (SBMP090UX) Gain: 38.9 (min) @ Rx Gain mid-band (SBMP090UX) Gain: 47.6 (min) @ Tx Gain mid-band (SBMP090A) Gain: 44.3 (min) @ Rx Gain mid-band (SBMP090A) Antenna type: Ring focus Mass: 13000 g @ without packing Mass: 17000 g @ with 1 backpack Operating temperature: -40-60 °C Survival temperature: -50-70 °C Envelope (L×W×H): 0.9 m ## Zenith — Spacemanic s.r.o. [antennas] https://newspacemarket.com/products/spacemanic-zenith-gnss-patch-antenna/ Flight heritage: Yes Operating temperature: -40-85 °C Envelope (L×W×H): 50 x 50 x 10 mm Mass: 20 g @ ~ Supply voltage: 3.3-5 Power consumption: 0.024 W @ average Frequency: 1550-1620 MHz Frequency band: L Gain: 4 @ ~, Patch antenna peak Polarization: RHCP Antenna type: patch Operating temperature: -40-105 °C @ Absolute maximum Survival temperature: -40-150 °C Connector: MMCX Molex 73415-1471 @ On module opt.1 Connector: Pigtail RG-178 with MMCX Molex 73415-0950 or MMCX Molex 73415-0972 @ On module opt.2 ## ST 6000 — Orbcomm [antennas] https://newspacemarket.com/products/orbcomm-skywave-st-6000/ Operating temperature: -40 °C Antenna type: integrated antennas Envelope (L×W×H): 6.9 x 10.1 x 2.1 cm ## Global Aero Terminal-5510 (GAT-5510) — Viasat, Inc. [antennas] https://newspacemarket.com/products/global-aero-terminal-5510-gat-5510-3363/ Power consumption: 420 W Antenna type: Tail or fuselage mount, parabolic reflector Ka-band TX/RX airborne antenna Antenna type: Parabolic reflector @ (variant 2) Frequency band: Ka Frequency: 27500000-31000000 MHz @ TX Frequency: 17700000-21200000 MHz @ RX Polarization: circular Polarization: electronically switchable, all combinations of R, L, co-pol, or cross-pol @ (variant 2) Envelope (L×W×H): Ø 31.7 x 33.3 cm @ Swept Volume (D x H) Mass: 11900 g Operating temperature: -55-70 °C ## GAT-5518 terminal — Viasat, Inc. [antennas] https://newspacemarket.com/products/gat-5518-terminal-3363/ Antenna type: Tail or fuselage mount, parabolic reflector Ka-band Tx/Rx airborne antenna Polarization: circular @ electronically switchable, all combinations of R, L, co-pol, or cross-pol Frequency band: Ka Frequency: 27500 MHz (min) @ Tx Frequency: 31000 MHz (max) @ Tx Frequency: 17700 MHz (min) @ Rx Frequency: 21200 MHz (max) @ Rx Beamwidth: 0 (min) @ Elevation coverage Beamwidth: 90 (max) @ Elevation coverage Beamwidth: 0 (min) @ Azimuth coverage Beamwidth: 360 (max) @ Azimuth coverage continuous Envelope (L×W×H): Ø49.8 x 49.8 cm @ Swept Volume (DxH) Mass: 15900 g Operating temperature: -55 °C (min) Operating temperature: 70 °C (max) Power consumption: 420 W ## Miniature Flex-coils — Minco Products, Inc [antennas] https://newspacemarket.com/products/miniature-flex-coils/ Envelope (L×W×H): 4.50" (114 mm) Envelope (L×W×H): 4.50" (114) max @ (variant 2) Envelope (L×W×H): 5.0" (127 mm) @ (variant 3) Operating temperature: -200-100 °C Operating temperature: -200-150 °C @ (variant 2) Antenna type: Telemetry coils with integrated flex circuits @ most laminated coils fabricated with wire insulated with solderable material Flight heritage: Qualified for medical, MIL, aerospace use @ most laminated coils fabricated with wire insulated with solderable material Antenna type: Telemetry coils with integrated flex circuits @ coils wound with polyimide insulated wire ## ANT61 Beacon S — ANT61 [batteries] https://newspacemarket.com/products/ant61-beacon-s/ Lead time: 12 Design lifetime: 6 years @ LEO Mass: 375 g Envelope (L×W×H): 95.9 (max) @ length Envelope (L×W×H): 90.2 (max) @ width Envelope (L×W×H): 25 (max) @ height Supply voltage: 3.5 (min) Supply voltage: 36 (max) Operating temperature: -40 °C (min) Operating temperature: 70 °C (max) Design lifetime: 6 years Power consumption: 4.2 W (min) @ Charging power consumption Power consumption: 5 W (max) @ Charging power consumption Data interface: RS-422 @ USART Data interface: RS-485 @ USART (variant 2) Data interface: CAN @ CAN-FD Data interface: SPI Data interface: I2C @ (variant 2) Data interface: UART @ USART (variant 3) Connector: Harwin M80-FC305F1-02 @ Antennas Connector: G125-2242096F1 @ Power and data (cable) Connector: Harwin Datamate 2-coax contact @ Antenna connection Connector: G125-2242096F1 @ 20-pin cable connector Connector: SAMTEC-ESQ-126-39-G-D @ 104-pin connector (PC/104 compatible) Connector: USB-C ## OPTIMUS Battery — AAC Clyde Space [batteries] https://newspacemarket.com/products/aac-optimus-40/ Capacity: 30 Wh @ OPTIMUS-30 Mass: 268 g @ OPTIMUS-30, typical Envelope (L×W×H): 95.89 mm x 90.17 mm x 21.55 mm @ OPTIMUS-30 Capacity: 40 Wh @ OPTIMUS-40 Mass: 335 g @ OPTIMUS-40, typical Envelope (L×W×H): 95.89 mm x 90.17 mm x 27.35 mm @ OPTIMUS-40 Capacity: 80 Wh @ OPTIMUS-80 Mass: 670 g @ OPTIMUS-80, typical Envelope (L×W×H): 95.89 mm x 90.17 mm x 56.94 mm @ OPTIMUS-80 Cell chemistry: Lithium Polymer Survival temperature: -10-10 °C @ Recommended Survival temperature: -20-20 °C @ 1 Year Survival temperature: -20-45 °C @ 3 Months Survival temperature: -20-60 °C @ 1 Month Operating temperature: -10-50 °C Supply voltage: 8.26 (nominal) @ EoC Voltage, typical Supply voltage: 6.2 (min) @ Full Discharge Voltage, typical Supply voltage: 8.4 (max) @ Charge Voltage Limit, max Supply voltage: 6.2 (min) @ Discharge Voltage Limit, min Power consumption: 0.1 W @ Quiescent Power Consumption, <, 30 Wh & 40 Wh Power consumption: 0.2 W @ Quiescent Power Consumption, <, 80 Wh Data interface: I2C TRL: 9 ## Airbus Space Battery Products — Airbus Defence and Space [batteries] https://newspacemarket.com/products/airbus-stellar-batt/ Capacity: 500-3000 Wh Supply voltage: 30 Supply voltage: 30 @ (variant 2) Supply voltage: 30 @ (variant 3) Supply voltage: 60 @ (variant 4) Flight heritage: OneWeb Constellation Flight heritage: Arrow Platform @ (variant 2) Flight heritage: Eurostar Neo Platform @ (variant 3) Flight heritage: Ariane 6 Launcher @ (variant 4) Flight heritage: OneSat Platform @ (variant 5) Flight heritage: ESA Forum Satellite @ (variant 6) Flight heritage: Galileo Platform @ (variant 7) ## ABSL CM1040 36s4p Li-ion Space Battery (126 V, 8 Ah) — EnerSys / ABSL Space Products [batteries] https://newspacemarket.com/products/absl-cm1040-36s4p-space-battery/ Capacity (charge): 8 Ah Capacity: 1066 Wh Cell chemistry: Li-ion Mass: 8400 g Envelope (L×W×H): 209 x 362 mm (footprint), 115 mm (height) Supply voltage: 126 (nominal) Flight heritage: over 5.5 billion cell hours of in-orbit heritage using ABSL™ Li-ion cell technology Connector: Two keyed circular connectors; no cell balancing electronics required ## ABSL CM2300 16s20p Li-ion Space Battery (56 V, 40 Ah) — EnerSys / ABSL Space Products [batteries] https://newspacemarket.com/products/absl-cm2300-16s20p-space-battery/ Cell chemistry: Li-ion Capacity (charge): 40 Ah Capacity: 2300 Wh Envelope (L×W×H): 260 x 359 mm (footprint), 177 mm (height) Mass: 19600 g Flight heritage: 5.5 billion cell hours of in-orbit heritage using ABSL™ Li-ion cell technology Supply voltage: 67.2-48 ## Intelligent Lithium Battery Module (BM2) — Pumpkin, Inc. [batteries] https://newspacemarket.com/products/pumpkin-bm2-battery/ Capacity: 86 Wh @ 2S4P (HG2) configuration Capacity: 100 Wh @ 2S4P (MJ1) configuration Capacity: 65 Wh @ 3S2P (HG2) configuration Capacity: 100 Wh @ 3S2P (MJ1) configuration Capacity: 86 Wh @ 4S2P (HG2) configuration Capacity: 100 Wh @ 4S2P (MJ1) configuration Mass: 700 g (max) Mass: 692 g @ Eight 18650 cells, with optional SUPERNOVA-compatible heatsink / mounting brackets Mass: 710 g (max) @ Eight 18650 cells, with optional SUPERNOVA-compatible heatsink / mounting brackets Mass: 542 g @ Eight 18650 cells, without SUPERNOVA-compatible heatsink / mounting brackets Mass: 560 g (max) @ Eight 18650 cells, without SUPERNOVA-compatible heatsink / mounting brackets Envelope (L×W×H): 100 @ Length Envelope (L×W×H): 100 @ Width, With SUPERNOVA-compatible heatsink / mounting bracket Envelope (L×W×H): 48.4 @ Height Supply voltage: 8.4 (nominal) @ 2S4P configurations Supply voltage: 12.6 (nominal) @ 3S2P configurations Supply voltage: 16.8 (nominal) @ 4S2P configurations Power consumption: 84 W @ peak power Power consumption: 168 W (max) @ peak power Power consumption: 1 W (max) Operating temperature: -40 °C @ Discharge Operating temperature: 75 °C (max) @ Discharge Operating temperature: -40 °C @ Charge Operating temperature: 50 °C (max) @ Charge Cell chemistry: 8× 18650-size Li-Ion ## Nanosatellite Power Subsystem — Stellar Exploration, Inc. [batteries] https://newspacemarket.com/products/nanosatellite-power-subsystem/ Capacity: 70 Wh @ single module Supply voltage: 28 (nominal) @ unregulated Design lifetime: 3 years (min) @ depending on usage Design lifetime: 5 years (max) @ depending on usage Data interface: RS-422 Data interface: CAN @ (variant 2) Flight heritage: >24 units launched 2018-2021 Lead time: 4-6 Cell chemistry: Lithium-ion, redundant modules with dedicated per-string balancing and control ## BAT-110 — Berlin Space Technologies [batteries] https://newspacemarket.com/products/bat-110-battery-system/ Operating temperature: -20 °C Survival temperature: -30 °C Envelope (L×W×H): 240x119x87mm³ Mass: 3000 g Supply voltage: 23.1 (nominal) Capacity: 172 Wh Design lifetime: 5 years @ LEO Cycles / reuses: 3000 @ @ 0.5C/1C & 100% DoD Flight heritage: Yes Radiation tolerance (TID): 30 krad Power consumption: 690 W (max) @ Peak @ 4C Power consumption: 170 W (max) @ Recommended @ 1C Cell chemistry: Lithium-Ferrite (Li-Fe) Capacity (charge): 2.5 Ah @ per string ## IM200 Smart Optical Imager — AAC Clyde Space [cameras] https://newspacemarket.com/products/aac-im200/ Focal length: 16 @ Standard lens Focal length: 25 @ Standard lens (variant 2) Focal length: 35 @ Standard lens (variant 3) Focal length: 50 @ Standard lens (variant 4) Mass: 59 g @ using 50mm F2.0 lens Supply voltage: 3.6 (min) @ Supply voltage Supply voltage: 3.651 (typical) @ Supply voltage Supply voltage: 5 (max) @ Supply voltage Power consumption: 0.7 W (typical) @ nominal (< 700 mW) Power consumption: 0.4 W (min) @ Power consumption Power consumption: 0.7 W (typical) @ Power consumption (At 3.65V, at 5Hz full frame capture rate) Power consumption: 1 W (max) @ Power consumption Operating temperature: -20 °C (min) Operating temperature: 40 °C (max) Radiation tolerance (TID): 9 krad (max) @ qualified up to Radiation tolerance (TID): 9 krad (min) @ >9 Flight heritage: LEO since 2019 (IM200), multiple missions since 2015 (ST200 Star Tracker) ## Gecko imager — Dragonfly Aerospace [cameras] https://newspacemarket.com/products/dragonfly-gecko-imager/ Ground sample distance: 39 m @ at 500 km Swath width: 80 km @ RGB at 500 km Swath width: 160 km @ WIDE SWATH at 500 km Mass: 500 g (max) @ incl. eleсtronics, RGB Mass: 500 g @ incl. eleсtronics, WIDE SWATH Spectral bands: 3 @ Standard RGB Power consumption: 6 W (max) @ Imaging mode (RGB) Power consumption: 7 W (max) @ Imaging mode (WIDE SWATH) Power consumption: 4 W (max) @ Readout mode Supply voltage: 5 @ Power Supply Operating temperature: 10 °C (min) Operating temperature: 30 °C (max) Survival temperature: -20 °C (min) Survival temperature: 55 °C (max) Envelope (L×W×H): 1U (65 mm x 90 mm x 105 mm) TRL: 9 Envelope (L×W×H): 1U (65 mm x 90 mm x 105 mm) @ (variant 2) TRL: 9 @ (variant 2) ## SOC-750 Midwave Infrared Hyperspectral Imager — Surface Optics Corporation [cameras] https://newspacemarket.com/products/surface-optics-soc-750-mwir-hyperspectral-imager/ Envelope (L×W×H): 256 x 240 pixels x 42 bands Spectral bands: 42 @ High Brightness configuration Spectral bands: 64 @ High Resolution configuration ## KissCAM V1.0 — Entry-Level CubeSat Camera — MVP Aerospace [cameras] https://newspacemarket.com/products/mvp-aerospace-kisscam-v1/ Sensor resolution: 1.2 Spectral bands: Colour Focal length: 2.3 @ stock lens Mass: 10 g Mass: 7 g @ without lens Mass: 3 g @ of stock lens Envelope (L×W×H): 38 x 20 x 18mm Envelope (L×W×H): 38 x 20 x 17 @ 1 mm tolerance Supply voltage: 3.3 (nominal) @ supply Supply voltage: 5 (nominal) @ supply (variant 2) Supply voltage: 3.2 (min) @ supply Supply voltage: 5.5 (max) @ supply Power consumption: 80mA @ supply current Data interface: UART Data interface: RS422 @ (variant 2) Connector: 6-way Molex Picoblade connector (53261-0671) Operating temperature: -20 °C (min) @ tested Operating temperature: 60 °C (max) @ tested Survival temperature: -20 °C (min) @ Storage Temperature Survival temperature: 85 °C (max) @ Storage Temperature Flight heritage: Confirmed ## KSOI-300 Optical Imager (300 mm) — Kairo Space [cameras] https://newspacemarket.com/products/kairo-space-ksoi-300/ Ground sample distance: 1 m @ @500km Swath width: 12 km @ @500km Mass: 16000 g (max) Envelope (L×W×H): 500 x 370 x 370 mm³ Power consumption: 12 W (max) Data interface: LVDS Data interface: ETHERNET @ (variant 2) Radiation tolerance (TID): 150 krad @ Lens Radiation tolerance (TID): 60 krad @ Electronics Design lifetime: 3 years Focal length: 2500 Sensor resolution: 12480 x 256 pixels Spectral bands: PAN(R, G, B optional) Operating temperature: -10 °C ## Satellite Imagery Analytics — Planet Labs PBC [cameras] https://newspacemarket.com/products/satellite-imagery-analytics/ Spectral bands: 8 Mass: 110000 g Envelope (L×W×H): 60 x 60 x 95 cm Design lifetime: 6 years Ground sample distance: 0.5 m @ Orthorectified, All assets Ground sample distance: 0.86 m @ Panchromatic, SkySat-1, SkySat-2 Ground sample distance: 1 m @ Multispectral, SkySat-1, SkySat-2 Ground sample distance: 0.65 m @ Panchromatic, SkySat-3 - SkySat-15 Ground sample distance: 0.81 m @ Multispectral, SkySat-3 - SkySat-15 Ground sample distance: 0.58 m @ Panchromatic, SkySat-16 - SkySat-21 Ground sample distance: 0.72 m @ Multispectral, SkySat-16 - SkySat-21 ## Mantis — Dragonfly Aerospace [cameras] https://newspacemarket.com/products/dragonfly-mantis-imager/ Ground sample distance: 16 m @ at 500 km, RGB Ground sample distance: 16 m @ at 500 km, PAN Ground sample distance: 32 m @ at 500 km, MS Swath width: 32 km @ at 500 km Mass: 500 g (max) @ incl. eleсtronics Spectral bands: 6 @ MS Spectral bands: 96 @ HS available Power consumption: 6 W (max) @ Imaging mode Power consumption: 4 W (max) @ Readout mode Supply voltage: 5 @ DC Operating temperature: 10 °C (min) Operating temperature: 30 °C (max) Survival temperature: -20 °C (min) Survival temperature: 55 °C (max) Envelope (L×W×H): 1U (65 mm x 90 mm x 107 mm) TRL: 9 Envelope (L×W×H): 1U (65 mm x 90 mm x 107 mm) @ (variant 2) TRL: 9 @ (variant 2) Envelope (L×W×H): 1U (65 mm x 90 mm x 107 mm) @ (variant 3) TRL: 9 @ (variant 3) ## Chameleon — Dragonfly Aerospace [cameras] https://newspacemarket.com/products/dragonfly-chameleon-imager/ Envelope (L×W×H): 2.5U (100 mm x 100 mm x 215 mm) (RGB) TRL: 9 Envelope (L×W×H): 2.5U (100 mm x 100 mm x 215 mm) (MULTISPECTRAL) @ (variant 2) Envelope (L×W×H): 2.5U (100 mm x 100 mm x 215 mm) (HYPERSPECTRAL) @ (variant 3) Ground sample distance: 10 m @ at 500 km Swath width: 39 km @ at 500 km Mass: 1600 g @ incl. eleсtronics Power consumption: 10 W (max) @ Imaging mode Power consumption: 5 W (max) @ Readout mode Supply voltage: 5 @ DC Operating temperature: 10-30 °C Survival temperature: -20-55 °C ## Caiman — Dragonfly Aerospace [cameras] https://newspacemarket.com/products/dragonfly-caiman-imager/ TRL: 9 TRL: 9 @ (variant 2) Ground sample distance: 3.25 m @ RGB at 500 km Ground sample distance: 3.25 m @ Multispectral PAN at 500 km Ground sample distance: 6.5 m @ Multispectral MS at 500 km Swath width: 13 km @ at 500 km Mass: 1400 g @ incl. electronics Spectral bands: 11 @ MS Envelope (L×W×H): 3U (100 mm x 100 mm x 250 mm with rear-mounted nCCM) Data interface: LVDS Data interface: SpaceWire @ (variant 2) Data interface: SPI @ (variant 3) Data interface: I2C @ (variant 4) Data interface: CAN @ (variant 5) Data interface: RS-422 @ (variant 6) Data interface: RS-485 @ (variant 7) Power consumption: 10 W (max) @ Imaging mode Power consumption: 4 W (max) @ Readout mode Supply voltage: 5 (nominal) @ DC Operating temperature: 10 °C (min) Operating temperature: 30 °C (max) Survival temperature: -20 °C (min) Survival temperature: 55 °C (max) ## Raptor — Dragonfly Aerospace [cameras] https://newspacemarket.com/products/dragonfly-raptor-imager/ Ground sample distance: 0.5 m @ PAN at 500 km Ground sample distance: 0.36 m @ PAN with super-resolution processing at 500 km Ground sample distance: 2 m @ MS at 500 km Swath width: 8 km @ at 500 km Mass: 60000 g @ Including electronics Spectral bands: 8 @ 6 x MS plus 2x PAN Envelope (L×W×H): 635 mm x 1633 mm (est) plus electronics Power consumption: 45 W (max) @ Imaging mode Power consumption: 25 W (max) @ Readout mode Supply voltage: 28 @ DC Operating temperature: 10 °C (min) Operating temperature: 30 °C (max) Survival temperature: -20 °C (min) Survival temperature: 55 °C (max) TRL: 5 ## Komodo — Dragonfly Aerospace [cameras] https://newspacemarket.com/products/dragonfly-komodo-imager/ TRL: 5 TRL: 5 @ (variant 2) Ground sample distance: 1.5 m @ RGB at 500 km Ground sample distance: 1.5 m @ MULTISPECTRAL PAN at 500 km Ground sample distance: 3 m @ MULTISPECTRAL MS (binned 2x2) at 500 km Swath width: 6.1 km @ RGB at 500 km Swath width: 15 km @ MULTISPECTRAL at 500 km Mass: 12000 g @ est, incl. electronics Spectral bands: 11 @ MS Envelope (L×W×H): 200 mm x 200 mm x 340 mm (est) Data interface: LVDS Data interface: SpaceWire @ (variant 2) Data interface: RS422 @ TMTC Interface Power consumption: 10 W (max) @ RGB Imaging mode Power consumption: 45 W @ est, MULTISPECTRAL Imaging mode Power consumption: 5 W (max) @ RGB Readout mode Power consumption: 25 W (max) @ MULTISPECTRAL Readout mode Supply voltage: 5 @ DC Supply voltage: 28 @ DC (variant 2) Operating temperature: 10-30 °C Survival temperature: -20-55 °C ## Orion12MP — Infinity Avionics [cameras] https://newspacemarket.com/products/infinity-avionics-orion12mp/ Operating temperature: -10 °C TRL: 9 Focal length: 550 Operating temperature: -10 °C @ (variant 2) TRL: 6 @ (variant 2) Sensor resolution: 12 Sensor resolution: 4096x3072 px @ (variant 2) Mass: 290 g Envelope (L×W×H): 96 mm x 91 mm x 37 mm Supply voltage: 5 Power consumption: 2.5 W @ Idle Power consumption: 6 W @ max ## SelfieCam Video — Infinity Avionics [cameras] https://newspacemarket.com/products/infinity-avionics-selfiecam-video/ Spectral bands: 1 @ VIS Focal length: 1 Mass: 10 g Envelope (L×W×H): 50 mm × 30 mm Supply voltage: 5 Power consumption: 0.75 W Data interface: UART @ with ASCII commands Data interface: UART Operating temperature: -20 °C (min) TRL: 9 Operating temperature: 60 °C (max) Survival temperature: -20 °C (min) Survival temperature: 60 °C (max) Radiation tolerance (TID): 30 krad (max) Flight heritage: demonstrated flight heritage through numerous space missions ## Owl 640 M — Raptor Photonics [cameras] https://newspacemarket.com/products/raptor-photonics-owl-640-m/ Spectral bands: 1 @ enabling the coverage from 600 to 1700 nm of the electromagnetic spectrum Spectral bands: 1 @ VIS-SWIR InGaAs technology | Enables imaging from 0.6μm to 1.7μm Power consumption: 2.5 W (max) ## KissCAM V2.0 — MVP Aerospace [cameras] https://newspacemarket.com/products/mvp-aerospace-kisscam-pro/ Flight heritage: Flight Heritage. See our photo gallery! Sensor resolution: 1.2 Sensor resolution: 1280 x 960 Resolution @ HD mode Sensor resolution: 640 x 480 pixels @ standard definition Spectral bands: Colour Bayer Filter Envelope (L×W×H): 38 x 20 x 18mm Mass: 10 g Supply voltage: 3.3-5 Data interface: UART Data interface: RS422 UART @ (variant 2) Operating temperature: -20-60 °C Survival temperature: -20-85 °C Supply voltage: 3.2-5.5 @ (variant 2) Connector: 6-way Molex Picoblade connector (53261-0671) Envelope (L×W×H): 38 x 20 x 17 mm @ 1 mm tolerance Mass: 7 g @ without lens Mass: 3 g @ stock lens Focal length: 2.3 @ stock lens ## Deployer SERIES 4x3U — KOSMOLAB Launch Services [deployers] https://newspacemarket.com/products/kosmolab-tpk-4x3u/ Separation velocity: 0.5-2 m/s Separation velocity: 2 m/s (max) Operating temperature: -60 °C Max payload mass: 26000 g Mass: 10000 g Envelope (L×W×H): 480 × 290 × 299 mm Flight heritage: TPK SERIES deployer have been flight-qualified as part of the Angara-A5 launch vehicle (2024 launch). All satellites were successfully deployed into target orbits. ## Deployer SERIES 2x3U/1x6U — KOSMOLAB Launch Services [deployers] https://newspacemarket.com/products/kosmolab-tpk-2x3u-1x6u/ Envelope (L×W×H): 480 × 290 × 299 mm Mass: 9500 g Max payload mass: 26000 g Operating temperature: -60 °C (min) Operating temperature: 60 °C (max) Lead time: 4 (min) Lead time: 6 (max) Flight heritage: Angara-A5 launch vehicle (2024 launch) Separation velocity: 0.5-2 m/s Separation velocity: 2 m/s (max) ## Deployer SERIES 2x6U — KOSMOLAB Launch Services [deployers] https://newspacemarket.com/products/kosmolab-tpk-2x6u/ Separation velocity: 0.5-2 m/s Separation velocity: 2 m/s (max) Operating temperature: -60 °C Capacity: 6 @ per CubeSat Envelope (L×W×H): 480 × 290 × 299 mm Mass: 9000 g Max payload mass: 26000 g Lead time: 4 @ min Lead time: 6 @ max Flight heritage: flight-qualified as part of the Angara-A5 launch vehicle (2024 launch) ## Deployer SERIES 12U — KOSMOLAB Launch Services [deployers] https://newspacemarket.com/products/kosmolab-tpk-12u/ Capacity: 12 Envelope (L×W×H): 480 × 290 × 299 mm Mass: 8500 g Max payload mass: 26000 g Operating temperature: -60 °C (min) Operating temperature: 60 °C (max) Lead time: 4 (min) Lead time: 6 (max) Flight heritage: flight-qualified as part of the Angara-A5 launch vehicle (2024 launch) Separation velocity: 0.5-2 m/s Separation velocity: 2 m/s (max) ## Deployer SERIES 16U — KOSMOLAB Launch Services [deployers] https://newspacemarket.com/products/kosmolab-tpk-16u/ Separation velocity: 0.5-2 m/s Separation velocity: 2 m/s (max) Capacity: 16 Envelope (L×W×H): 600 × 290 × 299 mm Mass: 12000 g Max payload mass: 40000 g Operating temperature: -60-60 °C Lead time: 4-6 Flight heritage: Angara-A5 launch vehicle (2024 launch) ## Deployer EXT 16U — KOSMOLAB Launch Services [deployers] https://newspacemarket.com/products/kosmolab-tpk-16u-ext/ Capacity: 16 Envelope (L×W×H): 600 × 290 × 299 mm Mass: 9000 g Max payload mass: 40000 g Operating temperature: -60-60 °C Lead time: 6-9 Flight heritage: TPK SERIES deployer have been flight-qualified as part of the Angara-A5 launch vehicle (2024 launch). All satellites were successfully deployed into target orbits. Separation velocity: 0.5-2 m/s Separation velocity: 2 m/s (max) ## Deployers 12U LIGHT — KOSMOLAB Launch Services [deployers] https://newspacemarket.com/products/kosmolab-tpk-12u-light/ Separation velocity: 0.5-2 m/s Separation velocity: 2 m/s (max) Capacity: 12 Mass: 6000 g Max payload mass: 26000 g Operating temperature: -60 °C (min) Operating temperature: 60 °C (max) Lead time: 6 (min) Lead time: 9 (max) ## Deployers 16U LIGHT — KOSMOLAB Launch Services [deployers] https://newspacemarket.com/products/kosmolab-tpk-16u-light/ Capacity: 16 Mass: 6000 g Max payload mass: 40000 g Operating temperature: -60 °C (min) Operating temperature: 60 °C (max) Lead time: 6 (min) Lead time: 9 (max) Separation velocity: 0.5-2 m/s Separation velocity: 2 m/s (max) ## Deployers 3U — KOSMOLAB Launch Services [deployers] https://newspacemarket.com/products/kosmolab-tpk-3u/ Operating temperature: -60 °C Capacity: 3 (nominal) Envelope (L×W×H): 557 × 158 × 187 mm Mass: 4700 g Max payload mass: 6000 g Separation velocity: 0.5 m/s (min) Separation velocity: 2 m/s (max) Lead time: 4 (min) Lead time: 6 (max) ## Deployers 4U — KOSMOLAB Launch Services [deployers] https://newspacemarket.com/products/kosmolab-tpk-4u/ Capacity: 4 Envelope (L×W×H): 557 × 158 × 187 mm Mass: 4700 g Max payload mass: 6000 g Operating temperature: -60-60 °C Lead time: 4-6 Separation velocity: 0.5-2 m/s Separation velocity: 2 m/s (max) ## EBAD TiNi Microlatch ML50-2 Separation System — Ensign-Bickford Aerospace & Defense (EBAD) [deployers] https://newspacemarket.com/products/ebad-tini-microlatch-ml50-2-separation-system/ Supply voltage: 10-18 Actuation: non-pyro Actuation: non-pyro @ (variant 2) ## Satellite Dispenser Systems — Beyond Gravity (ex-RUAG Space) [deployers] https://newspacemarket.com/products/beyond-gravity-satellite-dispenser-systems/ Flight heritage: Galileo, TerraBella, Radarsat Constellation, Amazon Leo, Eutelsat OneWeb Max payload mass: 700000 g @ per satellite Mass: 150000 g (max) @ structural mass Flight heritage: flight proven with the successful maiden launch of a Soyuz ST-B from the European spaceport in French Guiana, in October 2011. @ Galileo Dispenser ## Deployer SERIES 4x3U — KOSMOLAB Launch Services [deployers] https://newspacemarket.com/products/deployer-series-4x3u/ Capacity: 12 @ 4x3U configuration Max payload mass: 26000 g Mass: 10000 g Operating temperature: -60-60 °C Lead time: 4-6 Envelope (L×W×H): 480 × 290 × 299 mm Separation velocity: 0.5-2 m/s Separation velocity: 2 m/s (max) ## Deployer EXT 16U — KOSMOLAB Launch Services [deployers] https://newspacemarket.com/products/deployer-ext-16u/ Capacity: 16 Envelope (L×W×H): 600 × 290 × 299 mm Mass: 9000 g Max payload mass: 40000 g Operating temperature: -60-60 °C Lead time: 6-9 Flight heritage: TPK SERIES deployer have been flight-qualified as part of the Angara-A5 launch vehicle (2024 launch). All satellites were successfully deployed into target orbits. Separation velocity: 0.5-2 m/s Separation velocity: 2 m/s (max) ## Deployers 12U LIGHT — KOSMOLAB Launch Services [deployers] https://newspacemarket.com/products/deployers-12u-light/ Separation velocity: 0.5-2 m/s Separation velocity: 2 m/s (max) Operating temperature: -60 °C Capacity: 12 Mass: 6000 g Max payload mass: 26000 g ## Deployer SERIES 2x6U — KOSMOLAB Launch Services [deployers] https://newspacemarket.com/products/deployer-series-2x6u/ Separation velocity: 0.5-2 m/s Separation velocity: 2 m/s (max) Capacity: 6 @ num_max, x2 Envelope (L×W×H): 480 × 290 × 299 mm Mass: 9000 g Max payload mass: 26000 g Operating temperature: -60 °C (min) Operating temperature: 60 °C (max) Lead time: 4 (min) Lead time: 6 (max) Flight heritage: flight-qualified as part of the Angara-A5 launch vehicle (2024 launch) ## Deployer SERIES 2x3U/1x6U — KOSMOLAB Launch Services [deployers] https://newspacemarket.com/products/deployer-series-2x3u-1x6u/ Envelope (L×W×H): 480 × 290 × 299 mm Mass: 9500 g Max payload mass: 26000 g Operating temperature: -60 °C (min) Operating temperature: 60 °C (max) Lead time: 4 (min) Lead time: 6 (max) Flight heritage: flight-qualified as part of the Angara-A5 launch vehicle (2024 launch) Separation velocity: 0.5-2 m/s Separation velocity: 2 m/s (max) ## Deployer SERIES 12U — KOSMOLAB Launch Services [deployers] https://newspacemarket.com/products/deployer-series-12u/ Separation velocity: 0.5-2 m/s Separation velocity: 2 m/s (max) Operating temperature: -60 °C Capacity: 12 Envelope (L×W×H): 480 × 290 × 299 mm Mass: 8500 g Max payload mass: 26000 g Lead time: 4-6 Flight heritage: TPK SERIES deployer have been flight-qualified as part of the Angara-A5 launch vehicle (2024 launch) ## Deployer SERIES 16U — KOSMOLAB Launch Services [deployers] https://newspacemarket.com/products/deployer-series-16u/ Capacity: 16 Mass: 12000 g Max payload mass: 40000 g Operating temperature: -60 °C (min) Operating temperature: 60 °C (max) Lead time: 4 (min) Lead time: 6 (max) Envelope (L×W×H): 600 × 290 × 299 mm Separation velocity: 0.5-2 m/s Separation velocity: 2 m/s (max) ## Deployers 16U LIGHT — KOSMOLAB Launch Services [deployers] https://newspacemarket.com/products/deployers-16u-light/ Separation velocity: 0.5-2 m/s Separation velocity: 2 m/s (max) Capacity: 16 Mass: 6000 g Max payload mass: 40000 g Operating temperature: -60 °C (min) Operating temperature: 60 °C (max) Lead time: 6 (min) Lead time: 9 (max) ## Deployers 4U — KOSMOLAB Launch Services [deployers] https://newspacemarket.com/products/deployers-4u/ Capacity: 4 Envelope (L×W×H): 557 × 158 × 187 mm Mass: 4700 g Max payload mass: 6000 g Operating temperature: -60-60 °C Lead time: 4-6 Separation velocity: 0.5-2 m/s Separation velocity: 2 m/s (max) ## EXOpod Nova — Exolaunch [deployers] https://newspacemarket.com/products/exolaunch-exopod-nova/ Capacity: 0.25 Envelope (L×W×H): 6U/8U, 12U, 16U (configurable to smaller) Envelope (L×W×H): 0.25U to 16U @ (variant 2) Max payload mass: 2500 g @ 1U Max payload mass: 4500 g @ 2U Max payload mass: 7000 g @ 3U Max payload mass: 9000 g @ 4U Max payload mass: 14000 g @ 6U Max payload mass: 16000 g @ 6UXL Max payload mass: 18000 g @ 8U Max payload mass: 26000 g @ 12U Max payload mass: 36000 g @ 16U Actuation: spring Flight heritage: Flight heritage from the SpaceX Transporter Rideshare Program as well as from Rocket Lab’s Electron and ISRO’s PSLV. EXOpod and EXOpod Nova family of deployers has launched on 19 missions and has successfully deployed over 270 Cubesats between 0.25U to 16 Mass: 7700 g @ 8U S1 Mass: 8830 g @ 8U S2 Mass: 9770 g @ 12U S1 Mass: 11310 g @ 12U S2 Mass: 12320 g @ 12U S3 Mass: 13320 g @ 12U S4 Mass: 10750 g @ 16U S1 Mass: 12850 g @ 16U S2 Mass: 14050 g @ 16U S3 Mass: 15270 g @ 16U S4 ## EXOpod AIR — Exolaunch [deployers] https://newspacemarket.com/products/exolaunch-exopod-air/ Max payload mass: 2000 g @ per U Capacity: 12 Mass: 8630 g Flight heritage: The EXOpod family of deployers has launched across 30+ missions and has successfully deployed over 425+ CubeSats between 0.25U to 16U into orbit without failure. Envelope (L×W×H): 8U, 12U, 12UXL, 16U Envelope (L×W×H): 0.25U to 16U @ (variant 2) ## PicoSatellite Launcher PSL6U / PSL6U XL — EXA (Astro-und Feinwerktechnik) [deployers] https://newspacemarket.com/products/psl6u-psl6u-xl-picosatellite-launcher/ Capacity: 6 @ for PSL6U Capacity: 6 @ for PSL6U XL Max payload mass: 12000 g @ for PSL6U Max payload mass: 12000 g @ for PSL6U XL Mass: 12000 g (max) Mass: 12000 g (max) @ (variant 2) ## PicoSatellite Launcher PSL12U / PSL12U XL — EXA (Astro-und Feinwerktechnik) [deployers] https://newspacemarket.com/products/psl12u-psl12u-xl-picosatellite-launcher/ Mass: 24000 g (max) Mass: 24000 g (max) @ (variant 2) Max payload mass: 24000 g ## ST Engineering Power Control & Distribution Unit (PCDU) — ST Engineering Satellite Systems [eps] https://newspacemarket.com/products/stengg-pcdu/ Output power (total): 4000 W @ Peak Power in LEO SAR mission Conversion efficiency: 97 (min) Output power (total): 4000 W @ @ 32 V Conversion efficiency: 97 (min) @ (variant 2) Supply voltage: 22 (min) @ Primary Bus Voltage Supply voltage: 38 (max) @ Primary Bus Voltage Output rails: 1 A to 10 A LCL Power Distribution Lines Protections: 56 LCL @ 10 A or less Protections: 48 LCL @ 5 A or less @ (variant 2) Protections: 4 RLCL (retriggerable) for critical lines @ (variant 3) Protections: 72 heater lines @ (variant 4) Mass: 24500 g Envelope (L×W×H): 453 x 340 x 279 mm3 Data interface: CAN Operating temperature: -20 °C (min) Operating temperature: 60 °C (max) Radiation tolerance (TID): 20 krad Design lifetime: 5 years Flight heritage: In-house Heritage Design - 7th year in orbit without anomalies (TRL-9) Power consumption: 4000 W Power consumption: 2000 W @ (variant 2) ## Electrical Power System (EPS) 2000 — C3S LLC [eps] https://newspacemarket.com/products/c3s-ant-antenna-system/ Power consumption: 2 W Output power (total): 2 W Conversion efficiency: 98 Output rails: 23.1 - 33.6 V (28 V unregulated) Output rails: 5 V @ (variant 2) Output rails: 12 V @ (variant 3) Protections: Retriggering LCLs Mass: 6500 g @ 560 W, 345 Wh, 15x 28 V output channels Envelope (L×W×H): 210 x 255 x 115 mm @ 560 W, 345 Wh, 15x 28 V output channels Supply voltage: 6 (min) @ Input Supply voltage: 70 (max) @ Input Data interface: CAN @ Primary interface Data interface: UART @ Secondary interface Operating temperature: -40 °C (min) @ Qualification Operating temperature: 60 °C (max) @ Qualification Radiation tolerance (TID): 30 krad ## STARBUCK-NANO CubeSat EPS — AAC Clyde Space [eps] https://newspacemarket.com/products/aac-clyde-space-starbuck-nano-plus-eps/ Output rails: 3.3V, 5V, and 12V Protections: 10 Latching Current Limiters Mass: 86 g Envelope (L×W×H): 95.89 mm x 90.17 mm x 16.2 mm Supply voltage: 8.2 (max) Data interface: I2C Operating temperature: -40-85 °C Survival temperature: -50-100 °C Radiation tolerance (TID): 10 krad Design lifetime: 5 years TRL: 9 ## Compact Electrical Power Systems (ICEPS2) — Innovative Space Logistics [eps] https://newspacemarket.com/products/compact-electrical-power-systems-iceps2-1478/ Output rails: 3.3V, 5V, unregulated battery voltage Protections: Battery charge and discharge protection Protections: I2C Watchdog (stack reset on comms failure) @ (variant 2) Protections: Complete output bus protection including short circuit and backflow protection @ (variant 3) Flight heritage: Design based on heritage from ICEPS1 design flown on PEASSS CubeSat (2016) Flight heritage: ICEPS2, second generation, flown on the Hiber 1,2 CubeSats (2018) @ (variant 2) Flight heritage: PBP-4S1P has deployment heritage from ISS @ (variant 3) Protections: Back-to-back (B2B) protection MOSFETs @ (variant 4) Protections: Charge load switch for charge current limiting, with under and overvoltage lockout @ (variant 5) Protections: Trickle charge bypass diode to resuscitate batteries that have dropped to voltages below the charge undervoltage lockout threshold @ (variant 6) Protections: Discharge load switch for active discharge current limiting @ (variant 7) Protections: Surge protection using TVS protection diodes @ (variant 8) Protections: output ideal diode protecting against current backflow from the RAIL @ (variant 9) Operating temperature: -40-85 °C @ Without battery Survival temperature: -50-65 °C @ Storage temperature Design lifetime: 12 years @ Storage lifetime (at relative humidity < 60 %) Operating temperature: 10-45 °C @ With battery, charge (heaters disabled) Operating temperature: 0-45 °C @ With battery, charge up to 800 mA Operating temperature: -20-60 °C @ With battery, discharge Survival temperature: -20-50 °C @ With battery, up to 1 month (at relative humidity < 60 % and 30% state of charge) Survival temperature: -20-40 °C @ With battery, up to 3 months (at relative humidity < 60 % and 30% state of charge) Survival temperature: -20-20 °C @ With battery, up to 1 year (at relative humidity < 60 % and 30% state of charge) Design lifetime: 6-12 years @ Battery holding charge -20°C to +20°C Power consumption: 0.093 W @ Static (Idle) consumption Output rails: Battery Voltage @ VD0 Output rails: 4.99 V @ VD1, unloaded Output rails: 3.33 V @ VD2, unloaded Output rails: 4.99 V @ VD3 default (Type C only) Output rails: 2.8 V to 12.08 V @ VD3 custom output (Type C only) Output rails: 3.33 V @ VD4 default (Type C only) Output rails: 2.8 V to 12.08 V @ VD4 custom output (Type C only) Output rails: 28.2 V @ VD5 default (Type C only) Output rails: Vbat to 32.1 V @ VD5 custom output (Type C only) Mass: 184 g @ Type A Mass: 310 g @ Type B Mass: 360 g @ Type C Envelope (L×W×H): 96 x 92 x 26.5 mm3 @ Type A, IU mainboard + 2 cell BP (excluding CSKB) Envelope (L×W×H): 96 x 92 x 11.3 mm3 @ Type B, IU mainboard (excluding CSKB) Envelope (L×W×H): 96 x 92 x 16 mm3 @ Type C, IU mainboard + DaughterBoard (excluding CSKB) Envelope (L×W×H): 94 x 89 x 21.0 mm3 @ Type B and C, 4 cell BP (excluding CSKB) Data interface: I2C Supply voltage: 3.3 Supply voltage: 5 @ (variant 2) Supply voltage: 7.2 @ (variant 3) Supply voltage: 14.4 @ (variant 4) ## Electrical Power System eps lp — Dragonfly Aerospace [eps] https://newspacemarket.com/products/electrical-power-system-eps-lp/ Output power (total): 1500 W @ Total Input, Output & Battery Power Output rails: Unregulated unprotected power bus port & PDM ports as per configuration options Protections: Over current Protections: Over load @ (variant 2) Protections: External Trip Input @ (variant 3) Mass: 3300 g Envelope (L×W×H): 211 x 153 x 175 mm Supply voltage: 29.7 (nominal) Supply voltage: 22 (min) Supply voltage: 32 (max) Data interface: CAN Operating temperature: -10 °C (min) Operating temperature: 50 °C (max) Radiation tolerance (TID): 20 krad Design lifetime: 8 years @ LEO Flight heritage: TRL 9 Power consumption: 1500 W Power consumption: 600 W @ (variant 2) Power consumption: 1500 W @ (variant 3) ## SOLO-EPS-4 — 2NDSpace Srl [eps] https://newspacemarket.com/products/solo-eps-4/ Power consumption: 100 W Envelope (L×W×H): 97x92x44 Mass: 480 g Output rails: Standard 3.3 / 5 / 12 / 16.8V, Custom Output power (total): 104 W @ Overall Peak Power Data interface: RS485 Data interface: UART @ (variant 2) Data interface: CAN @ (variant 3) Data interface: I2C @ (variant 4) Protections: OV,UV,OC protection; Latch-up protected outputs ## SOLO-EPS-8 — 2NDSpace Srl [eps] https://newspacemarket.com/products/solo-eps-8/ Power consumption: 160 W Envelope (L×W×H): 97x92x66 Mass: 768 g Output rails: Standard 3.3 / 5 / 12 / 16.8 Output power (total): 160 W @ Overall Peak Power output Protections: OV,UV,OC protection; Latch-up protected outputs Data interface: RS-485 Data interface: UART @ (variant 2) Data interface: CAN @ (variant 3) Data interface: I2C @ (variant 4) ## CubeSat 0.5U Electronics Package — Tiger Innovations, Inc. [eps] https://newspacemarket.com/products/tiger-innovations-cubesat-electronics-package/ Flight heritage: TSX-5, STPSat-1, STPSat-2 Output rails: 5V@2A; 3.3V@2A Protections: Low V, Over V, Low Amp Power consumption: 0.05 W @ Quiescent Mass: 215 g @ with Batteries Envelope (L×W×H): 20mm (Height) ## ISIS Modular Electrical Power Subsystem version 2 (v2) — ISISPACE Group [eps] https://newspacemarket.com/products/isispace-modular-eps-integrated-power-stack/ Output rails: 3.3V, 5V, VBAT Protections: Hardware over-current protection Protections: voltage and over-current protection @ (variant 2) Protections: discharge current limiting @ (variant 3) Protections: charge current limiting, under and overvoltage lockout @ (variant 4) Protections: voltage surge protection using TVS protection diodes @ (variant 5) Mass: 184 g (typical) @ Type A Mass: 310 g (typical) @ Type B Mass: 360 g (typical) @ Type C Envelope (L×W×H): 96 x 92 x 26.5 mm3 @ IU mainboard + 2 cell BP, Type A Envelope (L×W×H): 96 x 92 x 11.3 mm3 @ IU mainboard, Type B Envelope (L×W×H): 96 x 92 x 16 mm3 @ IU mainboard + daughterboard, Type C Envelope (L×W×H): 94 x 89 x 21.0 mm3 @ 4 cell BP, Type B and C Power consumption: 0.093 W @ Static (Idle) consumption Data interface: I2C Operating temperature: -40 °C (min) @ Without battery Operating temperature: 85 °C (max) @ Without battery Operating temperature: 10 °C (min) @ With battery, charge (heaters disabled) Operating temperature: 45 °C (max) @ With battery, charge (heaters disabled) Operating temperature: 0 °C (min) @ With battery, charge up to 800 mA Operating temperature: 45 °C (max) @ With battery, charge up to 800 mA Operating temperature: -20 °C (min) @ With battery, discharge Operating temperature: 60 °C (max) @ With battery, discharge Survival temperature: -50 °C (min) @ Storage temperature, Without battery Survival temperature: 65 °C (max) @ Storage temperature, Without battery Survival temperature: -20 °C (min) @ Storage condition, up to 1 month Survival temperature: 50 °C (max) @ Storage condition, up to 1 month Survival temperature: -20 °C (min) @ Storage condition, up to 3 months Survival temperature: 40 °C (max) @ Storage condition, up to 3 months Survival temperature: -20 °C (min) @ Storage condition, up to 1 year Survival temperature: 20 °C (max) @ Storage condition, up to 1 year Flight heritage: Design based on heritage from PEASSS Cubesat (2016) Flight heritage: Second generation improvements flown on the Hiber 1,2 Cubesats (2018) @ (variant 2) Supply voltage: 4.99 Supply voltage: 3.33 @ (variant 2) ## ODALISS PDCU — Emxys [eps] https://newspacemarket.com/products/emxys-pdcu/ Power consumption: 8 W @ nominal (per pack for 3U) Power consumption: 36 W @ peak (per pack for 3U) Output rails: Main and redundant independent unregulated buses +7.6V nominal (+8.2V Max.), Safety dual battery-powered regulated +3.3V bus (1.5A max.), Regulated +5.0V and +3.3V buses (1.5A max. each) Protections: Battery overvoltage and undervoltage protections, overvoltage, undervoltage, overcurrent and short-circuit Mass: 360 g Envelope (L×W×H): 870mm x 870mm x 55mm Operating temperature: -45-85 °C Data interface: I2C Output power (total): 36 W Conversion efficiency: 95 ## NanoPower P60 — GomSpace [eps] https://newspacemarket.com/products/nanopower-p60/ Data interface: CAN Data interface: I2C @ (variant 2) Output rails: 3.3 V Output rails: 5 V @ (variant 2) Supply voltage: 16 @ recommended battery voltage Supply voltage: 32 @ recommended battery voltage (variant 2) Protections: Over Current (OC) Protection Protections: Over Voltage (OV) Protection @ (variant 2) Protections: Under Voltage (UV) Protection @ (variant 3) Data interface: UART @ (variant 3) Data interface: RS-422 @ (variant 4) Envelope (L×W×H): 92 mm x 88.9 mm x 19.9 to 28.9 mm ## NanoPower P80 — GomSpace [eps] https://newspacemarket.com/products/nanopower-p80/ Output rails: Vbat, 3.3V, 5V, 12V, 18V Protections: Software and hardware Latch-up Protection (LUP), software low voltage protection Supply voltage: 28.8 (nominal) @ Operating voltage Supply voltage: 33.6 (max) @ Operating voltage Power consumption: 0.5 W @ Idle power consumption, All features enabled (PMU) Power consumption: 0.45 W @ Idle power consumption, All channels disabled (PDU) Power consumption: 0.3 W @ Idle power consumption, All features enabled (ACU) Data interface: CAN Data interface: I2C @ (variant 2) Operating temperature: -40 °C (min) Operating temperature: 85 °C (max) Conversion efficiency: 80 (min) @ Output voltage of 3.3 V Conversion efficiency: 80 (min) @ Output voltage of 5 V Conversion efficiency: 80 (min) @ Output voltage of 12 V Output power (total): 300 W Envelope (L×W×H): 95 mm x 95 mm x 38.8 mm Envelope (L×W×H): 95 mm x 95 mm x 65 mm @ (variant 2) Mass: 360.8 g Mass: 619.6 g @ (variant 2) ## CELESTE GNSS Receiver — Spacemanic s.r.o. [gnss-receivers] https://newspacemarket.com/products/spacemanic-celeste-gnss-receiver/ Position accuracy: 5 m Constellations: GPS, GLONASS, Galileo and BeiDou Flight heritage: Flight heritage on 10+ nanostellite missions (e.g. LASARsat, CroCube, GRBBeta, Planetum-1 and external customers) and launchers. Operating temperature: -40-85 °C Envelope (L×W×H): 67x42x7.5 mm Supply voltage: 3.3 Supply voltage: 5 @ (variant 2) Mass: 25 g Power consumption: 0.25 W @ average Time to first fix (cold): 1 s @ Hot Time to first fix (cold): 28 s @ Warm Time to first fix (cold): 29 s @ Cold Time to first fix (cold): 29 s Data interface: I2C Data interface: RS485 @ (variant 2) Data interface: CAN @ (variant 3) Data interface: UART @ (variant 4) Connector: MMCX antenna connector Connector: Molex SlimStack 55650-0688 @ (variant 2) ## Gemini GPS/GNSS Receivers — NewSpace Systems (NSS) [gnss-receivers] https://newspacemarket.com/products/nss-gemini-gnss-receivers/ Flight heritage: > 10 years Position accuracy: 2 m @ 1 sigma, GEMINI-SR5 Position accuracy: 1.5 m @ 1 sigma, GEMINI-MR28 Velocity accuracy: 0.1 m/s @ 1 sigma, GEMINI-SR5 Velocity accuracy: 0.05 m/s @ 1 sigma, GEMINI-MR28 Update rate: 20 Hz @ Up to, GEMINI-SR5 Update rate: 20 Hz @ Up to, GEMINI-MR28 Constellations: L1 (1575.42 MHz) @ GEMINI-SR5 Constellations: GPS L1/L2C, GALILEO E1/E5b, QZSS, BDS B1I/B2I, GLONASS L1/L2 @ GEMINI-MR28 Time to first fix (cold): 50 s @ GEMINI-SR5 Time to first fix (cold): 50 s @ GEMINI-MR28 Envelope (L×W×H): 96 mm x 91 mm x 18 mm @ GEMINI-SR5 Envelope (L×W×H): 155 mm x 31 mm x 76 mm @ GEMINI-MR28 Mass: 154 g (max) @ GEMINI-SR5 Mass: 383 g (max) @ GEMINI-MR28 Power consumption: 0.5 W @ Nominal, excluding active antenna, GEMINI-SR5 Power consumption: 2 W @ Nominal, excluding active antenna, GEMINI-MR28 Operating temperature: -25 °C (min) @ GEMINI-SR5 Operating temperature: 70 °C (max) @ GEMINI-SR5 Operating temperature: -25 °C (min) @ GEMINI-MR28 Operating temperature: 70 °C (max) @ GEMINI-MR28 Radiation tolerance (TID): 30 krad @ Component level, GEMINI-SR5 Radiation tolerance (TID): 30 krad @ Component level, GEMINI-MR28 Supply voltage: 5 @ GEMINI-SR5 Supply voltage: 28 @ GEMINI-MR28 Data interface: RS-422 @ GEMINI-SR5 Data interface: RS-422 @ GEMINI-MR28 Connector: 2 x SMA Female (antenna), 15-pin Nano-D @ GEMINI-SR5 Connector: 2x SMA Female (antenna), Male D-Sub standard density 9-pin and female D-Sub standard density 9-pin @ GEMINI-MR28 ## LEORIX GNSS Receiver — Beyond Gravity (ex-RUAG Space) [gnss-receivers] https://newspacemarket.com/products/beyond-gravity-leorix-gnss-receiver/ Position accuracy: 1 m @ 3d rms Velocity accuracy: 2 m/s @ 3d rms Time to first fix (cold): 90 s @ Warm start Time to first fix (cold): 900 s @ Cold start GPS Time to first fix (cold): 2400 s @ Cold start GALILEO Constellations: GPS C/A on L1, Galileo E1 B/C Mass: 3000 g @ Electronic box Envelope (L×W×H): 280x240x81 mm Power consumption: 15 W @ avg. Operating temperature: -30 °C (min) Operating temperature: 60 °C (max) Operating temperature: -40 °C (min) @ Minimum switch-on temperature Flight heritage: SWARM (ESA), Sentinel-1, Sentinel-2 and Sentinel-3 A/B satellites (Copernicus), Sentinel-1, Sentinel-2 and Sentinel-3 C/D, Sentinel-6/Michael Freilich A/B (NASA/ESA), Earthcare (ESA/JAXA), ICESat-2 (NASA), PACE (NASA), OSAM-1 (NASA), Biomass (ESA), FLEX ( Supply voltage: 28 ## NavRIX Integral GNSS Receiver — Beyond Gravity (ex-RUAG Space) [gnss-receivers] https://newspacemarket.com/products/beyond-gravity-navrix-integral-gnss-receiver/ Position accuracy: 1 m (max) @ 3D rms Velocity accuracy: 25 m/s (max) @ 3D rms Time to first fix (cold): 150 s (max) @ Warm start (90%) Time to first fix (cold): 270 s (max) @ Cold start (90%) Constellations: GPS L1 C/A, Galileo E1 B/C Power consumption: 1 W (max) @ additional power consumption Flight heritage: SWARM (ESA), Sentinel-1, Sentinel-2 and Sentinel-3 A/B (Copernicus), Sentinel-1, Sentinel-2 and Sentinel-3 C/D, Sentinel-6/Michael Freilich A/B (NASA/ESA), EarthCare (ESA/JAXA), ICESat-2 (NASA), PACE (NASA), OSAM-1 (NASA), Biomass (ESA), FLEX (ESA), KOMPS Mass: 216 g ## EMXYS Ground Station — Emxys [ground-stations] https://newspacemarket.com/products/emxys-ground-station/ Supply voltage: 220 Operating temperature: -20 °C Operating temperature: -40 °C @ (variant 2) Power consumption: 60 W Survival temperature: -40 °C Frequency band: UHF @ TX Frequency band: UHF @ RX Frequency band: VHF @ RX (variant 2) Frequency band: S @ RX (variant 3) Frequency: 400 MHz (min) @ TX Frequency: 480 MHz (max) @ TX Frequency: 3500 MHz (max) @ RX Mass: 50000 g Envelope (L×W×H): 82 cm x 54 cm x 50 cm Data interface: Ethernet Data interface: USB @ (variant 2) Connector: RJ45 Connector: USB2.0 @ (variant 2) Connector: USB3.0 @ (variant 3) Connector: HDMI @ (variant 4) Connector: D-Sub 9 @ (variant 5) Connector: N-type @ (variant 6) Connector: NAC3MPA @ (variant 7) Connector: XLR @ (variant 8) ## Satellite Ground Stations Network — Swedish Space Corporation (SSC) [ground-stations] https://newspacemarket.com/products/ssc-global-ground-station-network/ Envelope (L×W×H): 3-13 m Envelope (L×W×H): 7-13 m @ (variant 2) Envelope (L×W×H): 5-13 m @ (variant 3) Envelope (L×W×H): 13 m @ (variant 4) Frequency band: S @ RX Frequency band: X @ RX (variant 2) Frequency band: Ka @ RX (variant 3) Frequency band: S @ TX Frequency band: Ku @ RX (variant 4) Frequency band: X @ TX (variant 2) Frequency band: Ku @ TX (variant 3) Frequency band: C @ RX (variant 5) Frequency band: L @ RX (variant 6) Frequency band: DBS @ RX (variant 7) Frequency band: C @ TX (variant 4) Frequency band: DBS @ TX (variant 5) Antenna diameter: 3 m (min) Antenna diameter: 32 m (max) ## NanoCom GS100 — GomSpace [ground-stations] https://newspacemarket.com/products/nanocom-gs100/ Power consumption: 25 W Frequency: 430 MHz (min) @ GS100U Frequency: 440 MHz (max) @ GS100U Frequency: 395 MHz (min) @ GS100UL Frequency: 405 MHz (max) @ GS100UL Frequency: 143 MHz (min) @ GS100V Frequency: 150 MHz (max) @ GS100V Supply voltage: 12 ## NanoCom GS2000 — GomSpace [ground-stations] https://newspacemarket.com/products/nanocom-gs2000/ Frequency band: S @ transceiver Frequency: 2025-2110 MHz @ transmitter Frequency: 2200-2290 MHz @ receiver EIRP: 6 dBW @ output power at RF connector Data rate: 500-2000 kbps @ bit data rate, transmitter Data rate: 500-2000 kbps @ bit data rate, receiver Data rate: 1510 kbps @ Layer-3 UDP throughput (FDD) Data rate: 620 kbps @ Layer-3 UDP throughput (TDD) Mass: 5400 g @ Approx. Envelope (L×W×H): 483 x 304 x 88 mm @ without power supply Supply voltage: 26-30 @ Supply voltage (Absolute Maximum Ratings) Supply voltage: 26-30 @ Supply voltage (Electrical Characteristics) Data interface: Ethernet Data interface: USB @ (variant 2) Connector: RF Type N (Rx) Connector: RF Type N (Tx) @ (variant 2) Connector: RJ45 @ Ethernet Connector: USB 2.0 Standard B @ USB to PC Connector: Hirose LF10WBR-4S @ 5 V OUT Operating temperature: 0-35 °C Survival temperature: -40-85 °C Power consumption: 25 W ## PG400 Gyroscope — AAC Clyde Space [imus-gyros] https://newspacemarket.com/products/aac-pg400-gyroscope/ Angle random walk: 0.23 Bias instability: 1 °/h Envelope (L×W×H): 30.8 x 25.7 x 17mm Data interface: RS-422 Gyro range: 125 (max) Supply voltage: 3.65 (min) Supply voltage: 5.5 (max) Operating temperature: -40 °C (min) Operating temperature: 85 °C (max) Flight heritage: successfully-flown on orbit and it based on the design heritage of the internal IMU used in our reliable and flight proven attitude determination and control system iADCS solutions. TRL: 9 Lead time: 16 Power consumption: 0.28 W ## ASTRIX 1090 Inertial Measurement / Accelerometer Unit — Airbus Defence and Space [imus-gyros] https://newspacemarket.com/products/airbus-astrix-1090/ Radiation tolerance (TID): 100 krad Design lifetime: 15 years Mass: 4500 g Envelope (L×W×H): ø 263 x h 192mm footprint Power consumption: 13.5 W Data interface: MIL-STD-1553 Data interface: RS-422 @ (variant 2) Gyro range: 20 @ Full performance measurement range Gyro range: 140 @ Measurement range Bias instability: 0.01 °/h @ Stability over 1 hour Bias instability: 0.3 °/h @ Thermal sensitivity (over 15°C) Bias instability: 0.09 °/h @ Repeatability after launch environment Bias instability: 0.3 °/h @ Stability end-of life (all effects included) Angle random walk: 0.005 Flight heritage: 3+ million flight hours Supply voltage: 22-50 ## Agile Actuators (CMG 15-45S, 40-60S, 75-75S) — Airbus Defence and Space [imus-gyros] https://newspacemarket.com/products/airbus-cmg-75-75s/ Operating temperature: -20 °C Design lifetime: 10 years @ LEO Mass: 69000 g @ per CMG Envelope (L×W×H): mechanism 550mm x 500mm x 570mm Envelope (L×W×H): electronics 390mm x 250mm x 175mm @ per box for 2 CMG channels Power consumption: 57 W @ quasi-static, @75Nms per CMG Power consumption: 145 W @ max maneuver per CMG Flight heritage: Airbus CMG products have cumulated over 1 millon hours on orbit, without failure ## HMR2300 3-Axis Magnetometer — Honeywell Aerospace [magnetometers] https://newspacemarket.com/products/honeywell-hmr2300-smart-digital-magnetometer/ Resolution: 0.1 nT (max) Measurement range: 200 µT @ Full Scale (FS), Total Field Applied Mass: 28 g @ PCB Only Mass: 98 g @ PCB and Flanged Enclosure Supply voltage: 6.5 (min) @ Pin 9 referenced to Pin 5 (Ground) Supply voltage: 15 (max) @ Pin 9 referenced to Pin 5 (Ground) Data interface: RS-232 Data interface: RS-485 @ (variant 2) Operating temperature: -40 °C (min) @ Ambient Operating temperature: 85 °C (max) @ Ambient Survival temperature: -55 °C (min) @ Ambient, Unbiased Survival temperature: 125 °C (max) @ Ambient, Unbiased ## HMC2003 3-Axis Magnetometer — Honeywell Aerospace [magnetometers] https://newspacemarket.com/products/honeywell-hmc2003-3-axis-magnetic-sensor-hybrid/ Measurement range: 200 µT (max) Update rate: 1000 Hz Supply voltage: 6 (min) Supply voltage: 15 (max) Operating temperature: -40 °C (min) Operating temperature: 85 °C (max) Survival temperature: -55 °C (min) Survival temperature: 125 °C (max) Resolution: 40 nT ## DMAG Digital Magnetometer — Lusospace [magnetometers] https://newspacemarket.com/products/lusospace-dmag-digital-magnetometer/ Measurement range: 65 µT (max) Resolution: 20 nT (max) Update rate: 50 Hz (max) Mass: 300 g (max) Envelope (L×W×H): 112x72x33 mm (excl. connectors) Supply voltage: 28 (nominal) Supply voltage: 5 (nominal) @ (variant 2) Power consumption: 1.5 W (max) Data interface: RS-485 Data interface: RS-422 @ (variant 2) Operating temperature: -40 °C (min) Operating temperature: 70 °C (max) Survival temperature: -50 °C (min) Survival temperature: 80 °C (max) Radiation tolerance (TID): 50 krad TRL: 8 Noise density: 20 nT (max) ## MAG28 Analogue Magnetometer — Lusospace [magnetometers] https://newspacemarket.com/products/lusospace-mag28-analogue-magnetometer/ Measurement range: 70 µT (max) Noise density: 40 nT (max) Update rate: 50 Hz (max) Mass: 300 g Supply voltage: 15 (min) Supply voltage: 40 (max) Power consumption: 1 W (max) Operating temperature: -30 °C (min) Operating temperature: 60 °C (max) Survival temperature: -40 °C (min) Survival temperature: 70 °C (max) Radiation tolerance (TID): 50 krad Envelope (L×W×H): 85x53x60 mm (excl. connectors) ## MACM Attitude Control Magnetometer — Magson GmbH [magnetometers] https://newspacemarket.com/products/magson-macm/ Supply voltage: 16 (min) Supply voltage: 40 (max) Power consumption: 0.86 W @ nominal (in earth field @28V) Measurement range: 120 µT (max) Operating temperature: -20 °C (min) Operating temperature: 60 °C (max) Survival temperature: -30 °C (min) Survival temperature: 75 °C (max) Envelope (L×W×H): 138 mm x 55 mm x 39 mm Mass: 249 g Data interface: RS-485 Resolution: 228.88 nT Noise density: 200 nT (max) Flight heritage: Multiple ESA/DLR/university small-sat missions incl. BIROS and TET; 13 launched satellite projects ## MAG-3 — AAC Clyde Space [magnetometers] https://newspacemarket.com/products/aac-mag-3/ Measurement range: 100 µT @ ±10 Volts Analog Output Measurement range: 60 µT @ ±5 Volts Analog Output Supply voltage: 15 (min) Supply voltage: 34 (max) Supply voltage: 5 (nominal) @ Regulated Connector: 9 Pin Male “D” Type Mass: 100 g Envelope (L×W×H): 3.51 cm x 3.23 cm x 8.26 cm Operating temperature: -55 °C (min) Operating temperature: 85 °C (max) Radiation tolerance (TID): 10 krad (min) Flight heritage: Georgia Tech PROX-1, Bigelow Aerospace Genesis-1 to Naval Research Laboratory missions Resolution: 0.1 nT Noise density: 0.1 nT (max) Power consumption: 0.05 W (max) Survival temperature: -55 °C TRL: 9 Resolution: 0.5 nT (max) ## Mag-03® — Bartington Instruments [magnetometers] https://newspacemarket.com/products/mag-03/ Measurement range: 70 µT (max) Measurement range: 100 µT (max) @ (variant 2) Measurement range: 250 µT (max) @ (variant 3) Measurement range: 500 µT (max) @ (variant 4) Measurement range: 1000 µT (max) @ (variant 5) Supply voltage: 12 (min) Supply voltage: 17 (max) Operating temperature: -20 °C ## Spacemag-Lite® — Bartington Instruments [magnetometers] https://newspacemarket.com/products/spacemag-lite/ Envelope (L×W×H): 20 mm x 20 mm x 20 mm Envelope (L×W×H): 90.2 mm x 95.9 mm @ (variant 2) Measurement range: 60 µT (max) @ Full-scale measuring range Mass: 67 g @ SpaceMag-Lite Mass: 94 g @ SpaceMag-Lite (harness variant) Mass: 42 g @ SpaceMag-Lite Probe Supply voltage: 5 (nominal) Supply voltage: 3.3 (nominal) @ (variant 2) Operating temperature: -40 °C (min) @ continuous Operating temperature: 65 °C (max) @ continuous Operating temperature: -40 °C (min) @ intermittent Operating temperature: 85 °C (max) @ intermittent Survival temperature: -40 °C (min) Survival temperature: 85 °C (max) ## Mag629 — Bartington Instruments [magnetometers] https://newspacemarket.com/products/mag629/ Measurement range: 75 µT (max) Measurement range: 75 µT (max) @ (variant 2) Operating temperature: -40 °C (min) @ continuous Operating temperature: 55 °C (max) @ continuous Operating temperature: 71 °C (max) @ intermittent (5 mins ON, 15 mins OFF) Survival temperature: -62 °C (min) Survival temperature: 85 °C (max) Envelope (L×W×H): 31 x 40 x 40mm @ Sensor Head Envelope (L×W×H): 165 x 42 x 43.4mm @ Electronics Mass: 171 g @ Sensor Head Mass: 202 g @ Electronics Connector: Amphenol D3899926WC98PN @ Sensor Head Connector: Amphenol D3899924WC98SN & Amphenol D3899924WC98PA @ Electronics Supply voltage: 28 (nominal) Supply voltage: 25.2 (min) Supply voltage: 30.8 (max) Envelope (L×W×H): 31 x 40 x 40 mm Envelope (L×W×H): 165 x 42 x 43.4 mm @ (variant 2) ## PSU1 — Bartington Instruments [magnetometers] https://newspacemarket.com/products/psu1/ Envelope (L×W×H): 106 x 60 x 148 mm Mass: 615 g @ (battery included) Operating temperature: 0-50 °C @ continuous Operating temperature: 0-40 °C @ for charging Survival temperature: 5-30 °C @ long term Survival temperature: -10-50 °C @ short term Survival temperature: -20-65 °C @ without batteries ## Mag669® — Bartington Instruments [magnetometers] https://newspacemarket.com/products/mag669/ Measurement range: 75 µT (max) @ Full Scale Measuring Range Envelope (L×W×H): 31 x 40 x 40mm @ Sensor Head Envelope (L×W×H): 55 x 35 x 10mm @ Electronics Supply voltage: 15 (nominal) Mass: 200 g (max) @ Sensor Head Mass: 15 g (max) @ Electronics Connector: Unterminated XL-ETFE wires @ Sensor Head Connector: 2 off Harwin M80-854-10-42 @ Electronics Operating temperature: -55 °C (min) @ continuous Operating temperature: 55 °C (max) @ continuous Operating temperature: -55 °C (min) @ continuous (variant 2) Operating temperature: 55 °C (max) @ continuous (variant 2) Operating temperature: 71 °C (max) @ intermittent (5 mins ON, 15 mins OFF) Survival temperature: -62 °C (min) Survival temperature: 85 °C (max) Envelope (L×W×H): 31 x 40 x 40 mm Envelope (L×W×H): 55 x 35 x 10 mm @ (variant 2) ## Mag613 — Bartington Instruments [magnetometers] https://newspacemarket.com/products/mag613/ Measurement range: 300 µT (max) Measurement range: 500 µT (max) @ (variant 2) Noise density: 0.5 nT @ at 1Hz Operating temperature: -10 °C (min) Operating temperature: 40 °C (max) Survival temperature: -40 °C (min) Survival temperature: 50 °C (max) Envelope (L×W×H): sensor head WxHxL: 8 x 8 x 15mm @ sensor head Envelope (L×W×H): WxHxL: 180 x 140 x 21mm @ Electronics Mass: 1700 g Supply voltage: 18 (min) Supply voltage: 24 (max) Envelope (L×W×H): sensor head WxHxL: 8 x 8 x 15 mm ## MTQ140 magnetorquer — Lusospace [magnetorquers] https://newspacemarket.com/products/lusospace-mtq140-magnetorquer/ TRL: 8 Residual moment: 0.5 A·m² (max) Magnetic dipole moment: 140 A·m² (nominal) Mass: 3800 g (max) Envelope (L×W×H): 620 x 90 x 60 mm Power consumption: 4.5 W (max) Radiation tolerance (TID): 100 krad Flight heritage: Space Rider ## MTQ400 magnetorquer — Lusospace [magnetorquers] https://newspacemarket.com/products/lusospace-mtq400-magnetorquer/ Magnetic dipole moment: 400 A·m² (max) Mass: 7000 g (max) Envelope (L×W×H): 950 x 80 x 80 mm Supply voltage: 28 (max) Power consumption: 15 W (max) Operating temperature: -35 °C (min) Operating temperature: 65 °C (max) Survival temperature: -40 °C (min) Survival temperature: 80 °C (max) Radiation tolerance (TID): 100 krad (max) Residual moment: 0.5 A·m² (max) ## MTQ800 — AAC Clyde Space [magnetorquers] https://newspacemarket.com/products/aac-mtq800/ Radiation tolerance (TID): 10 krad TRL: 9 Magnetic dipole moment: 15 A·m² @ Nominal Magnetic dipole moment: 30 A·m² @ Boost mode Mass: 489 g Data interface: RS-422 Data interface: RS-485 @ (variant 2) Power consumption: 3 W @ nominal dipole moment Flight heritage: The MTQ800 magnetorquer series has been flying on numerous missions since 2020 and is at TRL 9. It is based on the company’s experience in design and development of magnetorquers for CubeSats which have been flying since 2017. Envelope (L×W×H): 250 x 67 x 35 mm @ Torquer rods Envelope (L×W×H): 60 x 70 x 14 mm @ Driver Enclosure Operating temperature: -45 °C (min) Operating temperature: 45 °C (max) Magnetic dipole moment: 15 A·m² @ Design Magnetic dipole moment: 30 A·m² @ Peak Supply voltage: 8 (min) Supply voltage: 12.5 (max) Power consumption: 0.144 W @ Idle (Min) Power consumption: 0.156 W @ Idle (Typ) Power consumption: 0.18 W @ Idle (Max) Power consumption: 1.44 W @ Dipole moment of 10 Am2 (Min) Power consumption: 1.536 W @ Dipole moment of 10 Am2 (Typ) Power consumption: 1.632 W @ Dipole moment of 10 Am2 (Max) Power consumption: 4.8 W @ Dipole moment of 20 Am2 (Min) Power consumption: 5.04 W @ Dipole moment of 20 Am2 (Typ) Power consumption: 5.52 W @ Dipole moment of 20 Am2 (Max) Power consumption: 13.2 W (max) @ Maximum dipole moment ## Sirius OBC LEON3FT Development Kit — AAC Clyde Space [obc-computers] https://newspacemarket.com/products/aac-sirius-tcm-leon3ft-dev-kit/ Processor: 32-bit LEON3FT (IEEE-1754 SPARC v8) fault-tolerant processor CPU clock: 50 MHz RAM: 64 MB Storage: 2 GB @ Nonvolatile System Memory Nand Flash Storage: 32 GB @ Mass Memory Storage Operating system: RTEMS real-time operating system (RTOS) Envelope (L×W×H): 230 x 155 x 37 mm Data interface: SpaceWire Data interface: RS-422 @ (variant 2) Data interface: RS-485 @ (variant 3) Data interface: UART @ (variant 4) Data interface: LVDS @ (variant 5) Data interface: other @ GPIO Data interface: other @ JTAG Connector: Dsub/microD Operating temperature: Room temperature Design lifetime: 5 years Design lifetime: 5 years @ LEO Design lifetime: 5 years @ LEO (variant 2) Mass: 32 g ## Solid-State Recorders, Mass Memories and Payload Data Processing — Airbus Defence and Space [obc-computers] https://newspacemarket.com/products/airbus-nemo-2-2041-solid-state-recorder/ Design lifetime: 10 years @ LEO RAM: 10-14 MB Supply voltage: 22-37 Data interface: LVDS @ Video Inputs Data interface: LVDS @ TMI Data interface: other @ LCT: Wizard Links Data interface: other @ Test: Wizard Links Data interface: MIL-STD-1553 @ Redundant TM/TC links Operating temperature: -10-50 °C @ Operating Survival temperature: -20-60 °C @ Non-operating Design lifetime: 10 years @ LEO radiation compliant Mass: 5000-12000 g Envelope (L×W×H): From 365(L) x 104(W) x 220(H) mm3 to 365(L) x 224 (W) x 220(H) mm3 Power consumption: 60-180 W @ during simultaneous compression and replay Power consumption: 12-72 W @ in standby mode Storage: 4096-12288 GB @ User capacity Flight heritage: in flight since 2021 ## Q8 On-Board Computer — Xiphos Technologies [obc-computers] https://newspacemarket.com/products/xiphos-q8-obc/ Radiation tolerance (TID): 30 krad Flight heritage: TRL9 product built around the Q8 processor board, which has hundreds of years of flight heritage across over 100 missions. Flight heritage: Xiphos has been flying Q-Cards since 2002. @ (variant 2) Processor: AMD/Xilinx UltraScale+ MPSoC processor Data interface: RS-422 Data interface: RS-485 @ (variant 2) Data interface: CAN @ (variant 3) Data interface: LVDS @ (variant 4) Data interface: Ethernet @ (variant 5) Data interface: USB @ (variant 6) Operating system: Linux Data interface: Ethernet @ (variant 7) Data interface: USB @ (variant 8) Data interface: CAN @ (variant 9) Data interface: UART @ (variant 10) Data interface: RS-422 @ (variant 11) Data interface: RS-485 @ (variant 12) Data interface: other @ (variant 13) Data interface: LVDS @ (variant 14) Supply voltage: 9 (nominal) Power consumption: 7.5 W @ nominal Power consumption: 14 W @ peak Envelope (L×W×H): 167.3 mm x 182.6 mm x 91 mm Mass: 957 g Operating temperature: -40-60 °C Storage: 2 GB ## Robust On-Board Data Handling Unit (OBC) — S4 – Smart Small Satellite Systems GmbH [obc-computers] https://newspacemarket.com/products/s4-robust-obdh-onboard-computer/ Supply voltage: 3.3 Supply voltage: 3.3-9 Mass: 38 g Envelope (L×W×H): 90 x 90 x 6.9 mm RAM: 2 MB RAM: 2 MB @ (variant 2) CPU clock: 1-24 MHz Storage: 2 GB RAM: 32768 MB (max) Power consumption: 0.015 W @ nominal Flight heritage: uninterrupted operations in orbit since 2013 launch Processor: 1-24 MHz ## CAVU OBC-1 — CAVU Aerospace [obc-computers] https://newspacemarket.com/products/obc-1-on-board-computer/ Processor: ARM Cortex-M3 on FPGA Processor: Microchip/Microsemi SmartFuion2 Flash Based FPGA @ (variant 2) CPU clock: 128 MHz RAM: 10 MB @ 80Mbits MRAM RAM: 6 MB @ 48Mbits MRAM (Configurable as Triple 16Mbits) Storage: 96 GB @ SLC NAND Flash (Triple 32G) Mass: 75 g Envelope (L×W×H): 160x100mm Supply voltage: 5 (nominal) Power consumption: 1 W @ min Power consumption: 2 W @ max Data interface: CAN Data interface: RS-422 @ (variant 2) Data interface: RS-485 @ (variant 3) Data interface: RS232 @ (variant 4) Data interface: I2C @ (variant 5) Data interface: SPI @ (variant 6) Operating temperature: -40 °C (min) Operating temperature: 85 °C (max) Radiation tolerance (TID): 30 krad Design lifetime: 3 years (min) @ in LEO Design lifetime: 5 years (max) @ in LEO Operating system: 30Krad (Si)/yr ## Payload Data Handling System VPDHS — VECTRONIC Aerospace GmbH [obc-computers] https://newspacemarket.com/products/vectronic-vpdhs/ RAM: 4096 MB Storage: 16 GB Envelope (L×W×H): 290 mm x 192 mm x 34 mm Mass: 2300 g Power consumption: 15 W @ Max Supply voltage: 9-18 Supply voltage: 18-36 @ (variant 2) Data interface: RS-422 Data interface: RS-485 @ (variant 2) Connector: MDM-25 Operating temperature: -20-70 °C Survival temperature: -40-80 °C Radiation tolerance (TID): 10 krad Data interface: LVDS @ (variant 3) Random vibration: 13.4 ## Antelope Advanced Data Processing Unit — KP Labs [obc-computers] https://newspacemarket.com/products/kp-labs-antelope-dpu/ Envelope (L×W×H): 13.24 x 95.9 x 90.1 mm Processor: Zynq UltraScale+ MPSoC ZU2EG/ZU3EG/ZU4EG/ZU5EG: Quad ARM Cortex-A53 CPU CPU clock: 1500 MHz Processor: Dual ARM Cortex-R5 @ (variant 2) RAM: 8192 MB Storage: 4 GB Operating system: 64-bit Linux Data interface: CAN Data interface: I2C @ (variant 2) Data interface: other @ (variant 3) Data interface: SPI @ (variant 4) Data interface: RS422/485 @ (variant 5) Data interface: UART @ (variant 6) Data interface: other @ (variant 7) Data interface: LVDS @ (variant 8) Data interface: other @ (variant 9) Data interface: USB @ (variant 10) Data interface: USB @ (variant 11) Data interface: Ethernet @ (variant 12) Data interface: other @ (variant 13) Supply voltage: 5.5-14 Supply voltage: 5 Operating temperature: -40-85 °C Flight heritage: LEO for 8 weeks without failures or errors ## Sirius QuadCore — AAC Clyde Space [obc-computers] https://newspacemarket.com/products/aac-sirius-quadcore-leon4ft/ Processor: LEON4 quad core fault-tolerant processor CPU clock: 250 MHz RAM: 4096 MB Storage: 0.002 GB Storage: 0.25 GB @ (variant 2) Operating system: Linux Operating system: RTEMS @ (variant 2) Mass: 100 g @ ~ Envelope (L×W×H): 100 x 100 x 15 mm Supply voltage: 5-12 Power consumption: 4 W @ Normal Power Consumption Data interface: SpaceWire Data interface: CAN @ (variant 2) Data interface: other @ (variant 3) Data interface: UART @ (variant 4) Data interface: SPI @ (variant 5) Data interface: other @ (variant 6) Operating temperature: -30-60 °C Radiation tolerance (TID): 20 krad Design lifetime: 5-7 years TRL: 8 ## Q7S — AAC Clyde Space [obc-computers] https://newspacemarket.com/products/aac-q7s/ Radiation tolerance (TID): 20 krad TRL: 9 Flight heritage: >15 missions Processor: ARM® dual-­core Cortex™-­A9 MPCore processors CPU clock: 766 MHz (max) RAM: 512 MB RAM: 256 MB @ (variant 2) Storage: 32 GB (max) @ MicroSD storage_mb: 64 @ QSPI Flash (NOR) Operating system: Linux 3.10+ Operating system: RTEMS @ optional Mass: 24 g @ without connectors Mass: 32 g @ with RJ45 connector Envelope (L×W×H): 78 mm x 43 mm x 9 mm @ without connectors Envelope (L×W×H): 78 mm x 43 mm x 19 mm @ with RJ45 connector Supply voltage: 6-28 Power consumption: 1 W @ typical Data interface: Ethernet Data interface: USB @ (variant 2) Data interface: RS-232 @ (variant 3) Data interface: RS-422 @ (variant 4) Data interface: RS-485 @ (variant 5) Data interface: LVDS @ (variant 6) Connector: RJ45 Connector: Micro-AB @ USB 2.0 Operating temperature: -40-85 °C ## Q8J Data Storage and Interface Board — Xiphos Technologies [obc-computers] https://newspacemarket.com/products/xiphos-q8j-dsib/ Mass: 260 g @ DSIB + Q8J + mounting HW Storage: 1000 GB @ TLC mode Data interface: Ethernet @ 4x GigE (1Gbps) ports Data interface: CAN @ 2x CAN bus controllers Data interface: RS-422 @ 7x RS422 ports Data interface: RS-485 @ 1x RS485 Data interface: RS-422 @ 1x RS422/RS485 (full or half-duplex, factory-configured) Data interface: RS-485 @ 1x RS422/RS485 (full or half-duplex, factory-configured) (variant 2) Data interface: LVDS @ 16x LVDS outputs Data interface: LVDS @ 12x LVDS inputs Data interface: LVDS @ 4x factory-configured LVDS I/Os Operating system: Yocto Linux BSP (LTS distribution) Operating temperature: -40-60 °C Supply voltage: 11.4-12.6 Power consumption: 12 W @ typical with all interfaces active and 1 SSD Radiation tolerance (TID): 30 krad CPU clock: 300 MHz (min) Envelope (L×W×H): 90 x 190 x 25 mm ## Fortis™ VPX — Sidus Space, Inc. [obc-computers] https://newspacemarket.com/products/sidus-space-fortis-vpx/ Power consumption: 330 W Processor: NVIDIA® Jetson AGX Orin™ Industrial RAM: 8192 MB Storage: 0.5 GB Storage: 4096 GB @ (variant 2) Supply voltage: 28 (nominal) Data interface: LVDS Data interface: Ethernet @ (variant 2) Data interface: USB @ (variant 3) Data interface: UART @ (variant 4) Data interface: other @ PWM Data interface: SPI @ (variant 5) Data interface: I2C @ (variant 6) Operating temperature: -55 °C (min) Operating temperature: 125 °C (max) Envelope (L×W×H): 3U OpenVPX Operating system: Linux-based Radiation tolerance (TID): 100 krad ## Motherboard Module 2 (MBM2) — Pumpkin, Inc. [obc-computers] https://newspacemarket.com/products/pumpkin-mbm2/ Processor: 1 GHz ARM Cortex-A8 (BeagleBone Black) Operating system: Custom Linux-based image Operating system: Pumpkin's flight software (FSW) SupMCU service @ (variant 2) Data interface: Ethernet Data interface: USB @ (variant 2) Data interface: UART @ (variant 3) Data interface: SPI @ (variant 4) Data interface: I2C @ (variant 5) Data interface: GPIO @ (variant 6) Data interface: RS-422 @ (variant 7) Data interface: LVTTL UART/SPI/GPIO @ (variant 8) Data interface: analog input @ (variant 9) Mass: 34 g Envelope (L×W×H): 96mm W x 90mm L ## Motherboard Module (MBM) — Pumpkin, Inc. [obc-computers] https://newspacemarket.com/products/pumpkin-motherboard-module-mbm/ Mass: 77 g @ With standoff and fastener hardware to accept a short PPM (e.g., PPM A1) mounted 9mm above the M Mass: 88 g @ With PPM A1 mounted using abovementioned hardware Mass: 103 g @ With PPM A1 mounted using abovementioned hardware, 10mm CubeSat Kit Bus Connector extenders and Mass: 11.4 g (max) @ Without PPM, MHX transceiver or 10mm CubeSat Kit Bus Connector extenders fitted Envelope (L×W×H): 90 @ PCB length Envelope (L×W×H): 96 @ PCB width Envelope (L×W×H): 1.6 @ PCB thickness Envelope (L×W×H): 12.5 (max) @ Height of components above PCB with PPM fitted, and without MHX transceiver or 10mm CubeSat Kit Envelope (L×W×H): 24.5 (max) @ Height of components above PCB with MHX transceiver and 10mm CubeSat Kit Bus Connector extender Envelope (L×W×H): 3.5 (max) @ Height of components below PCB Supply voltage: 1.65-5.5 @ I/O voltage for all on-board peripherals except RTC and SD Card interface Supply voltage: 2.7-5.5 @ RTC Supply voltage: 3.3 @ SD Card interface Storage: 0.0313 GB @ SD/MMC card Storage: 2 GB @ SD/MMC card (variant 2) Operating temperature: -40-85 °C Processor: PPM A1, PPM A2, PPM A3, PPM B1, PPM D1, PPM D2, PPM E1 ## MA61C CubeSat — Space Products and Innovation (SPiN) [obc-computers] https://newspacemarket.com/products/ma61c-cubesat/ Processor: GR712RC dual-core LEON3 fault-tolerant SPARC V8 CPU clock: 50 MHz RAM: 64 MB @ SRAM RAM: 3072 MB @ SDRAM Storage: 0.0625 GB @ FLASH Envelope (L×W×H): 95.89mm x 90.17mm Mass: 150 g Data interface: SpaceWire Data interface: CAN @ (variant 2) Data interface: I2C @ (variant 3) Data interface: SPI @ (variant 4) Data interface: UART @ (variant 5) Data interface: RS-422 @ (variant 6) Data interface: RS-485 @ (variant 7) Data interface: USB @ Debug Port Operating system: USB (API + Windows GUI included) Flight heritage: TRL 9 - flown on SPiN-1 CubeSat (launched 25 May 2022) and ATMOS Space Cargo PHOENIX 1 (launched 22 April 2025) Operating temperature: -40 °C ## MA61C SmallSat — Space Products and Innovation (SPiN) [obc-computers] https://newspacemarket.com/products/ma61c-smallsat/ Operating system: USB (API + Windows GUI included) Processor: GR712RC dual-core 32-bit LEON3 fault-tolerant SPARC V8 processor CPU clock: 50 MHz RAM: 8 MB Storage: 0.0625 GB Mass: 435 g @ approx. Envelope (L×W×H): 131 mm x 131 mm x 30 mm @ with casing Supply voltage: 5-24 Data interface: SpaceWire Data interface: CAN @ (variant 2) Data interface: I2C @ (variant 3) Data interface: SPI @ (variant 4) Data interface: RS-422 @ (variant 5) Data interface: RS-485 @ (variant 6) Data interface: other @ Debug port Data interface: MIL-STD-1553 @ (variant 7) Data interface: JTAG @ (variant 8) Connector: micro-d 9 pins female @ SpaceWire Connector: dsub9 male @ CAN-bus Connector: dsub9 male @ MIL-STD-1553B Connector: mdm-25 female @ RS422 and RS485 Connector: mdm-37 male @ GPIO, Analogues Connector: dsub-9 @ power and JTAG Connector: mdm-15 male @ I2C Master, SPI master, PWM Operating temperature: -40-85 °C ## MA61C cPCI — Space Products and Innovation (SPiN) [obc-computers] https://newspacemarket.com/products/ma61c-cpci/ Processor: GR712RC dual-core LEON3 fault-tolerant SPARC V8 CPU clock: 50 MHz RAM: 10 MB Storage: 0.0078 GB Envelope (L×W×H): 160mm x 100mm Mass: 300 g Data interface: SpaceWire Data interface: CAN @ (variant 2) Data interface: I2C @ (variant 3) Data interface: RS-232 @ (variant 4) Data interface: RS-422 @ (variant 5) Data interface: other @ (variant 6) Data interface: other @ (variant 7) Connector: MDM-25 Female Connector: Micro-D 9 Female @ (variant 2) Operating system: USB (API + Windows GUI included) Operating temperature: -40 °C ## CDH-110 — Berlin Space Technologies [obc-computers] https://newspacemarket.com/products/cdh-110-command-data-handling-system/ Envelope (L×W×H): 176x94x69 mm³ Flight heritage: since 2015 Mass: 815 g Power consumption: 2 W (max) Design lifetime: 5 years Radiation tolerance (TID): 20 krad ## CAVU CDH-FS — CAVU Aerospace [obc-computers] https://newspacemarket.com/products/cdh-fs-fault-safe-cdh/ Processor: ARM Cortex-M3 on FPGA Processor: Microchip/Microsemi SmartFuion2 Flash Based FPGA @ (variant 2) Processor: Microsemi ProASIC3 Flash Based FPGA for Interaface @ (variant 3) Processor: FPU on FPGA Upon Request @ (variant 4) Processor: 150 DMIPS @ 128 MHz @ (variant 5) Processor: SoftConsole/Keil Programming and Debug via JTAG @ (variant 6) RAM: 0.25 MB RAM: 256 MB @ (variant 2) Operating system: 30Krad (Si)/yr Envelope (L×W×H): 205x203x87 mm Power consumption: 3 W Flight heritage: Flight proven onboard computer for number of satellite projects Mass: 4300 g Radiation tolerance (TID): 30 krad ## Remote Terminal Unit (RTU) — Beyond Gravity (ex-RUAG Space) [obc-computers] https://newspacemarket.com/products/beyond-gravity-remote-terminal-unit-rtu/ Data interface: MIL-STD-1553 @ OBC connection Power consumption: 15 W @ standby only acquisitions, Type A Power consumption: 15 W @ standby only acquisitions, Type B Mass: 16600 g @ Type A Mass: 15400 g @ Type B (10 modules) Mass: 17000 g @ Type B (12 modules) Design lifetime: 15 years @ Type A Design lifetime: 15 years @ Type B Envelope (L×W×H): 392 x 242 x 277 mm @ Type A Envelope (L×W×H): 446 x 212 x 250 mm @ Type B (10 modules) Envelope (L×W×H): 467 x 212 x 250 mm @ Type B (12 modules) Flight heritage: EDRS-C, MTG, ExoMars Rover, Hispasat 36W-1, SARah, Electra, Euclid, Gaia, Galileo, Solar Orbiter, Sentinel-2, EarthCARE, Sentinel-6, JUICE, Metop SG Supply voltage: 22-37 ## NanoMind HP MK3 — GomSpace [obc-computers] https://newspacemarket.com/products/nanomind-hp-mk3/ Processor: Xilinx Zynq 7030/7045 Programmable SoC (Dual ARM Cortex A9 MPCore) CPU clock: 800 MHz (max) RAM: 1024 MB Storage: 70 GB @ eMMC (pSLC) Storage: 233 GB @ eMMC (MLC) Storage: 0.25 GB @ NOR flash Mass: 240 g @ typical Envelope (L×W×H): 95 x 95 x 24,15 mm Supply voltage: 12-32 Power consumption: 1.8 W @ Idle, Vin = 12V, 25°C Power consumption: 1.854 W @ Idle, Vin = 18V, 25°C Power consumption: 1.92 W @ Idle, Vin = 24V, 25°C Power consumption: 2.08 W @ Idle, Vin = 32V, 25°C Data interface: SpaceWire Data interface: USB @ (variant 2) Data interface: CAN @ (variant 3) Data interface: RS-422 @ (variant 4) Data interface: I2C @ (variant 5) Data interface: LVDS @ (variant 6) Data interface: RS-485 @ (variant 7) Operating temperature: -40-50 °C Survival temperature: -40-85 °C Radiation tolerance (TID): 20 krad ## COBRA-HPX Gimbal — Tethers Unlimited, Inc. (AMERGINT) [pointing-mechanisms] https://newspacemarket.com/products/tethers-unlimited-cobra-hpx-gimbal/ Mass: 450 g Power consumption: 7 W @ Operational Power consumption: 4 W (max) @ Standby Radiation tolerance (TID): 50 krad @ Gimbal Mechanism Radiation tolerance (TID): 15 krad @ Commander Angular resolution: 0.0767 deg (min) ## APPMAX2 Electric Propulsion Pointing Mechanism — Beyond Gravity (ex-RUAG Space) [pointing-mechanisms] https://newspacemarket.com/products/beyond-gravity-appmax2-pointing-mechanism/ Power consumption: 1-5 W Travel range: 15 Angular resolution: 0.1 deg (max) @ Repeatability Mass: 13800 g @ APPMAX2 Mass Envelope (L×W×H): 486x484x281 @ LxWxH ## PureLine Topaz/THORs — Airbus Defence and Space [propulsion] https://newspacemarket.com/products/airbus-pureline-topaz-thors-ppu/ Thrust: 200 mN Design lifetime: 10 years @ LEO Mass: 10000 g Specific impulse: 1300 Power consumption: 300 W Supply voltage: 27-38 Propulsion type: electric Propellant: Xenon Design lifetime: 10 years @ in LEO Data interface: CAN Data interface: RS-422 @ (variant 2) Data interface: MIL-STD-1553 @ (variant 3) ## Nanosatellite Mono & Bipropellant Propulsion Thruster — Stellar Exploration, Inc. [propulsion] https://newspacemarket.com/products/nanosatellite-mono-bipropellant-propulsion-thruster/ Propellant: Gear pumps for precise propellant metering, low-pressure tank design Propellant: Hypergolic bipropellant; monopropellant variants also available @ (variant 2) Flight heritage: NASA CAPSTONE (12U lunar mission), EchoStar EG-3 (small-satellite delta-V record) Propulsion type: chemical @ bipropellant Specific impulse: 285 @ bipropellant Propulsion type: chemical @ monopropellant Specific impulse: 200 @ monopropellant Thrust: 3000 mN ## Aurora Resistojet Module for Orbit Control (ARM-O) — Aurora Propulsion Technologies [propulsion] https://newspacemarket.com/products/aurora-arm-c/ Flight heritage: IOD 2026 Propulsion type: electric Propellant: water ## MONARC Monopropellant Thrusters — Moog Space Defense Group [propulsion] https://newspacemarket.com/products/moog-space-propulsion/ Export status: Equipment described herein falls under the jurisdiction of the EAR and may require US Government Authorization for export purposes. Diversion contrary to US law is prohibited. Flight heritage: Galileo, Sentinel, SMAP, Mars 2020, Jason-CS, MMS, EarthCare, LCROSS, Worldview, Skynet, ExoMars, SWOT, GOES, Landsat-8, Chandra Propulsion type: chemical @ Steady State Thrust @ 260 psia Thrust: 100 mN @ Steady State Thrust @ 260 psia Propulsion type: chemical Feed/tank pressure: 4.8 bar Propulsion type: chemical @ (variant 2) Feed/tank pressure: 27.6 bar @ (variant 2) Propulsion type: chemical @ Valve Power Power consumption: 58 W @ Valve Power Propulsion type: chemical @ (variant 3) Mass: 1.6 g Propulsion type: chemical @ Engine Length/Exit Diam Envelope (L×W×H): 16 in (41 cm) / 5.8 in (14.8 cm) @ Engine Length/Exit Diam Propulsion type: chemical @ Nominal Specific Impulse Specific impulse: 235 @ Nominal Specific Impulse Propulsion type: chemical @ (variant 4) Propellant: hydrazine ## HYDROS® Thruster — Tethers Unlimited, Inc. (AMERGINT) [propulsion] https://newspacemarket.com/products/tethers-unlimited-hydros-m-thruster/ Specific impulse: 310 (min) Power consumption: 5-25 W Total impulse: 2151 N·s (min) Specific impulse: 310 (min) @ (variant 2) Power consumption: 7-40 W @ (variant 2) Total impulse: 18000 N·s (min) @ (variant 2) Propulsion type: hybrid Flight heritage: Proven capability on-orbit Thrust: 1200 mN (min) Thrust: 1200 mN (min) @ (variant 2) ## SPS-40 Propulsion System — Space Electric Thruster Systems (SETS) [propulsion] https://newspacemarket.com/products/sets-sps-40-propulsion-system/ Power consumption: 300-600 W TRL: 9 Propulsion type: electric Propellant: Xenon, Krypton Power at thrust: 300 W (min) @ Total power consumption Power at thrust: 600 W (max) @ Total power consumption Thrust: 31 mN (max) Specific impulse: 1650 (max) Total impulse: 300000 N·s (max) @ one thruster configuration Mass: 9000 g (max) @ Dry mass (without tank) ## ST-100 Hall Thruster — Space Electric Thruster Systems (SETS) [propulsion] https://newspacemarket.com/products/sets-st-100-hall-effect-thruster/ Power consumption: 800-1500 W TRL: 6 Propulsion type: electric Thrust: 95 mN (max) Thrust: 50 mN (min) Thrust: 95 mN (max) @ (variant 2) Specific impulse: 1400 (min) Specific impulse: 1900 (max) Propellant: Xenon Propellant: Krypton @ (variant 2) Mass: 3000 g @ including two cathodes Envelope (L×W×H): 215 × 143.5 × 110 Power at thrust: 800 W (min) Power at thrust: 1500 W (max) ## ST-40 Hall Thruster — Space Electric Thruster Systems (SETS) [propulsion] https://newspacemarket.com/products/sets-st-40-hall-effect-thruster/ Power consumption: 250-600 W Power consumption: 250-600 W @ (variant 2) TRL: 9 Propulsion type: electric Thrust: 36 mN (max) Thrust: 13 mN (min) Thrust: 36 mN (max) @ (variant 2) Specific impulse: 1000 (min) Specific impulse: 1750 (max) Total impulse: 300000 N·s (max) Propellant: Xenon Propellant: Krypton @ (variant 2) Power at thrust: 250 W (min) @ total power consumption Power at thrust: 600 W (max) @ total power consumption Mass: 1400 g @ including two cathodes Envelope (L×W×H): 156 x 130 x 105 ## ST-25 Hall Thruster — Space Electric Thruster Systems (SETS) [propulsion] https://newspacemarket.com/products/sets-st-25-hall-effect-thruster/ TRL: 9 Propulsion type: electric Propellant: Xenon, Krypton Power consumption: 100 W (min) @ total power consumption Power consumption: 250 W (max) @ total power consumption Thrust: 5 mN (min) Thrust: 15 mN (max) Specific impulse: 950 (min) Specific impulse: 1500 (max) Total impulse: 75000 N·s (max) Mass: 1000 g @ including two cathodes Envelope (L×W×H): 123 x 101 x 72.5 ## SPS-25 Propulsion System — Space Electric Thruster Systems (SETS) [propulsion] https://newspacemarket.com/products/sets-sps-25-propulsion-system/ Power consumption: 120-275 W Flight heritage: Flown on EOS SAT-1 satellite TRL: 9 Propulsion type: electric Power at thrust: 120 W @ min Power at thrust: 275 W @ max Thrust: 14 mN (max) Specific impulse: 1500 (max) Total impulse: 75000 N·s (max) @ one thruster configuration Propellant: Xenon Propellant: Krypton @ (variant 2) Mass: 5000 g (max) @ Dry mass (without tank) ## T5 Ion Thruster — QinetiQ Space [propulsion] https://newspacemarket.com/products/qinetiq-t5-ion-thruster/ Flight heritage: ESA GOCE (2009–2013) Power consumption: 700 W Propulsion type: electric Thrust: 1-20 mN @ atmospheric drag compensation Propellant: xenon Envelope (L×W×H): 10cm diameter ## Pocket Rocket Vacuum Arc Thruster — Solid State Propulsion [propulsion] https://newspacemarket.com/products/solid-state-propulsion-vacuum-arc-thruster/ Specific impulse: 700 Propellant: Unpressurised solid metal cathode (vacuum arc, no moving parts) Propulsion type: electric Flight heritage: First 2x units sold, launching on Transporter 12 Flight heritage: First Flight Q4 2024 @ (variant 2) Envelope (L×W×H): 45x45x25mm Thrust: 0.2 mN (max) Total impulse: 8 N·s Mass: 85 g @ wet Supply voltage: 5 @ Power Supply voltage: 3.3 @ Logic Power consumption: 0.5 W (min) @ Input Power consumption: 20 W (max) @ Input Connector: Samtec LSHM-110-02.5 Lead time: 2.5 ## HALO THRUSTERS — ExoTerra Resource [propulsion] https://newspacemarket.com/products/exoterra-halo-8/ Power consumption: 100-450 W Power consumption: 100-300 W @ (variant 2) Power consumption: 250-1650 W @ (variant 3) TRL: 5 Power consumption: 375-1650 W @ (variant 4) TRL: 5 @ (variant 2) Propulsion type: electric Propulsion type: electric @ (variant 2) Propulsion type: electric @ (variant 3) Mass: 850 g Power at thrust: 100-450 W Specific impulse: 600-1400 Thrust: 4-30 mN Total impulse: 400000 N·s Propellant: Xenon Mass: 850 g @ (variant 2) Envelope (L×W×H): 80 mm diameter by 75 mm long envelope Flight heritage: First flight hardware was delivered in 2022 and launched June 2023. Multiple Halo systems are currently in orbit. ## Integrated Propulsion System (IPS) — VACCO Industries [propulsion] https://newspacemarket.com/products/vacco-integrated-propulsion-system/ Flight heritage: 56 units successfully flown since 2010 Propulsion type: chemical Thrust: 1000 mN @ throttlable min Thrust: 3970 mN @ throttlable max net axial Total impulse: 12000 N·s Propellant: LMP-103S Feed/tank pressure: 22 bar @ MEOP Mass: 9000 g @ dry Mass: 14700 g @ wet Supply voltage: 12 (nominal) @ Safe Power Input Power consumption: 24 W @ Safe Power Input max Supply voltage: 28 (nominal) @ Arm Input Power Power consumption: 50 W @ Arm Input Power max Data interface: RS-422 Operating temperature: 10 °C (min) Operating temperature: 40 °C (max) Survival temperature: -34 °C (min) Survival temperature: 40 °C (max) Power consumption: 1 W @ communication and health monitoring Power consumption: 50 W @ peak power ## VACCO JPL MarCO Micro Propulsion System — VACCO Industries [propulsion] https://newspacemarket.com/products/vacco-jpl-marco-micro-propulsion/ Power consumption: 0.5 W Propulsion type: cold-gas Total impulse: 755 N·s Propellant: R236fa Mass: 3490 g @ wet mass Thrust: 25 mN @ axial and RCS thrusters Data interface: RS-422 Min impulse bit: 0.5 mN·s Supply voltage: 9-12.6 Operating temperature: -30-55 °C Time to thrust: 20 s (max) @ Thruster valve response time ## Air-Scooping Electric Thruster (ASET) — Air-Breathing VLEO Propulsion — Viridian Space [propulsion] https://newspacemarket.com/products/viridian-space-aset-air-breathing-vleo-propulsion/ Power consumption: 50-550 W Propulsion type: electric Propellant: atmospheric gas Propellant: oxygen @ (variant 2) Propellant: nitrogen @ (variant 3) Propellant: air @ (variant 4) ## TRINITY HET Hall Effect Thruster — Blue Orbit Space Systems [propulsion] https://newspacemarket.com/products/blue-orbit-trinity-het-hall-effect-thruster/ Specific impulse: 1100 (max) Total impulse: 1500000 N·s (max) Propulsion type: electric Propellant: Argon, Nitrogen Mass: 2500 g @ inc. Thruster and Cathode Envelope (L×W×H): 90 x 85 x 115 mm Power consumption: 800-1200 W @ Nominal Input Power consumption: 1500 W @ Operational Power Range Thrust: 100 mN (max) ## TRINIT-ION Gridded Ion Thruster — Blue Orbit Space Systems [propulsion] https://newspacemarket.com/products/blue-orbit-trinit-ion-gridded-ion-thruster/ Total impulse: 2000000 N·s (max) Propulsion type: electric Propellant: Argon, Nitrogen Mass: 2500 g @ inc. Thruster and Cathode Envelope (L×W×H): 90 x 85 x 115 mm Power at thrust: 800 W @ Nominal Input Power Power at thrust: 1200 W @ Nominal Input Power (variant 2) Power consumption: 1500 W @ Operational Power Range Thrust: 50 mN (max) Specific impulse: 2500 (max) ## TRINITY ABE Air Breathing Thruster — Blue Orbit Space Systems [propulsion] https://newspacemarket.com/products/blue-orbit-trinity-abe-air-breathing-thruster/ Total impulse: 1500000 N·s (max) Propellant: Argon, Nitrogen Mass: 2500 g Envelope (L×W×H): 90 x 85 x 115 mm Power consumption: 800-1200 W @ Nominal Input Power Power consumption: 1500 W @ Operational Power Range Thrust: 20 mN (max) Specific impulse: 2000 (max) ## Blue Orbit Water Resistojet — Blue Orbit Space Systems [propulsion] https://newspacemarket.com/products/blue-orbit-water-resistojet/ Mass: 270 g Power consumption: 10-18 W Mass: 250 g @ (variant 2) Power consumption: 80 W Propulsion type: electric Propellant: Water Propellant mass: 270 g Envelope (L×W×H): 55 x 33 x 122 mm Power at thrust: 10-18 W Thrust: 3.3-4.4 mN Specific impulse: 103-108 ## AIS-gPPT3-1C Series Integrated Propulsion Module — Applied Ion Systems [propulsion] https://newspacemarket.com/products/applied-ion-systems-ais-gppt3-1c/ Mass: 34 g Propellant mass: 50-99 g Propellant: Teflon Power consumption: 0.5 W Propellant: 50-99 mg (estimate) @ (variant 2) Min impulse bit: 0.0007 mN·s (min) Total impulse: 325 N·s TRL: 7 Propulsion type: electric Envelope (L×W×H): 40mm x 38mm x 24mm Supply voltage: 3.3 (nominal) @ main power Supply voltage: 3.3 (nominal) @ thruster module powered via Arduino Uno Thrust: 0.0002 mN ## PPU-1500 (Power Processing Unit) — Space Electric Thruster Systems (SETS) [propulsion] https://newspacemarket.com/products/sets-ppu-1500/ Operating temperature: -35-80 °C Power consumption: 800-1500 W TRL: 4 Supply voltage: 80-140 @ Input Voltage Data interface: CAN @ Communication Data interface: RS-485 @ Communication (variant 2) Data interface: MIL-1553B @ optional, Communication Data interface: Ethernet @ optional, Communication (variant 2) Power at thrust: 800-1500 W @ Discharge Power, Anode Power Supply Radiation tolerance (TID): 30 krad @ Radiation tolerance (COTS) ## PPU-500 (Power Processing Unit) — Space Electric Thruster Systems (SETS) [propulsion] https://newspacemarket.com/products/sets-ppu-500/ Operating temperature: -35-80 °C Propulsion type: electric Power at thrust: 500 W (max) Supply voltage: 24-36 @ Unregulated Data interface: CAN Data interface: RS-485 @ (variant 2) Data interface: Ethernet @ optional Radiation tolerance (TID): 30 krad @ COTS Flight heritage: Successful flight heritage ## PPU-200 (Power Processing Unit) — Space Electric Thruster Systems (SETS) [propulsion] https://newspacemarket.com/products/sets-ppu-200/ TRL: 9 Supply voltage: 28 (nominal) @ Unregulated Supply voltage: 26 (min) @ Input Supply voltage: 36 (max) @ Input Power consumption: 230 W (max) @ Discharge Power Supply Data interface: RS-485 Data interface: CAN @ (variant 2) Radiation tolerance (TID): 30 krad (max) Envelope (L×W×H): 218 x 124 x 102 @ with connectors Flight heritage: flight heritage ## Multi-Modal Electric Propulsion Engine (MEPE) — Aurora Propulsion Technologies [propulsion] https://newspacemarket.com/products/aurora-mepe/ Propellant: Green (non-toxic) Flight heritage: IOD launched 2023 (ORB-12 STRIDER) Propellant: ~ 1 kg @ (variant 2) Envelope (L×W×H): 125 x 220 x 220 mm3 Mass: 5000 g @ wet Propellant mass: 1000 g Thrust: 3 mN @ MUSIC Specific impulse: 1000 @ MUSIC Power at thrust: 100 W @ MUSIC Thrust: 1 mN @ ARM (per thruster) Specific impulse: 40 @ ARM Power at thrust: 4 W @ ARM (per thruster) Data interface: RS422 Total impulse: 10000 N·s ## BHT-200 — Busek Co. [propulsion] https://newspacemarket.com/products/busek-bht-200-hall-effect-thruster/ Power consumption: 200 W Propulsion type: electric Power at thrust: 200 W @ Discharge Power Supply voltage: 250 Thrust: 13 mN Specific impulse: 1390 Propellant: Xenon, Iodine Mass: 980 g @ Thruster Mass Mass: 120 g @ Cathode Mass Total impulse: 74880 N·s @ Demonstrated Impulse Total impulse: 140000 N·s (min) @ Predicted Total Impulse Flight heritage: TacSat-2, FalconSat-5, FalconSat-6 ## BHT-350 — Busek Co. [propulsion] https://newspacemarket.com/products/busek-bht-350-hall-effect-thruster/ Power consumption: 350 W Propulsion type: electric @ Hall Effect Thruster Power at thrust: 300 W @ Nominal Discharge Power Power at thrust: 200 W (min) @ Throttle Range Power at thrust: 600 W (max) @ Throttle Range Thrust: 17 mN @ Nominal Specific impulse: 1244 @ Nominal Propellant: Xenon Propellant: Krypton @ (variant 2) Propellant: Iodine @ (variant 3) Mass: 1700 g @ Thruster Mass Mass: 200 g @ Cathode Mass Total impulse: 212000 N·s @ Demonstrated Total impulse: 250000 N·s (min) @ Predicted Total Impulse ## BGT-X5 — Busek Co. [propulsion] https://newspacemarket.com/products/busek-bgt-x5-green-monopropellant-thruster/ Power consumption: 20 W Propulsion type: chemical Thrust: 500 mN @ nominal Total impulse: 565 N·s Thrust: 500 mN @ nominal (variant 2) Specific impulse: 220 (min) Specific impulse: 225 (max) Feed/tank pressure: 27.579 bar Min impulse bit: 50 mN·s Data interface: RS-485 Supply voltage: 6 (min) Supply voltage: 16 (max) Supply voltage: 12 @ nominal Data interface: RS-485 @ (variant 2) Envelope (L×W×H): 10x10x10cm @ external Mass: 1500 g @ BOL Propellant: ASCENT Feed/tank pressure: 31.0264 bar @ (variant 2) Thrust: 500 mN @ nominal (variant 3) Specific impulse: 220 (min) @ (variant 2) Specific impulse: 225 (max) @ (variant 2) Min impulse bit: 50 mN·s @ (variant 2) Total impulse: 565 N·s @ (variant 2) ## BHT-20K — Busek Co. [propulsion] https://newspacemarket.com/products/busek-bht-20k-hall-thruster/ Power consumption: 20000 W Total impulse: 35 N·s (min) Propulsion type: electric Thrust: 1000 mN @ 1 Newton Thrust: 1006 mN @ Nominal Specific impulse: 2515 @ Nominal Propellant: Xenon Propellant: Krypton @ (variant 2) Propellant: Iodine @ (variant 3) Propellant mass: 1000000 g (min) @ estimated throughput Power at thrust: 20000 W @ Discharge Power Power at thrust: 5000 W @ throttling range Power at thrust: 22000 W @ throttling range max Mass: 45000 g @ Assembly Mass Supply voltage: 450 @ Nominal Supply voltage: 700 (max) @ discharge potentials ## BHT-600 — Busek Co. [propulsion] https://newspacemarket.com/products/busek-bht-600-hall-thruster/ Total impulse: 1.5 N·s (min) Propulsion type: electric @ Hall Effect Thruster Power at thrust: 600 W @ Discharge Power Power consumption: 300 W (min) @ Throttle Range Power consumption: 800 W (max) @ Throttle Range Thrust: 39 mN @ Nominal Thrust Specific impulse: 1300 (min) @ Nominal Specific Impulse Specific impulse: 1500 (max) @ Nominal Specific Impulse Propellant: Xenon Propellant: Krypton @ (variant 2) Propellant: Iodine @ (variant 3) Mass: 2600 g @ Thruster Mass ## BHT-6000 — Busek Co. [propulsion] https://newspacemarket.com/products/busek-bht-6000-hall-thruster/ Power consumption: 5000 W Power consumption: 6000 W @ (variant 2) Total impulse: 8.5 N·s (min) Power consumption: 2-6 W Propulsion type: electric Mass: 13500 g @ Assembly Mass Propellant: Xenon Propellant: Krypton @ (variant 2) Power at thrust: 5000 W @ High Thrust Mode Supply voltage: 300 @ High Thrust Mode Thrust: 320 mN @ High Thrust Mode Specific impulse: 1900 @ High Thrust Mode Power at thrust: 6000 W @ High Impulse Mode Supply voltage: 600 @ High Impulse Mode Thrust: 288 mN @ High Impulse Mode Specific impulse: 2600 @ High Impulse Mode ## Rogue — Magdrive [propulsion] https://newspacemarket.com/products/magdrive-rogue/ Propellant: 2.5 kg Power consumption: 2-100 W Total impulse: 3000 N·s (min) Mass: 3000 g Propulsion type: electric @ ECO Propulsion type: electric @ SPORT Thrust: 4000 mN @ ECO Thrust: 10000 mN @ SPORT Specific impulse: 4500 @ ECO Specific impulse: 1800 @ SPORT Power at thrust: 150 W @ ECO Power at thrust: 150 W @ SPORT Envelope (L×W×H): 20 10 10 ## FireStar Foundation Drive — Miles Space / RocketStar [propulsion] https://newspacemarket.com/products/miles-space-firestar-foundation-drive/ Thrust: 2.9 mN Thrust: 17.6 mN @ (variant 2) Propellant: H2O (filled as liquid; liquid or solid during storage/use) Envelope (L×W×H): 95 x 95 x 95 mm (1U with 5 mm margin) Mass: 980 g Propellant: 250 grams of liquid, pure water @ (variant 2) Survival temperature: -40 °C Specific impulse: 7300 Total impulse: 17800 N·s Propulsion type: electric @ fusion-enhanced pulsed plasma ## VACCO ArgoMoon MiPS — VACCO Industries [propulsion] https://newspacemarket.com/products/vacco-argomoon-micro-propulsion-system/ Propellant mass: 420 g Propulsion type: chemical @ green thruster Propulsion type: cold-gas @ cold gas thrusters Thrust: 100 mN @ green thruster Total impulse: 783 N·s @ green thruster Thrust: 25 mN @ cold gas thrusters Total impulse: 72 N·s @ cold gas thrusters Propellant: 420 @ propellant Propellant: 215 @ pressurant Propellant: LMP-103S & R134a Feed/tank pressure: 16.8 bar @ MDP Total impulse: 72 N·s @ cold gas @10°C Total impulse: 783 N·s @ green @10°C Mass: 1430 g (max) @ Dry Mass Mass: 2065 g (max) @ Wet Mass 95% Fill @ 10°C Supply voltage: 9-12.6 @ Operating Voltage For Telemetry Supply voltage: 9-12.6 @ Operating Voltage For Heaters & Valves Power consumption: 1 W (max) @ Standby Power Power consumption: 20 W (max) @ Warmup Power Power consumption: 4.3 W (max) @ Thruster Operating Power Data interface: RS-422 Operating temperature: 10-40 °C Survival temperature: -34-60 °C Power consumption: 1 W @ <, for health and status monitoring Envelope (L×W×H): 92.8 (3.652) x 122.2 (4.812) x 143.5 (5.648) mm ## Multipurpose Satellite Platform — Beyond Gravity (ex-RUAG Space) [propulsion] https://newspacemarket.com/products/beyond-gravity-multipurpose-satellite-platform/ Mass: 150000-250000 g Propulsion type: electric @ Electric Propulsion Design lifetime: 7 years @ in Low Earth Orbit (LEO) ## EPSylon — OHB Sweden AB [propulsion] https://newspacemarket.com/products/epsylon/ Thrust: 8 mN Mass: 15000-20000 g Propulsion type: electric Propellant: Xe Propellant: Kr @ Under qualification Supply voltage: 28 @ Unregulated Supply voltage: 70 @ Unregulated (variant 2) ## NanoCom AX2150 S-Band Transceiver — GomSpace [radios] https://newspacemarket.com/products/gomspace-nanocom-ax2150-transceiver/ Supply voltage: 5 Data interface: UART @ Debug UART Data interface: UART @ KISS UART Data interface: CAN Data interface: I2C @ (variant 2) Frequency band: S ## Cubesat UHF/VHF Radio — Aphelion Orbitals [radios] https://newspacemarket.com/products/cubesat-uhf-vhf-radio-3474/ Frequency: 143-146 MHz Frequency: 430-438 MHz @ (variant 2) Mass: 72 g Envelope (L×W×H): 95.9mm X 90.1mm X 15mm Frequency band: UHF @ downlink Frequency band: VHF @ uplink Modulation: OOK, FSK, GFSK Power consumption: 0.18 W @ receive only Power consumption: 3.1 W @ transmitting TX power: 1.995 W RX sensitivity: -118 Data rate: 1.2 kbps Data rate: 2.4 kbps @ (variant 2) Data rate: 4.8 kbps @ (variant 3) Data rate: 9.6 kbps @ (variant 4) Supply voltage: 3.3 (nominal) Data interface: UART Connector: 50 ohm MMCX connectors ## LYNX-X-band and LYNX-Ka-band Transmitters — NewSpace Systems (NSS) [radios] https://newspacemarket.com/products/nss-lynx-x-band-transmitter/ Modulation: Variable and adaptive coding and modulation Frequency band: X @ TX (LYNX-X) Frequency band: Ka @ TX (LYNX-Ka) Frequency: 8025-8400 MHz @ TX (LYNX-X) Frequency: 25500-27000 MHz @ TX (LYNX-Ka) TX power: 0.5-2 W @ Adjustable (LYNX-X) TX power: 0.5-2 W @ Adjustable (LYNX-Ka) Data rate: 400000 kbps @ TX (LYNX-X) Data rate: 1000000 kbps @ TX (LYNX-Ka) Mass: 450 g (max) @ LYNX-X Mass: 450 g (max) @ LYNX-Ka Envelope (L×W×H): 150 mm × 120 mm × 30 mm @ LYNX-X Envelope (L×W×H): 150 mm × 120 mm × 30 mm @ LYNX-Ka Supply voltage: 9-34 @ LYNX-X Supply voltage: 9-34 @ LYNX-Ka Power consumption: 25 W (max) @ LYNX-X Power consumption: 25 W (max) @ LYNX-Ka Data interface: Ethernet @ LYNX-X Data interface: SpaceWire @ LYNX-X (variant 2) Data interface: Ethernet @ LYNX-Ka Data interface: SpaceWire @ LYNX-Ka (variant 2) Data interface: RS-485 @ Control and Telemetry (LYNX-X) Data interface: CAN @ Control and Telemetry (LYNX-X) (variant 2) Data interface: RS-485 @ Control and Telemetry (LYNX-Ka) Data interface: CAN @ Control and Telemetry (LYNX-Ka) (variant 2) Connector: 25-way female Micro-D @ LYNX-X Connector: 25-way female Micro-D @ LYNX-Ka Operating temperature: -35-65 °C @ LYNX-X Operating temperature: -35-65 °C @ LYNX-Ka Survival temperature: -40-85 °C @ X-Band TX Radiation tolerance (TID): 30 krad @ component level (LYNX-X) Radiation tolerance (TID): 30 krad @ component level (LYNX-Ka) Design lifetime: 10 years (max) @ LEO missions ## LYNX X-band / Ka-band Transmitter — NewSpace Systems (NSS) [radios] https://newspacemarket.com/products/nss-lynx-ka-band-transmitter/ Modulation: Variable and adaptive coding and modulation Frequency band: X @ TX Frequency band: Ka @ TX (variant 2) Frequency: 8025 MHz (min) @ X-Band Transmitter Frequency: 8400 MHz (max) @ X-Band Transmitter Frequency: 25500 MHz (min) @ Ka-Band Transmitter Frequency: 27000 MHz (max) @ Ka-Band Transmitter TX power: 0.5 W (min) @ Adjustable TX power: 2 W (max) @ Adjustable Data rate: 400000 kbps @ LYNX-X Transmitter Data rate: 1000000 kbps @ LYNX-KA Transmitter Mass: 450 g (max) @ LYNX-X/Ka Transmitter Envelope (L×W×H): 150 mm × 120 mm × 30 mm @ LYNX-X Transmitter Envelope (L×W×H): 150 mm × 120 mm × 30 mm @ LYNX-KA Transmitter Power consumption: 25 W (max) @ LYNX-X/Ka Transmitter Supply voltage: 9 (min) Supply voltage: 34 (max) Data interface: Ethernet @ LYNX-X/Ka Transmitter Data interface: SpaceWire @ LYNX-X/Ka Transmitter (variant 2) Data interface: RS-485 @ Control and Telemetry Data interface: CAN @ Control and Telemetry (variant 2) Connector: 25-way female Micro-D @ LYNX-X Transmitter Connector: 25-way female Micro-D @ LYNX-KA Transmitter Operating temperature: -35 °C (min) Operating temperature: 65 °C (max) Survival temperature: -40 °C (min) @ X-Band TX Survival temperature: 85 °C (max) @ X-Band TX Radiation tolerance (TID): 30 krad Design lifetime: 10 years @ suitable for LEO missions ## X-Band Transmitter — Plan-S (Connecta) [radios] https://newspacemarket.com/products/x-band-transmitter-4217/ Frequency: 8025-8400 MHz Supply voltage: 10.5-28 Operating temperature: -20 °C Frequency band: X TX power: 1.995 W (max) @ configurable Modulation: QPSK, 8PSK, 16APSK, 32APSK Envelope (L×W×H): 126 x 128 x 42.5 mm @ Main Envelope (L×W×H): 82.5 x 90 x 25 mm @ PA Power consumption: 32 W @ Full Transmit Mode Data interface: Ethernet Data interface: other @ SERDES Data interface: LVDS @ (variant 2) Data interface: CAN @ (variant 3) Flight heritage: demonstrated on 1 Satellite ## Pulsar-UTRX — AAC Clyde Space [radios] https://newspacemarket.com/products/aac-pulsar-utrx/ Operating temperature: -25-61 °C Frequency: 400-420 MHz Frequency: 430-440 MHz @ (variant 2) Frequency band: UHF @ UHF uplink & downlink TX power: 0.501 W Data rate: 9.6 kbps @ GMSK Data rate: 1.2 kbps @ AFSK RX sensitivity: -115 @ for 12 dB SINAD Modulation: GMSK Modulation: AFSK @ (variant 2) Mass: 100 g (max) Envelope (L×W×H): 96 mm x 90 mm x 16.51 mm Supply voltage: 3.3 Power consumption: 3 W @ Transmit DC Power Power consumption: 0.24 W (max) @ Receive DC Power Data interface: I2C ## TRX-U — AAC Clyde Space [radios] https://newspacemarket.com/products/aac-trx-u/ Radiation tolerance (TID): 10 krad TRL: 9 Frequency band: UHF @ Uplink & Downlink Frequency: 370-470 MHz TX power: 0.25-5 W Data rate: 2.4-19.2 kbps @ Transmit Data rate: 2.4-19.2 kbps @ Receive RX sensitivity: -113 @ @ 9600 bps RX sensitivity: -108 @ @ 19.2 Kbps Modulation: FSK, GFSK Mass: 125 g Envelope (L×W×H): 83 mm x 57 mm x 16 mm Supply voltage: 3.3-42 Power consumption: 0.23 W @ RX Power consumption: 8 W @ TX: for >5W RF Output with 6V Input Data interface: other @ Clock and Data Output Connector: 15 Pin Micro-D Socket @ Power and Data Connector: MCX Socket @ RF Operating temperature: -35-80 °C Survival temperature: -35-80 °C Flight heritage: Space Qualified (Multiple Units On Orbit) Flight heritage: in use by clients around the world. They have been deployed on orbit in various configurations for two decades of successful operations. @ (variant 2) ## THPR1060 — Triad RF Systems [radios] https://newspacemarket.com/products/triad-rf-thpr1060/ Power consumption: 120 W Frequency band: S @ TX and RX Frequency: 2200 MHz (min) Frequency: 2500 MHz (max) TX power: 120 W @ overall TX power: 30 W @ per channel TX power: 50 W (min) @ per MIMO stream, 5 Mbps TX power: 10 W (min) @ per MIMO stream, 20+ Mbps Supply voltage: 22 (min) Supply voltage: 32 (max) Data interface: USB Data interface: RS232 @ (variant 2) Data interface: Ethernet @ (variant 3) Connector: TNC-F @ Antenna RF Connectors Connector: 801-011-07M10-2PA @ DC Connector Connector: 801-011-07M13-37PA @ Signal Connector Operating temperature: -40 °C (min) Operating temperature: 55 °C (max) Envelope (L×W×H): 233.93 x 146.55 x 135.89 Mass: 3912 g ## THPR1070 — Triad RF Systems [radios] https://newspacemarket.com/products/triad-rf-thpr1070/ Power consumption: 80 W Frequency band: C Frequency: 4700-5000 MHz TX power: 80 W @ total TX power: 20 W @ per channel TX power: 20 W @ Per MIMO Stream (5 Mbps) TX power: 5 W @ Per MIMO Stream (20+ Mbps) Envelope (L×W×H): 233.9 x 146.6 x 135.9 @ L x W x H Connector: TNC-F @ Antenna RF Connectors Connector: 801-011-07M10-2PA @ DC Connector Connector: 801-011-07M13-37PA @ Signal Connector Mass: 3912 g Supply voltage: 22-32 @ Input Supply voltage: 22-32 @ Supply Operating temperature: -45-70 °C @ Ambient Data interface: USB @ Internal Microcontroller Data interface: USB @ Radio USB0 Data interface: USB @ Radio USB1 Data interface: USB @ Internal Microntoller USB Data interface: RS232 @ From Radio Data interface: Ethernet ## THPR1076 — Triad RF Systems [radios] https://newspacemarket.com/products/triad-rf-thpr1076/ Power consumption: 40 W Frequency band: L @ TX Frequency: 1140 MHz (min) Frequency: 1450 MHz (max) TX power: 20 W @ Per MIMO Stream (5 Mbps) TX power: 5 W @ Per MIMO Stream (20+ Mbps) Supply voltage: 16 (min) Supply voltage: 32 (max) Envelope (L×W×H): 139.7 x 137.7 x 71.1 mm Mass: 1474 g Operating temperature: -45 °C (min) Operating temperature: 70 °C (max) Data interface: USB Data interface: Ethernet @ (variant 2) Data interface: UART @ RS232 Data interface: RS-485 @ (variant 3) Connector: TNC-F Connector: 801-011-07M10-2PA @ (variant 2) Connector: 801-011-07M13-37PA @ (variant 3) ## THPR1080 — Triad RF Systems [radios] https://newspacemarket.com/products/triad-rf-thpr1080/ Power consumption: 40 W Frequency band: C @ TX and RX Frequency: 4400 MHz (min) Frequency: 5000 MHz (max) TX power: 20 W @ per MIMO Stream (5 Mbps) TX power: 5 W @ per MIMO Stream (20+ Mbps) Envelope (L×W×H): 139.7 x 137.7 x 71.1 Supply voltage: 16 (min) Supply voltage: 32 (max) Data interface: USB Data interface: RS232 @ (variant 2) Data interface: Ethernet @ (variant 3) Connector: TNC-F @ Antenna RF Connectors Connector: 801-011-07M10-2PA @ DC Connector Connector: 801-011-07M13-37PA @ Signal Connector Operating temperature: -45 °C (min) Operating temperature: 70 °C (max) Mass: 1474 g ## Murgas — Spacemanic s.r.o. [radios] https://newspacemarket.com/products/spacemanic-murgas/ Operating temperature: -40 °C Data rate: 0.1-38.4 kbps Envelope (L×W×H): 67x42x7.5 mm Mass: 25 g Supply voltage: 3.3 Supply voltage: 5 @ for CAN Power consumption: 0.14 W @ receiving Power consumption: 3.3 W @ transmitting Modulation: GFSK/GMSK Data interface: I2C Data interface: RS-485 @ (variant 2) Data interface: CAN @ (variant 3) Data interface: UART @ (variant 4) Connector: MMCX, 50 Ω Connector: Molex SlimStack 55650-0688 (on module) @ (variant 2) Connector: Molex PicoLock 503763-0691 (on module) @ (variant 3) Connector: Molex MMCX 73415-1000 (on module) @ (variant 4) Frequency band: VHF @ amateur VHF band RX sensitivity: -100 @ 9600 bps, GFSK, BT = 0.5 Frequency band: UHF @ commercial UHF band RX sensitivity: -100 @ 9600 bps, GFSK, BT = 0.5 (variant 2) Frequency band: UHF @ amateur UHF band RX sensitivity: -100 @ 9600 bps, GFSK, BT = 0.5 (variant 3) Flight heritage: multiple missions (e.g. LASARsat, CroCube, GRBBeta and external customers) ## MCR8 High Performance SCPC Receiver — SpaceBridge Inc. [radios] https://newspacemarket.com/products/mcr8-high-performance-scpc-receiver/ Frequency: 950 MHz Frequency band: L @ RX RX sensitivity: -5 @ Max composite allowed over entire L-band Modulation: DVB-S2X, GSE encapsulation, QPSK up to 256APSK LDPC/BCH Mass: 10900 g Envelope (L×W×H): 17” x 1.72” x 29” W x H x D (435 x 45 x 737 mm) Power consumption: 120 W @ Consumption Data interface: Ethernet @ GbE user data ports Connector: F-type/75 Ω Connector: N-type/50 Ω @ option ## SBTR6030 OEM 3W Ku-Band VSAT Transceiver — SpaceBridge Inc. [radios] https://newspacemarket.com/products/sbtr6030-oem-3w-ku-band-vsat-transceivers/ Power consumption: 3 W Frequency band: Ku @ low band LNB input Frequency: 10700000-11700000 MHz @ LNB RF input, low band Frequency band: Ku @ high band LNB input Frequency: 11700000-12750000 MHz @ LNB RF input, high band Frequency: 950-1950 MHz @ LNB IF output, low band Frequency: 1100-2150 MHz @ LNB IF output, high band Supply voltage: 10-26 @ LNB supply Frequency: 950-1700 MHz @ BUC IF input Frequency band: Ku @ BUC RF output Frequency: 13750000-14500000 MHz @ BUC RF output TX power: 3 W @ BUC operational output at P1dB Supply voltage: 12-30 @ BUC supply Operating temperature: -40-60 °C Connector: F-type (Receptacle) @ 75 Ohm Envelope (L×W×H): 159 x 96.20 x 52 mm @ without Feed Horn Mass: 1600 g @ with Feed Horn ## SBTR003UL 3W Lower Ku-band Transceiver — SpaceBridge Inc. [radios] https://newspacemarket.com/products/sbtr003ul-3w-lower-ku-band-transceiver/ Frequency band: 80 (min) Frequency band: 30 (min) @ (variant 2) Envelope (L×W×H): 217 x 96.8 x 53.5mm Mass: 1095 g Supply voltage: 15-24 Power consumption: 18 W @ Pout = 34dBm, typical Power consumption: 25 W (max) @ Pout = 34dBm Power consumption: 4 W (max) @ 10MHz ref. off Connector: F-type female @ Tx Connector: F-type female @ Rx Operating temperature: -40-55 °C Survival temperature: -40-85 °C Frequency band: Ku @ Rx Frequency: 10700-11700 MHz @ Rx Input frequency Frequency band: Ku @ Tx TX power: 2.818 W @ Tx output power @ P1dB, typical Frequency: 12750-13250 MHz @ Tx output frequency ## NanoCom Link S — GomSpace [radios] https://newspacemarket.com/products/gomspace-nanocom-link-s/ Mass: 112-123 g Power consumption: 15 W (max) Data rate: 7500000 kbps @ S-band Frequency band: S @ TX Frequency: 2200-2290 MHz @ TX Frequency band: S @ RX Frequency: 2025-2110 MHz @ RX TX power: 1.585 W @ adjustable Modulation: BPSK and QPSK Data interface: CAN Data interface: RS-422 @ (variant 2) Data interface: SpaceWire @ (variant 3) Design lifetime: 5 years Survival temperature: -40 °C (min) Survival temperature: 85 °C (max) Supply voltage: 12-32 @ SDR MK3 supply Supply voltage: 8-18 @ ANT2150-DUP supply ## NanoCom Link SX — GomSpace [radios] https://newspacemarket.com/products/gomspace-nanocom-link-sx/ Modulation: BPSK/QPSK, symbol rates 0.5-7.5 MBd Mass: 315 g Power consumption: 7-23 W Data rate: 7500 kbps @ S-band, up to Data rate: 50000 kbps @ X-band, up to Data rate: 150000 kbps @ X-band, up to (variant 2) Data rate: 225000 kbps @ X-band, up to (variant 3) Design lifetime: 5 years (min) Frequency: 2200-2290 MHz @ S-Band Transmit Frequency: 2025-2110 MHz @ S-Band Receiver TX power: 1.585 W @ S-Band, up to Frequency: 8000-8400 MHz @ X-Band Transmit, standard configuration TX power: 1.995 W @ X-Band, standard configuration, up to Frequency: 8020-8280 MHz @ X-Band Transmit, with optional DSN Filter Kit TX power: 1.259 W @ X-Band, with optional DSN Filter Kit, up to Survival temperature: -40 °C (min) Survival temperature: 85 °C (max) Operating temperature: -35 °C (min) @ SDR Thermal Interface Operating temperature: 53 °C (max) @ SDR Thermal Interface Operating temperature: -35 °C (min) @ ANT8250 Thermal Interface Operating temperature: 57 °C (max) @ ANT8250 Thermal Interface Operating temperature: -35 °C (min) @ ANT2150 Thermal Interface Operating temperature: 57 °C (max) @ ANT2150 Thermal Interface Supply voltage: 12-32 @ SDR MK3 supply voltage Supply voltage: 8-18 @ ANT2150-DUP supply voltage Supply voltage: 12-32 @ ANT8250 Frontend supply voltage ## NanoCom Link X — GomSpace [radios] https://newspacemarket.com/products/gomspace-nanocom-link-x/ Frequency band: 500 Mass: 272 g Frequency band: X @ TX Data rate: 50000 kbps @ X-band DVB-S2 standard TX Data rate: 150000 kbps @ X-band DVB-S2 standard TX (variant 2) Data rate: 225000 kbps @ X-band DVB-S2 standard TX (variant 3) Frequency: 8000-8400 MHz @ X-band TX, standard configuration TX power: 1.995 W (max) @ X-band TX, standard configuration Frequency: 8020-8280 MHz @ X-band TX, with optional DSN Filter Kit TX power: 1.259 W (max) @ X-band TX, with optional DSN Filter Kit Modulation: DVB-S2 modulation and coding, MODCOD 1 to 28 @ X-band Supply voltage: 12-32 @ SDR MK3 supply voltage Supply voltage: 12-32 @ ANT8250 Frontend supply voltage Data interface: CAN @ control and telemetry (CSP) Data interface: RS-422 @ low-speed payload data transfer Data interface: SpaceWire @ high-speed payload data transfer Design lifetime: 5 years (min) @ operation in space Survival temperature: -40-85 °C ## NanoCom AX2150 — GomSpace [radios] https://newspacemarket.com/products/gomspace-nanocom-ax2150/ Power consumption: 0.008 W Frequency: 2025-2110 MHz Frequency: 2200-2290 MHz @ (variant 2) TX power: 0.008 W Frequency band: S Flight heritage: NanoCom AX100 product, which has been extensively space proven with a long and successful flight heritage by our customers worldwide since 2014. Radiation tolerance (TID): 20 krad @ ECSS-22900 level E RX sensitivity: 20 (max) @ RX front-end protection Modulation: GFSK/GMSK Data interface: I2C Data interface: UART @ (variant 2) Data interface: CAN @ (variant 3) Data interface: other @ ESD protected UART/GOSH console interface Mass: 32 g (max) @ including aluminum shield ## BR-MOD (Series) — AVCOM of Virginia [radios] https://newspacemarket.com/products/avcom-br-mod-series/ Supply voltage: 25 Frequency band: 10-750 Frequency band: 10-150 @ (variant 2) Operating temperature: -40 °C Survival temperature: -40 °C Connector: SMA RX sensitivity: -100 @ -40 REF LVL Modulation: CW, or BPSK signals (No Demod) @ PEAK FOLLOWING Modulation: Wideband carrier signals (DVB-like) (No Demod) @ CEPT (CARRIER EDGE POWER TRACKING) Data interface: Ethernet Connector: 4-pin Molex @ (variant 2) Data interface: RS-422 @ (variant 2) Connector: 9-pin Molex @ (variant 3) Data interface: RS-232 @ (variant 3) Connector: 9-pin Molex @ (variant 4) Data interface: USB @ (variant 4) Connector: 3-pin Molex @ (variant 5) Power consumption: 3 W (max) Envelope (L×W×H): 3 in. x 3.5 in. x 1.062 in. Mass: 200 g ## EVO-RBR (Rev B) — AVCOM of Virginia [radios] https://newspacemarket.com/products/avcom-evo-rbr/ Frequency band: 10-750 Frequency band: 10-150 @ (variant 2) Frequency: 900 MHz (min) @ Model 2290 Frequency: 2200 MHz (max) @ Model 2290 Frequency: 400 MHz (min) @ Model 3040 Frequency: 3000 MHz (max) @ Model 3040 Frequency: 70 MHz (min) @ Model 6070 Frequency: 6000 MHz (max) @ Model 6070 RX sensitivity: -100 @ RF Sensitivity (-40 REF LVL) Modulation: CW, BPSK (No Demod), CEPT (Carrier-Edge-Power-Track) on DVB (No Demod) Mass: 3270 g Envelope (L×W×H): 48.26 cm x 46.04 cm x 4.37 cm Supply voltage: 15 (nominal) Data interface: Ethernet Data interface: RS-232 @ (variant 2) Data interface: USB @ (variant 3) Connector: SMA Connector: BNC @ (variant 2) Connector: F @ (variant 3) Connector: N @ (variant 4) Connector: RJ45 @ (variant 5) Connector: DB-9 @ (variant 6) Connector: USB-B @ (variant 7) Connector: 6-Pos Terminal Block @ (variant 8) Connector: Barrel Connector Jack @ (variant 9) Operating temperature: 0 °C (min) Operating temperature: 50 °C (max) Survival temperature: -40 °C (min) Survival temperature: 85 °C (max) ## Reation Wheel RWT150 — EXA (Astro-und Feinwerktechnik) [reaction-wheels] https://newspacemarket.com/products/rwt150-reaction-wheel/ Supply voltage: 18-34 Survival temperature: -40 °C Angular momentum storage: 1 N·m·s @ @6000rpm Wheel speed: 6000 (nominal) Wheel speed: 7080 (max) Max torque: 100 mN·m (nominal) Mass: 1500 g (max) Envelope (L×W×H): 150mm*150mm*60mm Operating temperature: -20 °C (min) Operating temperature: 50 °C (max) Design lifetime: 7 years ## MicroWheel 1000 — Microsat Systems Canada [reaction-wheels] https://newspacemarket.com/products/microwheel-1000/ Angular momentum storage: 1.1 N·m·s Max torque: 30 mN·m Mass: 1440 g (max) Envelope (L×W×H): 129 mm × 129 mm × 89 mm Power consumption: 1.5 W (max) @ Idle Power consumption: 9 W (max) @ Steady-state Power consumption: 50 W (max) @ Peak Supply voltage: 28 (nominal) Static imbalance: 0.5 (max) Dynamic imbalance: 0.05 (max) Design lifetime: 7.5 years Radiation tolerance (TID): 25 krad Data interface: RS-422 Data interface: RS-485 @ (variant 2) Flight heritage: Extensive flight history Operating temperature: -24 °C ## MicroWheel 200 — Microsat Systems Canada [reaction-wheels] https://newspacemarket.com/products/microwheel-200/ Supply voltage: 28 Operating temperature: -24 °C Angular momentum storage: 0.18 N·m·s Max torque: 30 mN·m Mass: 940 g (max) @ without rate sensor Mass: 1000 g (max) @ with rate sensor Envelope (L×W×H): 89 mm × 102 mm × 89 mm Power consumption: 1.5 W (max) @ Idle (28 V, +25 °C) without rate sensor Power consumption: 2.5 W (max) @ Idle (28 V, +25 °C) with rate sensor Power consumption: 7 W (max) @ Steady-state (28 V, +25 °C) Power consumption: 50 W (max) @ Peak (28 V, +25 °C) Static imbalance: 0.5 (max) Dynamic imbalance: 0.05 (max) Design lifetime: 7.5 years (min) Radiation tolerance (TID): 25 krad @ at board level, plus > 1 mm shielding Data interface: RS-422 @ Asynchronous Data interface: RS-485 @ Asynchronous (variant 2) Flight heritage: Extensive flight history ## SADM-200 — Comat [sadm] https://newspacemarket.com/products/comat-sadm-1500-solar-array-drive-mechanism/ Random vibration: 20.8 Power transfer: 400 W Wheel speed: 0.1 @ Nominal Wheel speed: 1.3 @ Max Max torque: 350000 mN·m Mass: 465 g Supply voltage: 14 (nominal) Power consumption: 3.5 W @ MAX TORQUE Slip-ring channels: 16 @ Power/Signal tracks Slip-ring channels: 1 @ Ground track Operating temperature: -20-50 °C Survival temperature: -40-60 °C Radiation tolerance (TID): 24 krad (max) Design lifetime: 5 years ## Sx4000 OBP/SDR ASIC — MDA Space [sdr-modems] https://newspacemarket.com/products/sx4000-obp-sdr-asic/ Design lifetime: 15-18 years Protocols / waveforms: DVB-S2X/RCS2 @ compliance Data rate: 10000000 kbps Modulation: BPSK, QPSK, 8PSK, 16 APSK, 32 APSK, 64 APSK, 128 APSK, 256 APSK and VL SNR Data interface: Ethernet @ 5 port Data interface: JESD204C Radiation tolerance (TID): 100 krad Data interface: SPI @ (variant 2) Data interface: UART @ (variant 3) Data interface: I2C @ (variant 4) Data interface: SpaceWire @ (variant 5) Data interface: PCIe @ (variant 6) ## SDR Rack — Alén Space [sdr-modems] https://newspacemarket.com/products/sdr-rack/ Envelope (L×W×H): 3U of 19” rack Frequency: 140-180 MHz @ PA - VHF TX power: 50 W (max) @ PA - VHF TX power: 50.119 W (max) @ PA - VHF (variant 2) Frequency: 400-480 MHz @ PA - UHF TX power: 50 W (max) @ PA - UHF TX power: 50.119 W (max) @ PA - UHF (variant 2) Data interface: USB @ SDR1 Data interface: USB @ SDR2 Supply voltage: 12-13.8 @ Input power supply Supply voltage: 13.8 @ Bias-T output voltage Frequency: 140-180 MHz @ SDR1 - Transmission frequency range - VHF TX power: 50.119 W (max) @ SDR1 - Maximum output power - VHF Frequency: 0.1-1500 MHz @ SDR1 - Reception frequency range - VHF RX sensitivity: 7 (max) @ SDR1 - Maximum input power - VHF Frequency: 400-480 MHz @ SDR1 - Transmission frequency range - UHF TX power: 50.119 W (max) @ SDR1 - Maximum output power - UHF Frequency: 0.1-1500 MHz @ SDR1 - Reception frequency range - UHF RX sensitivity: 7 (max) @ SDR1 - Maximum input power - UHF Frequency: 0.1-3000 MHz @ SDR2 - Reception range - Antenna 3 port RX sensitivity: 7 (max) @ SDR2 - Maximum input power - Antenna 3 port Frequency: 100-3800 MHz @ SDR2 - Transmission frequency range - SDR2 RF Output port TX power: 0.01 W (max) @ SDR2 - Transmission maximum output power (CW) - At 1.7 GHz TX power: 0.001 W @ SDR2 - Transmission maximum output power (CW) - At 2.5 GHz TX power: 0 W @ SDR2 - Transmission maximum output power (CW) - At 3.0 GHz TX power: 0 W @ SDR2 - Transmission maximum output power (CW) - At 3.5 GHz ## TOTEM nanosatellite SDR platform — Alén Space [sdr-modems] https://newspacemarket.com/products/totem-nanosatellite-sdr-platform/ Frequency: 70-6000 MHz Mass: 130 g (max) Supply voltage: 5 Power consumption: 2.65 W @ TX mode Power consumption: 2.25 W @ RX mode Power consumption: 1.4 W @ stand - by mode TX power: 0.005 W @ output Data interface: CAN Data interface: Ethernet @ (variant 2) Data interface: UART @ (variant 3) Data interface: other @ (variant 4) Data interface: I2C @ (variant 5) Flight heritage: flight proven Envelope (L×W×H): 89.3 x 93.3 x 14 mm ## RADIOSAT Software Defined Radio — PicoSaTs [sdr-modems] https://newspacemarket.com/products/picosats-radiosat-software-defined-radio/ Protocols / waveforms: DVB-S2X with ACM and pre-distortion on transmit, CCSDS on receive; optional DVB-RCS2 or custom Data rate: 4000000 kbps (max) @ transmission Data rate: 1000000 kbps (max) @ reception Frequency: 300 MHz (min) Frequency: 7000 MHz (max) Frequency: 300 MHz (min) @ (variant 2) Frequency: 7000 MHz (max) @ (variant 2) Data rate: 4000000 kbps (max) @ TX datarate Data rate: 1000000 kbps (max) @ RX datarate Operating temperature: -20 °C (min) Operating temperature: 70 °C (max) Survival temperature: -30 °C (min) Survival temperature: 90 °C (max) Power consumption: 35 W (max) Supply voltage: 12 (min) Supply voltage: 24 (max) Mass: 500 g (max) ## NanoCom SDR MK3 — GomSpace [sdr-modems] https://newspacemarket.com/products/nanocom-sdr-mk3/ Frequency: 70-6000 MHz @ TR600 Mass: 272 g @ with 1xTR600 (typical) Mass: 306 g @ with 2xTR600 (typical) Mass: 342 g @ with 3xTR600 (typical) Envelope (L×W×H): 95 x 95 x 23,85 @ with 1xTR600 (L x W x H) Envelope (L×W×H): 95 x 95 x 31,65 @ with 2xTR600 (L x W x H) Envelope (L×W×H): 95 x 95 x 31,65 @ with 3xTR600 (L x W x H) Supply voltage: -0.3-36 @ Supply Voltage (Main/Backup) Operating temperature: -40-50 °C @ Thermal interface temperature Survival temperature: -40-85 °C @ Storage Temperature Operating temperature: -40-50 °C @ with three TR600 modules Survival temperature: -40-85 °C @ non-operational Power consumption: 2.22 W @ Supply (Main/Backup), in Idle, Vin = 12V, 25°C Power consumption: 2.25 W @ Supply (Main/Backup), in Idle, Vin = 18V, 25°C Power consumption: 2.4 W @ Supply (Main/Backup), in Idle, Vin = 24V, 25°C Power consumption: 2.56 W @ Supply (Main/Backup), in Idle, Vin = 32V, 25°C Power consumption: 5.46 W @ Supply (Main/Backup), enable one TR600 on Slot A, Vin = 12V, 25°C Power consumption: 5.58 W @ Supply (Main/Backup), enable one TR600 on Slot A, Vin = 18V, 25°C Power consumption: 5.688 W @ Supply (Main/Backup), enable one TR600 on Slot A, Vin = 24V, 25°C Power consumption: 5.888 W @ Supply (Main/Backup), enable one TR600 on Slot A, Vin = 32V, 25°C Power consumption: 7.14 W @ Supply (Main/Backup), enable two TR600 on Slot A and Slot B, Vin = 12V, 25°C Power consumption: 7.164 W @ Supply (Main/Backup), enable two TR600 on Slot A and Slot B, Vin = 18V, 25°C Power consumption: 7.248 W @ Supply (Main/Backup), enable two TR600 on Slot A and Slot B, Vin = 24V, 25°C Power consumption: 7.424 W @ Supply (Main/Backup), enable two TR600 on Slot A and Slot B, Vin = 32V, 25°C Power consumption: 8.76 W @ Supply (Main/Backup), enable three TR600 on Slot A, Slot B and Slot C, Vin = 12V, 25°C Power consumption: 8.73 W @ Supply (Main/Backup), enable three TR600 on Slot A, Slot B and Slot C, Vin = 18V, 25°C Power consumption: 8.784 W @ Supply (Main/Backup), enable three TR600 on Slot A, Slot B and Slot C, Vin = 24V, 25°C Power consumption: 8.96 W @ Supply (Main/Backup), enable three TR600 on Slot A, Slot B and Slot C, Vin = 32V, 25°C Supply voltage: 12-32 @ Supply voltage (Main/Backup) (variant 2) Radiation tolerance (TID): 20 krad ## AX-62 Space Mission Ground Modem — WORK Microwave [sdr-modems] https://newspacemarket.com/products/ax-62-space-mission-ground-modem/ Frequency: 950 MHz (min) @ TX Signal output L-band Frequency: 2150 MHz (max) @ TX Signal output L-band TX power: 0 W (min) TX power: 0.001 W (max) Modulation: BPSK @ CCSDS 231.0 Modulation: QPSK @ CCSDS 231.0 (variant 2) Modulation: QPSK @ DVB-S2X, normal FEC frame Modulation: 8PSK @ DVB-S2X, normal FEC frame (variant 2) Modulation: 16APSK @ DVB-S2X, normal FEC frame (variant 3) Modulation: 32APSK @ DVB-S2X, normal FEC frame (variant 4) Modulation: 64APSK @ DVB-S2X, normal FEC frame (variant 5) Modulation: 128PSK @ DVB-S2X, normal FEC frame (variant 6) Modulation: 256PSK @ DVB-S2X, normal FEC frame (variant 7) Modulation: QPSK @ DVB-S2X, short FEC frame Modulation: 8PSK @ DVB-S2X, short FEC frame (variant 2) Modulation: 16APSK @ DVB-S2X, short FEC frame (variant 3) Modulation: 32APSK @ DVB-S2X, short FEC frame (variant 4) Modulation: 16APSK @ DVB-S2X, normal FEC frame, linear Modulation: 32APSK @ DVB-S2X, normal FEC frame, linear (variant 2) Modulation: 64APSK @ DVB-S2X, normal FEC frame, linear (variant 3) Modulation: 256PSK @ DVB-S2X, normal FEC frame, linear (variant 4) Modulation: QPSK @ DVB-S2 Modulation: 8PSK @ DVB-S2 (variant 2) Modulation: 16APSK @ DVB-S2 (variant 3) Modulation: 32APSK @ DVB-S2 (variant 4) Protocols / waveforms: CCSDS 231.0-B-3 TC uplinks Protocols / waveforms: CCSDS 131.0-B-3 TM downlinks @ (variant 2) Protocols / waveforms: DVB-S2X - ETSI EN 302 307-2 @ (variant 3) Protocols / waveforms: DVB-S2 - ETSI EN 302 307-1 @ (variant 4) Protocols / waveforms: CCSDS 131.3-B-1 CADU frames over DVB-S2 @ (variant 5) Frequency: 950 MHz (min) @ RX Signal input L-band Frequency: 2150 MHz (max) @ RX Signal input L-band Frequency: 680 MHz (min) @ RX Signal input L-band w/ licenses RXL680 and RXL2300 Frequency: 2300 MHz (max) @ RX Signal input L-band w/ licenses RXL680 and RXL2300 RX sensitivity: -70 (min) RX sensitivity: -10 (max) Data interface: Ethernet @ Data network Data interface: Ethernet @ M&C network Connector: RJ-45 @ Data network Connector: RJ-45 @ M&C network Connector: BNC female @ 10 MHz reference input w/ option RI Connector: DSUB-9 female @ Alarm w/ option RI Operating temperature: 0 °C (min) Operating temperature: 50 °C (max) Operating temperature: -30 °C (min) @ w/ option EXT Operating temperature: 60 °C (max) @ w/ option EXT Survival temperature: -30 °C (min) Survival temperature: 80 °C (max) Supply voltage: 100 (min) @ nominal Supply voltage: 240 (max) @ nominal Supply voltage: 90 (min) @ max Supply voltage: 264 (max) @ max Power consumption: 45 W @ typical Connector: IEC C14 @ Mains power Envelope (L×W×H): 483 x 44 x 505 mm³ (WxHxD) Mass: 10000 g (max) @ depending on device type Data rate: 360000 kbps @ rx+tx processing Warranty: 3 ## K/Ka-Band Single Channel Transceiver TR1000 — ReliaSat [sdr-modems] https://newspacemarket.com/products/arralis-tr1000-k-ka-single-channel-transceiver/ Connector: Waveguide flanges Frequency: 17000 MHz (min) @ TX output Frequency: 21000 MHz (max) @ TX output Frequency: 27000 MHz (min) @ RX input Frequency: 31000 MHz (max) @ RX input TX power: 10 W @ CW Power consumption: 28 W @ DC power Mass: 2200 g Frequency: 17000 MHz (min) @ TX Output (variant 2) Frequency: 21000 MHz (max) @ TX Output (variant 2) TX power: 10 W @ CW (variant 2) Operating temperature: -40 °C (min) Operating temperature: 85 °C (max) Supply voltage: 25 (min) Supply voltage: 28 (max) Frequency: 27000 MHz (min) @ RX Input (variant 2) Frequency: 31000 MHz (max) @ RX Input (variant 2) Mass: 2200 g @ (variant 2) Operating temperature: -40 °C (min) @ (variant 2) Operating temperature: 85 °C (max) @ (variant 2) ## U7400 VSAT Router for Professional Mobility/Trunking — SpaceBridge Inc. [sdr-modems] https://newspacemarket.com/products/u7400/ Data rate: 100000 kbps @ Download Speed Data rate: 100000 kbps @ Upload Speed Modulation: QPSK up to 256APSK LDPC/BCH @ Forward Link/TX, DVB-S2/S2X ACM Modulation: BPSK, QPSK, 8PSK, 16QAM @ Return Link/TX, MF-TDMA Modulation: DVB-S2 QPSK up to 32APSK LDPC/BCH @ Return Link/TX, SCPC Protocols / waveforms: DVB TDM @ Forward Link/TX Protocols / waveforms: DVB-S2/S2X ACM @ Forward Link/TX (variant 2) Protocols / waveforms: MF-TDMA CF-DAMA @ Return Link/TX Protocols / waveforms: DVB-S2X SCPC @ Return Link/TX point-to-point and hub-spoke Mass: 3300 g Envelope (L×W×H): 435 x 45 (1RU) x 315mm (W x H x D) Supply voltage: 48 @ DC power supply option Supply voltage: 24 @ DC provided to BUC Power consumption: 35 W @ not including RF equipment / BUC power Power consumption: 80 W @ available for installation and RF equipment Data interface: Ethernet @ 10/100/1000 Mbps RJ-45 Data interface: other @ out-of-band satellite modem management Connector: F-type 75 ohm @ Terminal IFL Input Connector: F-type 75 ohm @ Terminal IFL Output Connector: RJ-45 @ 10/100/1000 Mbps Eth Protocols / waveforms: DVB-S2/S2X ACM, GSE encapsulation, QPSK up to 256APSK LDPC/BCH Protocols / waveforms: BPSK, QPSK, 8PSK, 16QAM @ (variant 2) Protocols / waveforms: DVB-S2 QPSK up to 32APSK LDPC/BCH @ (variant 3) ## Polaris AIS — Satlab A/S [sdr-modems] https://newspacemarket.com/products/satlab-polaris-ais/ Random vibration: 14.1 TRL: 9 Frequency: 156.775, 156.825, 161.975, 162.025 MHz RX sensitivity: -121 @ 80 % reception rate Supply voltage: 4.5 V to 40 V Power consumption: 1.5 W @ Typical, 5 V input, 25°C Operating temperature: -40 °C to +85 °C Data interface: CAN Data rate: 1000 kbps Data interface: RS-422 @ Full duplex Data rate: 3000 kbps @ Full duplex Data interface: Ethernet @ Full duplex (variant 2) Data rate: 100000 kbps @ Full duplex (variant 2) Envelope (L×W×H): 87.2 x 93.0 x 12.5 mm Mass: 185 g Data interface: CAN @ (variant 2) Data interface: RS-422 @ (variant 3) Data interface: Ethernet @ (variant 4) Flight heritage: QubeAIS receiver which has flown on several missions since 2013 Connector: Harwin Gecko Connector: Amphenol coaxial SMP @ (variant 2) Survival temperature: -40 °C Survival temperature: 85 °C @ (variant 2) RX sensitivity: -121 @ 80% reception rate RX sensitivity: -120 (max) @ 80% reception rate Power consumption: 1.5 W @ VIN 5 V, CAN on, Ethernet off, RS-422 off Power consumption: 1.82 W @ VIN 28 V, CAN on, Ethernet off, RS-422 off Power consumption: 0.08 W @ Additional power for SDRAM enabled @ VIN 5 V Power consumption: 0.185 W @ Additional power for Ethernet enabled @ VIN 5 V Power consumption: 0.11 W @ Additional power for RS-422 enabled @ VIN 5 V Radiation tolerance (TID): 20 krad @ board level ## Satlab Polaris ADS-B — Satlab A/S [sdr-modems] https://newspacemarket.com/products/satlab-polaris-adsb/ Frequency: 865 MHz (min) Frequency: 870 MHz (max) RX sensitivity: -130 @ 99% reception rate, SF9 with CR4 RX sensitivity: -128.9 @ PER <10 % @ 869.525 MHz, SF8, Gain 25 RX sensitivity: -127.8 @ PER <10 % @ 869.525 MHz, SF8, Gain 20 RX sensitivity: -123 @ PER <10 % @ 869.525 MHz, SF8, Gain 15 RX sensitivity: -131.4 @ PER <10 % @ 869.525 MHz, SF9, Gain 25 RX sensitivity: -130.3 @ PER <10 % @ 869.525 MHz, SF9, Gain 20 RX sensitivity: -125.9 @ PER <10 % @ 869.525 MHz, SF9, Gain 15 RX sensitivity: -127.6 @ PER <1 % @ 869.525 MHz, SF8, Gain 25 RX sensitivity: -126.6 @ PER <1 % @ 869.525 MHz, SF8, Gain 20 RX sensitivity: -121.8 @ PER <1 % @ 869.525 MHz, SF8, Gain 15 RX sensitivity: -130.1 @ PER <1 % @ 869.525 MHz, SF9, Gain 25 RX sensitivity: -129.1 @ PER <1 % @ 869.525 MHz, SF9, Gain 20 RX sensitivity: -124.7 @ PER <1 % @ 869.525 MHz, SF9, Gain 15 Modulation: LoRa Mass: 185 g Envelope (L×W×H): 93.0 x 87.2 x 12.5 mm Supply voltage: 4.5 (min) Supply voltage: 40 (max) Power consumption: 1.5 W @ typical, 5 V input, 25°C Power consumption: 1.35 W @ VIN 5V, CAN on, Ethernet off, RS-422 off Power consumption: 1.5 W @ max, VIN 5V, CAN on, Ethernet off, RS-422 off Power consumption: 1.625 W @ VIN 28V, CAN on, Ethernet off, RS-422 off Power consumption: 1.8 W @ max, VIN 28V, CAN on, Ethernet off, RS-422 off Power consumption: 0.08 W @ additional for SDRAM enabled Power consumption: 0.185 W @ additional for Ethernet enabled Power consumption: 0.11 W @ additional for RS-422 enabled Data interface: CAN Data interface: RS-422 @ (variant 2) Data interface: Ethernet @ (variant 3) Data rate: 1000 kbps @ CAN-bus Data rate: 3000 kbps @ RS-422 Data rate: 100000 kbps @ Ethernet Operating temperature: -40 °C (min) Operating temperature: 85 °C (max) Survival temperature: -40 °C (min) Survival temperature: 85 °C (max) Radiation tolerance (TID): 20 krad Flight heritage: first tested in space 2022 Q2 Random vibration: 14.1 TRL: 9 ## Polaris LoRa — Satlab A/S [sdr-modems] https://newspacemarket.com/products/satlab-polaris-lora/ Random vibration: 14.1 Flight heritage: Reliable flight heritage since 2019 (Polaris SDR product line), QubeAIS receiver flown since 2013 TRL: 9 Frequency: 865 MHz (min) @ Frequency coverage Frequency: 870 MHz (max) @ Frequency coverage RX sensitivity: -130 @ 99% reception rate, SF9 with CR4 RX sensitivity: -128.9 @ PER <10 %, SF8, Gain setting 25 RX sensitivity: -127.6 @ PER <1 %, SF8, Gain setting 25 RX sensitivity: -127.8 @ PER <10 %, SF8, Gain setting 20 RX sensitivity: -126.6 @ PER <1 %, SF8, Gain setting 20 RX sensitivity: -123 @ PER <10 %, SF8, Gain setting 15 RX sensitivity: -121.8 @ PER <1 %, SF8, Gain setting 15 RX sensitivity: -131.4 @ PER <10 %, SF9, Gain setting 25 RX sensitivity: -130.1 @ PER <1 %, SF9, Gain setting 25 RX sensitivity: -130.3 @ PER <10 %, SF9, Gain setting 20 RX sensitivity: -129.1 @ PER <1 %, SF9, Gain setting 20 RX sensitivity: -125.9 @ PER <10 %, SF9, Gain setting 15 RX sensitivity: -124.7 @ PER <1 %, SF9, Gain setting 15 Mass: 185 g Envelope (L×W×H): 93.0 x 87.2 x 12.5 mm Supply voltage: 4.5 (min) @ Input voltage Supply voltage: 40 (max) @ Input voltage Power consumption: 1.5 W @ Typical, 5 V input, 25°C Power consumption: 1.35 W @ VIN 5V, CAN on, Ethernet off, RS-422 off Power consumption: 1.5 W (max) @ VIN 5V, CAN on, Ethernet off, RS-422 off Power consumption: 1.625 W @ VIN 28V, CAN on, Ethernet off, RS-422 off Power consumption: 1.8 W (max) @ VIN 28V, CAN on, Ethernet off, RS-422 off Power consumption: 0.08 W @ Additional, SDRAM enabled Power consumption: 0.185 W @ Additional, Ethernet enabled Power consumption: 0.11 W @ Additional, RS-422 enabled Data rate: 1000000 kbps @ CAN-bus Data rate: 3000000 kbps @ RS-422 Data rate: 100000 kbps @ Ethernet Operating temperature: -40 °C (min) Operating temperature: 85 °C (max) Survival temperature: -40 °C (min) @ Storage Temperature Survival temperature: 85 °C (max) @ Storage Temperature Radiation tolerance (TID): 20 krad @ board level ## IQ Spacecom X Link-X — IQ Spacecom [sdr-modems] https://newspacemarket.com/products/iq-spacecom-x-link-x/ Frequency: 8025000-8400000 MHz @ X band Tx operation Frequency: 7145000-7250000 MHz @ X band Rx operation Frequency: 2025000-2110000 MHz @ S band Rx operation Data rate: 2000-200000000 kbps @ Sat2Ground Data rate: 56 kbps @ Ground2Sat TX power: 1 W @ Linear RF output power TX power: 0.501 W @ Linear RF output power (2 x) Power consumption: 16 W @ max (Tx + Rx) Power consumption: 4 W @ Rx-S Power consumption: 5.5 W @ Rx-X Supply voltage: 6-18 @ DC supply Supply voltage: 28 @ DC supply Mass: 200 g Frequency: 8025000-8400000 MHz @ Tx Frequency Band (Default Configuration) Frequency: 7900000-8500000 MHz @ Tx Frequency Band (Optional Configuration) Data rate: 500000-100000000 kbps @ Tx Payload Data (Default Configuration) Data rate: 2000-200000000 kbps @ Tx Payload Data (Optional Configuration) TX power: 0.501 W @ RF Power Output (2 Tx channels, w/o aerial) TX power: 1 W @ RF Power Output (combined, w/o aerial) Frequency: 7145000-7250000 MHz @ Rx Frequency Bands (X band) Frequency: 2025000-2110000 MHz @ Rx Frequency Bands (S band) Data rate: 56 kbps @ Rx Payload Data (Default Configuration) Data rate: 3.5-896 kbps @ Rx Payload Data (Optional Configuration) Supply voltage: 6-18 @ DC supply (Default Configuration) Supply voltage: 28 @ DC supply (Optional Configuration) Power consumption: 16 W @ DC Power Consumption (Tx + Rx) Power consumption: 4 W @ DC Power Consumption (Rx-S only) Power consumption: 5.5 W @ DC Power Consumption (Rx-x) Mass: 200 g @ incl. housing (Default Configuration) Mass: 365 g @ incl. housing (High Radiation Tolerance) Operating temperature: -30-60 °C TRL: 9 ## TREVO — Alén Space [sdr-modems] https://newspacemarket.com/products/trevo/ Lead time: 16 Frequency: 70 MHz (min) Frequency: 6000 MHz (max) Data interface: CAN Data interface: UART @ (variant 2) Data interface: I2C @ (variant 3) Data interface: USB @ (variant 4) Data interface: Ethernet @ (variant 5) Power consumption: 0.775 W @ Nominal power Frequency: 70 MHz (min) @ (variant 2) Frequency: 6000 MHz (max) @ (variant 2) Power consumption: 1.5 W @ Maximum Power consumption: 1.05 W @ Full duplex (RX and TX) ## GAMALINK — TEKEVER [sdr-modems] https://newspacemarket.com/products/tekever-gamalink-inter-satellite-link/ Data interface: RS-422 @ 2 x (up to 460800 baud) Data interface: other @ 2 x PPS input Radiation tolerance (TID): 20 krad Envelope (L×W×H): 160 x 120 x 65 mm @ Deep Space Envelope (L×W×H): 96 x 94 x 45 mm @ New Space Mass: 910 g @ Deep Space Mass: 450 g @ New Space Flight heritage: ESA HERA MISSION Flight heritage: ESA PROBA 3 MISSION @ (variant 2) Power consumption: 0.1 W ## NanoCom SR2000 — GomSpace [sdr-modems] https://newspacemarket.com/products/nanocom-sr2000/ Operating temperature: -40 °C Modulation: High-speed QPSK transceiver @ S-band communication Data rate: 500 kbps (max) @ Layer-3 bandwidth, TDD Data rate: 1250 kbps (max) @ Layer-3 bandwidth, FDD Frequency: S-band operation (1980-2290 MHz) Protocols / waveforms: Partial CCSDS Proximity-1 Compliance, Category A Protocols / waveforms: SFCG recommendation 21-4R4 spectral mask compliance @ (variant 2) Data interface: RS-422 @ for payload data transfer (either TCP/IP via PPP or CSP) Data interface: CAN @ for configuration and CSP datagram transfer Modulation: Filtered QPSK modulation RX sensitivity: High sensitivity @ PER less than 1e-4 at Eb/No = 5 dB Data interface: UART @ GOSH console interface Data rate: 1250 kbps (max) @ Layer-3 UDP throughput (max), FDD Data rate: 500 kbps (max) @ Layer-3 UDP throughput (max), TDD Frequency: S-band operation 1980-2290 MHz @ (variant 2) Data interface: RS-422 @ for payload data transfer Data interface: CAN Data rate: 1250 kbps (max) @ Layer-3 UDP throughput (max), FDD (variant 2) Data rate: 500 kbps (max) @ Layer-3 UDP throughput (max), TDD (variant 2) Frequency: S-band operation 1980-2290 MHz @ (variant 3) Data interface: RS-422 @ for payload data transfer (variant 2) Data interface: CAN @ (variant 2) Data rate: 1250 kbps (max) @ Layer-3 UDP throughput (max), FDD (variant 3) Data rate: 500 kbps (max) @ Layer-3 UDP throughput (max), TDD (variant 3) Frequency: S-band operation 1980-2290 MHz @ (variant 4) Data interface: RS-422 @ for payload data transfer (variant 3) Data interface: CAN @ (variant 3) ## Quadro Arrow — Exolaunch [separation-systems] https://newspacemarket.com/products/exolaunch-quadro-arrow/ Flight heritage: First flight Q1 2025 (SpaceX Transporter-13), 4 missions, 9 microsats Export status: ITAR-FREE Mass: 1580 g @ S-Adapter Mass: 6820 g @ L-Adapter Mass: 8400 g @ Combined Mass Preload / holding force: 75 kN (max) @ Maximum Axial Preload / holding force: 20 kN (max) @ Maximum Lateral (Shear) Release time: 100 ms @ Average Separation Time Operating temperature: -34 °C @ Lower Operating Limit Operating temperature: 71 °C @ Upper Operating Limit Survival temperature: -55 °C @ Lower Survival Limit Survival temperature: 130 °C @ Upper Survival Limit Mass: 1580 g @ S-Adapter Mass (all four points) Mass: 6820 g @ L-Adapter Mass Mass: 8400 g @ Combined Stowed Mass Preload / holding force: 75 kN (max) @ Maximum Axial Force Preload / holding force: 20 kN (max) @ Maximum Shear Force Preload / holding force: 0.07 kN @ Holding force Supply voltage: 28 @ Nominal Voltage Supply voltage: 24 (min) Supply voltage: 36 (max) Release time: 500 ms @ Nominal Pulse Duration Mass: 20 g @ Separation Switch (incl. mounting bracket and plunger receptacle) Mass: 11.4 g @ Upper Separation Connector Mass: 14.6 g @ Lower Separation Connector ## CarboNIX NEO — Exolaunch [separation-systems] https://newspacemarket.com/products/exolaunch-carbonix-neo/ Mass: 400 g @ NEO 8 S-Ring Mass: 820 g @ NEO 15 S-Ring Mass: 1280 g @ NEO 24 S-Ring Mass: 1680 g @ NEO 31.6 S-Ring Mass: 2000 g @ NEO 38.81 S-Ring Mass: 2400 g @ NEO 8 L-Ring Mass: 3960 g @ NEO 15 L-Ring Mass: 6020 g @ NEO 24 L-Ring Mass: 7670 g @ NEO 31.6 L-Ring Mass: 9400 g @ NEO 38.81 L-Ring Supply voltage: 28 @ Nominal Separation Signal Release time: 100 ms (nominal) @ Average Separation Time Operating temperature: -34 °C (min) Operating temperature: 79 °C (max) Survival temperature: -55 °C (min) Survival temperature: 130 °C (max) Release shock: 2000 @ at 1 kHz Release shock: 5000 @ at 10 kHz Mass: 19 g @ Separation Switch (incl. mounting bracket) Mass: 20 g @ Upper Separation Connector Mass: 28 g @ Lower Separation Connector Mass: 7.9 g @ M6x25 Socket Head Screw + NL6ss washer Export status: not subject to strict export regulations such as ITAR Envelope (L×W×H): 8", 15", 24", 31.6", 38.81" (custom) Flight heritage: First flight Q4 2025, 3 missions, 3 microsats ## Quadro Versa — Exolaunch [separation-systems] https://newspacemarket.com/products/exolaunch-quadro-versa/ Mass: 540 g @ S-Adapter [kg each] Preload / holding force: 44 kN (max) @ Axial Release time: 100 ms @ Average Separation Time Supply voltage: 28 (nominal) @ Nominal Separation Signal Operating temperature: -34 °C (min) Operating temperature: 79 °C (max) Survival temperature: -55 °C (min) Survival temperature: 130 °C (max) Flight heritage: Critical subsystems like lock mechanism and pusher arms have flight heritage across dozens of missions. Mass: 11600 g @ L-Adapter, Size 24x16 Mass: 12400 g @ L-Adapter, Size 24x20 Mass: 13100 g @ L-Adapter, Size 24x24 Mass: 13900 g @ L-Adapter, Size 24x28 Mass: 14600 g @ L-Adapter, Size 24x32 Mass: 15400 g @ L-Adapter, Size 24x36 Mass: 16100 g @ L-Adapter, Size 24x40 Mass: 11900 g @ L-Adapter, Size 28x16 Mass: 12700 g @ L-Adapter, Size 28x20 Mass: 13400 g @ L-Adapter, Size 28x24 Mass: 14200 g @ L-Adapter, Size 28x28 Mass: 14900 g @ L-Adapter, Size 28x32 Mass: 15700 g @ L-Adapter, Size 28x36 Mass: 16400 g @ L-Adapter, Size 28x40 Mass: 12200 g @ L-Adapter, Size 32x16 Mass: 13000 g @ L-Adapter, Size 32x20 Mass: 13700 g @ L-Adapter, Size 32x24 Mass: 14500 g @ L-Adapter, Size 32x28 Mass: 15200 g @ L-Adapter, Size 32x32 Mass: 16000 g @ L-Adapter, Size 32x36 Mass: 16700 g @ L-Adapter, Size 32x40 Mass: 12500 g @ L-Adapter, Size 36x16 Mass: 13300 g @ L-Adapter, Size 36x20 Mass: 14000 g @ L-Adapter, Size 36x24 Mass: 14800 g @ L-Adapter, Size 36x28 Mass: 15500 g @ L-Adapter, Size 36x32 Mass: 16300 g @ L-Adapter, Size 36x36 Mass: 17000 g @ L-Adapter, Size 36x40 Mass: 12800 g @ L-Adapter, Size 40x16 Mass: 13600 g @ L-Adapter, Size 40x20 Mass: 14300 g @ L-Adapter, Size 40x24 Mass: 15100 g @ L-Adapter, Size 40x28 Mass: 15800 g @ L-Adapter, Size 40x32 Mass: 16600 g @ L-Adapter, Size 40x36 Mass: 17300 g @ L-Adapter, Size 40x40 Mass: 2200 g @ S-Adapter Preload / holding force: 44 kN @ Maximum Axial Force Preload / holding force: 37 kN @ Maximum Shear Force Envelope (L×W×H): 24"×24" to 40"×40" (scalable) ## Solar Array Drive Assemblies — Blue Canyon Technologies [sadm] https://newspacemarket.com/products/solar-array-drive-assemblies/ Power consumption: 12 W @ MANUEVER Mass: 1500 g Envelope (L×W×H): ø11.1 x 12.5 cm Max torque: 10000 mN·m Wheel speed: 10 (max) Power consumption: 12 W @ maneuver Design lifetime: 5 years Output power (BOL): 12 W ## PHOTON CubeSat Solar Arrays — AAC Clyde Space [solar-panels] https://newspacemarket.com/products/aac-photon-side/ TRL: 9 Cell efficiency: 30.7 Operating temperature: -40 °C (min) Operating temperature: 80 °C (max) Output power (BOL): 9 W @ per 3U populated face Form factor: 3U to 12U Deployable: body, single, double and triple deployment options Mass: 135 g @ PHOTON-SIDE (3U) Envelope (L×W×H): 3.5mm (PHOTON-SIDE stowed height) Mass: 310 g @ PHOTON-SD (3U) Envelope (L×W×H): 7mm (PHOTON-SD stowed height) @ (variant 2) Mass: 330 g @ PHOTON-DD (3U) Envelope (L×W×H): 9.55mm (PHOTON-DD stowed height) @ (variant 3) Mass: 330 g @ PHOTON-TD (3U) Envelope (L×W×H): 9.5mm (PHOTON-TD stowed height) @ (variant 4) Flight heritage: decades of on-orbit heritage Flight heritage: unparalleled track record in orbit @ (variant 2) ## CORE Solar Panels — 2NDSpace Srl [solar-panels] https://newspacemarket.com/products/2ndspace-core-solar-panels/ Flight heritage: flight heritage Power consumption: 2.45 W Form factor: 1U to 16U Output power (BOL): 2.45 W Supply voltage: 5.2 Mass: 38 g ## Roll Out Solar Array (ROSA) — Redwire Corporation [solar-panels] https://newspacemarket.com/products/redwire-rosa-roll-out-solar-array/ Power consumption: 3.3 W Power consumption: 5.3 W @ (variant 2) Power consumption: 12.9 W @ (variant 3) Power consumption: 17.6 W @ (variant 4) Power consumption: 28 W @ (variant 5) Power consumption: 37 W @ (variant 6) Flight heritage: LEO, GEO, and deep space missions Flight heritage: key NASA programs, including DART and ISS @ (variant 2) Flight heritage: delivered 8 SUNSTONE ROSA solar wings to NASA to improve power generation on the International Space Station (ISS) @ (variant 3) Supply voltage: 12-300 Mass: 36000 g Output power (BOL): 3.3 W Mass: 42700 g @ (variant 2) Output power (BOL): 5.3 W @ (variant 2) Mass: 160000 g @ (variant 3) Output power (BOL): 12.9 W @ (variant 3) Mass: 180000 g @ (variant 4) Output power (BOL): 17.6 W @ (variant 4) Mass: 331000 g @ (variant 5) Output power (BOL): 28 W @ (variant 5) Mass: 521000 g @ (variant 6) Output power (BOL): 37 W @ (variant 6) ## ODALISS Solar Panels — Emxys [solar-panels] https://newspacemarket.com/products/emxys-solar-panels/ Connector: 2.2 mm @ (variant 5) Form factor: 123 grams @ (variant 2) Form factor: 14.7 V @ (variant 3) Form factor: 66.6 W/Kg @ (variant 4) Form factor: 8.2 W @ (variant 5) Form factor: 33.6 V @ (variant 6) Form factor: 53.3 W/Kg @ (variant 7) Form factor: 17.6 W @ (variant 8) Cell efficiency: 29 (min) Output power (BOL): 8.2 W @ LEO (3U) Form factor: 3U/6U CubeSat platform compatible Envelope (L×W×H): 327.5mm x 83.0mm @ 3U Envelope (L×W×H): 2.2mm @ thickness (without connectors) Mass: 123 g @ 3U Connector: Three 4-pin solar array power output Connector: One 4-pin connector for temperature sensor @ (variant 2) Connector: One 2-pin connector for sun sensor @ (variant 3) Connector: ODALISS Interface port connector @ (variant 4) Operating temperature: -45 °C (min) Operating temperature: 125 °C (max) Supply voltage: 14.7 Power consumption: 66.6 W Power consumption: 8.2 W @ (variant 2) Supply voltage: 33.6 @ (variant 2) Power consumption: 53.3 W @ (variant 3) Power consumption: 17.6 W @ (variant 4) ## Solis & Solis+ Spacecraft Solar Arrays — Dhruva Space [solar-panels] https://newspacemarket.com/products/solis-solis-spacecraft-solar-arrays/ Power consumption: 2.4 W Power consumption: 8.4 W @ (variant 2) Power consumption: 4.8 W @ (variant 3) Power consumption: 16.8 W @ (variant 4) Power consumption: 9.6 W @ (variant 5) Power consumption: 24 W @ (variant 6) Cell efficiency: 30 (max) Output power (BOL): 2.4 W @ 3Z Form factor: 1U, 2U, 3U @ 3Z Output power (BOL): 8.4 W @ 3X/Y Form factor: 3U, 6U @ 3X/Y Output power (BOL): 4.8 W @ 6Z Form factor: 6U @ 6Z Output power (BOL): 16.8 W @ 6X Form factor: 6U, 12U @ 6X Output power (BOL): 9.6 W @ 12Z Form factor: 12U, 16U @ 12Z Output power (BOL): 24 W @ 16X/Y Form factor: 16U @ 16X/Y Deployable: yes ## 220W Deployable Clamshell Solar Array (DCSA) — Pumpkin, Inc. [solar-panels] https://newspacemarket.com/products/pumpkin-dcsa-220w/ Output power (BOL): 220 W @ max Form factor: hinged clamshell halves Deployable: two wings Mass: 5100 g Envelope (L×W×H): 439 x 116 x 136mm @ Stowed Envelope (L×W×H): 878 x 116 x 1390mm @ Deployed Cell efficiency: 32.2 Power consumption: 220 W Flight heritage: 100% success rate in LEO and GTO orbits (PMDSAS solar panel/array technology) ## DROP-03 3U Deployable Solar panel — 2NDSpace Srl [solar-panels] https://newspacemarket.com/products/drop-03-deployable-solar-panels/ Power consumption: 7.5 W Power consumption: 22.5 W @ (variant 2) Power consumption: 22.5 W @ (variant 3) Form factor: 3U Deployable: 1 Output power (BOL): 7.5 W @ Front Side Peak Power Output power (BOL): 8 W @ Body Mounted Option Output power (BOL): 8 W @ Back String Option Output power (BOL): 22.5 W @ Total Available Power Supply voltage: 15.6 @ Panel Voc Supply voltage: 14.58 @ Peak PWR Voltage Cell efficiency: 30 (min) Flight heritage: TRL9 solution with flight heritage ## DROP-12 12U Deployable Solar panel — 2NDSpace Srl [solar-panels] https://newspacemarket.com/products/drop-12-deployable-solar-panels/ Deployable: 1 Output power (BOL): 20 W @ Front Side Peak Power Supply voltage: 20.8 @ Panel Voc Supply voltage: 19.44 @ Peak PWR Voltage Flight heritage: TRL9 solution with flight heritage Power consumption: 20 W Power consumption: 60 W @ (variant 2) Power consumption: 60 W @ (variant 3) ## DROP-08 8U/4U Deployable Solar panel — 2NDSpace Srl [solar-panels] https://newspacemarket.com/products/drop-16-deployable-solar-panels/ Deployable: 1 Deployable: 135°/90° @ (variant 2) Power consumption: 10 W Power consumption: 30 W @ (variant 2) Power consumption: 30 W @ (variant 3) Supply voltage: 20.8 Deployable: Dual redundant @ (variant 3) Output power (BOL): 20 W @ Front Side Peak Power Output power (BOL): 10 W @ Body Mounted Option Output power (BOL): 10 W @ Back String Option Output power (BOL): 40 W @ Total Available Power Deployable: 2 @ N° of deployable Elements Cell efficiency: 30 @ UTJ ## CORE-01 1U Cubesat Solar panel — 2NDSpace Srl [solar-panels] https://newspacemarket.com/products/core-01-1u-cubesat-solar-panel/ Power consumption: 2.45 W Supply voltage: 5.2 Output power (BOL): 2.45 W Form factor: 1x1 Mass: 35 g Flight heritage: flight heritage ## CORE-03 3U Cubesat Solar panel — 2NDSpace Srl [solar-panels] https://newspacemarket.com/products/core-03-3u-cubesat-solar-panel/ Output power (BOL): 8.54 W Cell efficiency: 30 (min) Form factor: 1x3 Form factor: 3U / 6U @ Suggested for Mass: 118 g Power consumption: 8.54 W ## CORE-12 6U/12U Cubesat Solar panel — 2NDSpace Srl [solar-panels] https://newspacemarket.com/products/core-12-6u-12u-cubesat-solar-panel/ Power consumption: 19.6 W Output power (BOL): 19.52 W Cell efficiency: 30 @ gt Form factor: 2x3 Deployable: no Mass: 289 g Supply voltage: 10.4 Supply voltage: 20.8 @ (variant 2) ## CORE-02 2U Cubesat Solar panel — 2NDSpace Srl [solar-panels] https://newspacemarket.com/products/core-02-2u-cubesat-solar-panel/ Output power (BOL): 4.88 W Cell efficiency: 30 (min) Form factor: 1x2 Mass: 75 g Supply voltage: 5.2 Supply voltage: 10.4 @ (variant 2) Flight heritage: TRL9 solution with flight heritage Power consumption: 5 W ## CORE-01Z 1U Cubesat Top Solar panel — 2NDSpace Srl [solar-panels] https://newspacemarket.com/products/core-01z-1u-cubesat-top-solar-panel/ Power consumption: 2.45 W Output power (BOL): 2.45 W @ Peak Power Cell efficiency: 30 (max) Form factor: 1x1 Mass: 38 g Supply voltage: 5.2 @ OC Voltage Flight heritage: flight heritage ## CORE-06Z 6U/8U Cubesat Top Solar panel — 2NDSpace Srl [solar-panels] https://newspacemarket.com/products/core-06z-6u-8u-cubesat-top-solar-panel/ Output power (BOL): 4.88 W Cell efficiency: 30 (min) Form factor: 2x1 Mass: 91 g Supply voltage: 5.2-10.4 Flight heritage: TRL9 solution with flight heritage Power consumption: 4.9 W ## CORE-08 4U/8U Cubesat Solar panel — 2NDSpace Srl [solar-panels] https://newspacemarket.com/products/core-08-4u-8u-cubesat-solar-panel/ Output power (BOL): 11 W Cell efficiency: 30 @ gt Form factor: 1x4 Mass: 148 g Supply voltage: 5.2 Supply voltage: 7.8 @ (variant 2) Supply voltage: 10.4 @ (variant 3) Supply voltage: 23.4 @ (variant 4) Power consumption: 11 W ## DROP-16 8U/16U Deployable Solar panel — 2NDSpace Srl [solar-panels] https://newspacemarket.com/products/drop-16-8u-16u-deployable-solar-panel/ Deployable: 1 Output power (BOL): 25 W @ Front Side Peak Power Output power (BOL): 25 W @ Body Mounted Option Output power (BOL): 25 W @ Back String Option Output power (BOL): 75 W @ Total Available Power Supply voltage: 24.3 Power consumption: 25 W Power consumption: 75 W @ (variant 2) Supply voltage: 24.3 @ (variant 2) ## CLASP Composite Lightweight Array with Shape-memory Polymer — CTD (Composite Technology Development) [solar-panels] https://newspacemarket.com/products/ctd-clasp-solar-array/ Cell efficiency: 110 Form factor: CubeSat dispenser compatible Deployable: yes Flight heritage: CLASP Flight Qualified ## CORE-12Z — 2NDSpace Srl [solar-panels] https://newspacemarket.com/products/core-12z/ Output power (BOL): 9.76 W @ Peak Power Cell efficiency: 30 @ gt Form factor: 2x2 Mass: 195 g Supply voltage: 5.2 @ OC Voltage Supply voltage: 10.4 @ OC Voltage (variant 2) Supply voltage: 20.8 @ OC Voltage (variant 3) Flight heritage: TRL9 solution with flight heritage Power consumption: 9.76 W ## CORE-16 — 2NDSpace Srl [solar-panels] https://newspacemarket.com/products/core-16/ Power consumption: 24.4 W Output power (BOL): 24.4 W Form factor: 2x4 Mass: 387 g Supply voltage: 10.4/13.0/26.0 Cell efficiency: 30 (min) Flight heritage: TRL9 solution with flight heritage ## NanoPower MSP — GomSpace [solar-panels] https://newspacemarket.com/products/nanopower-msp/ Operating temperature: -55 °C Cell efficiency: 28-30 Output power (BOL): 1.2 W @ per cell in LEO ## ST200 — AAC Clyde Space [star-trackers] https://newspacemarket.com/products/aac-st200/ Update rate: 5 Hz Data interface: UART @ TTL Data interface: RS-422 @ optional Data interface: RS-485 @ optional (variant 2) Data interface: I2C @ optional (variant 3) Radiation tolerance (TID): 9 krad Mass: 42 g Power consumption: 0.6 W @ nominal Envelope (L×W×H): 29 x 29 x 38.1 mm @ without baffle Attitude accuracy (cross-boresight): 30 @ pitch, yaw, 3-sigma Accuracy around boresight (roll): 200 @ 3-sigma Max tracking slew rate: 0.3 (max) @ tip/tilt Max tracking slew rate: 0.6 (max) @ roll Sun exclusion angle: 30 @ optional baffle Sun exclusion angle: 45 @ optional baffle (variant 2) Operating temperature: -20 °C (min) Operating temperature: 40 °C (max) Supply voltage: 3.6 (min) Supply voltage: 34 (max) Power consumption: 0.37 W (min) Power consumption: 0.7 W @ typical Power consumption: 1 W (max) Flight heritage: flying since 2015 on over 20 missions Field of view: 15 TRL: 9 ## ST400 — AAC Clyde Space [star-trackers] https://newspacemarket.com/products/aac-st400/ Field of view: 10 TRL: 8 Update rate: 5 Hz Data interface: RS-422 Data interface: RS-485 @ (variant 2) Radiation tolerance (TID): 9 krad Mass: 280 g Power consumption: 0.7 W @ nominal power consumption when running at 5Hz update rate Envelope (L×W×H): 53.8 x 53.8 x 90.5 mm @ excluding baffle Flight heritage: since 2016 Attitude accuracy (cross-boresight): 10 @ pitch, yaw, 3-sigma Accuracy around boresight (roll): 120 @ 3-sigma Update rate: 5 Hz @ (variant 2) Max tracking slew rate: 0.5 (max) @ tip/tilt Max tracking slew rate: 1 (max) @ roll Envelope (L×W×H): 53.8 x 53.8 x 90.5 mm Mass: 280 g @ (variant 2) Sun exclusion angle: 40 @ Optional baffle sun exclusion half angle, Standard size Operating temperature: -20 °C (min) Operating temperature: 40 °C (max) Radiation tolerance (TID): 9 krad @ (variant 2) Supply voltage: 3.6 (min) Supply voltage: 34 (max) Power consumption: 0.37 W @ Min. Power consumption: 0.7 W @ Typ. At 5V, at 5Hz update rate. Power consumption: 1 W @ Max. ## Sodern Auriga SA — Sodern [star-trackers] https://newspacemarket.com/products/sodern-auriga-sa/ Field of view: 9 Design lifetime: 10 years @ LEO 400-1200km Design lifetime: 15 years @ GEO with EOR Envelope (L×W×H): 66 x 56 x 94 (height) @ OH, including baffle Envelope (L×W×H): 91 x 117 x 25 (height) @ EU Mass: 225 g @ OH, including baffle Mass: 315 g @ EU Lost-in-space acquisition time: 3.8 s @ typical Max tracking slew rate: 0.3 @ Acquisition, in baseline Max tracking slew rate: 2 @ Acquisition, up to Max tracking slew rate: 3 @ Tracking, up to Sun exclusion angle: 35 @ Baffle Supply voltage: 5 (nominal) Power consumption: 0.8 W @ OH, typical Power consumption: 1.1 W @ OH, max Power consumption: 2.5 W @ EU, typical Power consumption: 3.4 W @ EU, max Data interface: RS-422 @ EU output data Data interface: UART @ EU output data (variant 2) Update rate: 8 Hz Update rate: 10 Hz @ (variant 2) Flight heritage: Flight proven since 2019 ## ST200 — Berlin Space Technologies [star-trackers] https://newspacemarket.com/products/bst-st200-star-tracker/ Data interface: UART Data interface: RS-422 @ (variant 2) Power consumption: 0.55 W @ 3.7V Envelope (L×W×H): 30x30x39mm³ @ ST200 Envelope (L×W×H): 50x50x83mm³ @ with Baffle 40° Sun Exclusion Mass: 40 g @ ST200 with UART Interface Mass: 106 g @ with Baffle 40° Sun Exclusion Attitude accuracy (cross-boresight): 10 @ pitch & yaw Accuracy around boresight (roll): 70 Update rate: 5 Hz Max tracking slew rate: 0.3 @ pitch, yaw (nominal conditions) Max tracking slew rate: 1 @ pure roll (nominal conditions) Radiation tolerance (TID): 11 krad Design lifetime: 5 years @ LEO Sun exclusion angle: 40 @ with Baffle Limiting star magnitude: 6 Flight heritage: since 2014 ## ZAPHOD CubeSat Structure — AAC Clyde Space [structures] https://newspacemarket.com/products/aac-clyde-zaphod-cubesat-structures/ TRL: 9 Mass: 394 g Mass: 674 g @ (variant 2) Material: Aluminium 7075 & 6082 Form factor: 1 Form factor: 6 @ (variant 2) ## 1P Skeleton Wall PocketQube Structure — Alba Orbital [structures] https://newspacemarket.com/products/1p-skeleton-wall-pocketqube-structure-1479/ Envelope (L×W×H): 1P (Unit) - 50 mm x 50 mm external dimensions. 47 mm x 47 mm internal dimensions (widest point) Flight heritage: Earlier version has Flight Heritage Random vibration: 3.924 Material: Al6082 T6 Material: Steel @ (variant 2) Form factor: 1 Mass: 69 g Operating temperature: -50.2 °C (min) Operating temperature: 89.9 °C (max) ## 2P Skeleton Wall PocketQube Structure — Alba Orbital [structures] https://newspacemarket.com/products/2p-skeleton-wall-pocketqube-structure-1479/ Material: Al6082 T6 Material: Steel @ (variant 2) Mass: 109 g Envelope (L×W×H): 2P (Unit) Envelope (L×W×H): 114 mm x 50 mm x 50 mm @ (variant 2) Envelope (L×W×H): 114 mm x 47 mm x 47 mm @ (variant 3) Flight heritage: Earlier version has Flight Heritage Random vibration: 3.924 ## 3P Skeleton Wall PocketQube Structure — Alba Orbital [structures] https://newspacemarket.com/products/3p-skeleton-wall-pocketqube-structure-1479/ Envelope (L×W×H): 3P (Unit) Envelope (L×W×H): 178 mm x 50 mm x 50 mm @ (variant 2) Envelope (L×W×H): 178 mm x 47 mm x 47 mm @ (variant 3) Flight heritage: Earlier version has Flight Heritage Random vibration: 3.924 Material: Al6082 T6 Material: Steel @ (variant 2) Mass: 151 g Operating temperature: -50.2 °C (min) Operating temperature: 89.9 °C (max) ## Satellite Structure Panels — Beyond Gravity (ex-RUAG Space) [structures] https://newspacemarket.com/products/beyond-gravity-satellite-structure-panels/ Flight heritage: Over 650 OneWeb satellites Envelope (L×W×H): up to 5m Mass: 40000 g (min) Mass: 100000 g (max) Material: Sandwich structure made of CFRP and Aluminium honeycomb ## Coarse Sun Sensor (CSS) Pyramid — Adcole Space (Redwire) [sun-sensors] https://newspacemarket.com/products/adcole-coarse-sun-sensor-pyramid/ Field of view: 2 @ cone Accuracy: 1 ° @ AT NULL (TYPICALLY) Accuracy: 5 ° @ THROUGHOUT LINEAR RANGE Mass: 130 g @ NOMINAL Radiation tolerance (TID): 100 krad Flight heritage: Yes — 1,000+ sensors flown since 1960s ## Miniature Spinning Sun Sensor — Adcole Space (Redwire) [sun-sensors] https://newspacemarket.com/products/adcole-miniature-spinning-sun-sensor/ Field of view: 87.5 @ from normal to spin axis Accuracy: 0.25 ° Supply voltage: 12 (min) Supply voltage: 15 (max) Power consumption: 0.5 W @ less than Mass: 250 g (max) Flight heritage: Yes ## Sun Sensor Stimulator System — Adcole Space (Redwire) [sun-sensors] https://newspacemarket.com/products/adcole-sun-sensor-stimulator-system/ Supply voltage: 120-240 Operating temperature: -30 °C (min) @ approximate Operating temperature: 60 °C (max) @ approximate Flight heritage: decades of flight heritage combined with the agile and innovative culture of a commercial space platform ## Fine Sun Sensor — SSBV Aerospace & Technology [sun-sensors] https://newspacemarket.com/products/ssbv-fine-sun-sensor/ Operating temperature: -25 °C Field of view: 140 @ full cone Update rate: 5 Hz Accuracy: 0.1 ° @ 2 sigma Mass: 35 g Envelope (L×W×H): 34mm x 32mm x 21mm Radiation tolerance (TID): 20 krad @ component level Flight heritage: 14 on-orbit sensors on 4 LEO satellites. ## Star Trackers, Sun Sensors and GPS — Voyager Technologies [sun-sensors] https://newspacemarket.com/products/medium-sun-sensor/ Operating temperature: -40 °C Field of view: 60 @ full-angle circular Accuracy: 1 ° @ 2-axis knowledge Output type: analog Mass: 36 g @ with 1.27m flying leads Envelope (L×W×H): Housing diameter .75” (1.91cm), Flange diameter 1.375” (3.49 cm), Sensor height 0.957” (2.43 cm) Data interface: other @ Four 0 to 3.0mA (typical) current sources on five flying leads Connector: five flying leads: 50 inch (1.27 m) in length, M22759/33-26, 26 AWG wire Design lifetime: 20 years Flight heritage: ALEXIS, HETE, and TERRIERS, and FASTSAT ## Bradford Cosine Sun Sensor (CoSS) — Bradford Space [sun-sensors] https://newspacemarket.com/products/bradford-cosine-sun-sensor/ Mass: 24 g @ Exclusive cable Mass: 50 g @ With 1.5 meter of cable Envelope (L×W×H): 30 x 30 x 14.5 mm3 (exclusive cable fixation provisions) Envelope (L×W×H): Overall height including cable clamp: 35 mm @ (variant 2) Field of view: 160 @ Minimum operational FOV Output type: analog Accuracy: 3 ° @ plusminus, if on-board corrections are made for sun sensor temperature Operating temperature: -50 °C (min) @ Qualification temperature Operating temperature: 80 °C (max) @ Qualification temperature Survival temperature: -145 °C (min) @ qualified excursions Survival temperature: 120 °C (max) @ qualified excursions Radiation tolerance (TID): 100 krad (min) ## Bradford Coarse Sun Sensor (CSS) — Bradford Space [sun-sensors] https://newspacemarket.com/products/bradford-coarse-sun-sensor-css/ Radiation tolerance (TID): 100 krad (min) Mass: 215 g @ Baseline (no strap-on baffle) with rear cover Envelope (L×W×H): 110 x 110 x 30 mm3 @ exclusive dimensions of extensions such as strap-on baffles, bondpin and connectors Field of view: 90 (max) @ Hemispherical Field of view: 12 @ Range for linear output (values given for detector pyramid tilt angle of 22°) Output type: analog @ voltage mode Output type: analog @ current mode Accuracy: 1.5 ° @ on sensor boresight (throughout mission lifetime), without albedo Accuracy: 1 ° @ on sensor boresight (BOL at ambient temp), without albedo Accuracy: 3 ° @ beyond central portion of the FOV (depends on choice for pyramid tilt angle), without albedo Flight heritage: Continuously in production since 1975 and applied in a variety of different applications with spacecraft in LEO, MEO, HEO, GEO, planetary and interplanetary orbits. ## Bradford Redundant Cosine Sun Sensor (COSS-R) — Bradford Space [sun-sensors] https://newspacemarket.com/products/bradford-cosine-sun-sensor-redundant/ Mass: 15 g @ exclusive cable Envelope (L×W×H): 45 x 37 x 6 mm3 ( inclusive cable fixation provisions) Field of view: 180 @ Minimum operational FOV Power consumption: nil @ CoSS-R is passive Accuracy: 3 ° @ plus/minus, if on-board corrections are made for sun sensor temperature Radiation tolerance (TID): 100 krad (min) ## Redwire Coarse Sun Sensor – Cosine Type — Redwire Corporation [sun-sensors] https://newspacemarket.com/products/redwire-coarse-sun-sensor-cosine-type/ Mass: 10 g @ NOMINAL Envelope (L×W×H): 1.10" X 0.74" X 0.47" Envelope (L×W×H): 2.8 CM X 1.9 CM X 1.2 CM @ (variant 2) Radiation tolerance (TID): 100 krad @ Rad hard Flight heritage: GRAIL, Mars Phoenix, GPM, GPIM, LRO/LCROSS, WISE, Kepler, SDO, EMM (Hope), Worldview, Fermi (GLAST), MRO, Deep Impact, Swift, Classified Programs Output type: 500-1300 ## Redwire Sun Sensor Stimulator System — Redwire Corporation [sun-sensors] https://newspacemarket.com/products/redwire-sun-sensor-stimulator-system/ Supply voltage: 120-240 Operating temperature: -30 °C (min) Operating temperature: 60 °C (max) ## SUN SENSOR (AQUILA series) — NewSpace Systems (NSS) [sun-sensors] https://newspacemarket.com/products/nss-aquila-sun-sensors/ Field of view: 140 Update rate: 5 Hz (max) Envelope (L×W×H): 34 mm × 40 mm × 20 mm Power consumption: 0.015 W @ Idle: bootloader mode Power consumption: 0.08 W @ bootloader mode Power consumption: 0.2 W @ application mode Active Mass: 37 g (max) Radiation tolerance (TID): 10 krad @ component Level Supply voltage: 5 @ nominal Data interface: RS-485 Data interface: RS-422 @ (variant 2) Connector: 9-way female Micro-D Design lifetime: 5 years @ in orbit Flight heritage: Over 5 years in Low Earth Orbit (LEO) Accuracy: 0.5 ° (max) Operating temperature: -20 °C ## SS200 — AAC Clyde Space [sun-sensors] https://newspacemarket.com/products/aac-ss200/ Power consumption: 0.015 W (max) Operating temperature: -40 °C TRL: 9 Mass: 3 g Update rate: 100 Hz (max) Update rate: 10 Hz (max) @ (variant 2) Accuracy: 0.3 ° (max) @ +/- 45° Accuracy: 0.3 ° (max) @ +/- 45° range Field of view: 110 Field of view: 110 @ (variant 2) Data interface: I2C Radiation tolerance (TID): 36 krad (min) Supply voltage: 5 Envelope (L×W×H): 24.66 x 15.00 x 3.50 mm Flight heritage: flying since 2018 ## SSOC-D60 — Solar MEMS Technologies [sun-sensors] https://newspacemarket.com/products/solar-mems-ssoc-d60/ Operating temperature: -30 °C (min) Operating temperature: 85 °C (max) Radiation tolerance (TID): 30 krad Flight heritage: Flight heritage since 2009 with hundreds of units in orbit. Field of view: 60 @ half-angle Mass: 35 g Supply voltage: 5 (nominal) Envelope (L×W×H): 60 x 30 x 12 mm Accuracy: 0.3 ° (max) ## FSSA-110 — Berlin Space Technologies [sun-sensors] https://newspacemarket.com/products/fssa-110-fine-sun-sensor-assembly/ Power consumption: 0.185 W Accuracy: 5 ° Update rate: 10 Hz Data interface: RS-422 @ Main Interface Output type: analog @ Sun sensor interface Mass: 102 g @ With 3x sensors Mass: 87 g @ Without sensors Envelope (L×W×H): 95 x 44 x 20 mm Radiation tolerance (TID): 20 krad @ > Field of view: 114 @ one sensor Design lifetime: 5 years Flight heritage: since 2015 ## XFS (Xenon Feed System) — Space Electric Thruster Systems (SETS) [tanks-valves] https://newspacemarket.com/products/sets-xfs-xenon-feed-system/ Operating temperature: -20-60 °C TRL: 9 Media / propellant: Xenon Media / propellant: Krypton @ (variant 2) Operating pressure (MEOP): 180 bar Mass: 1100 g @ Dry mass Envelope (L×W×H): 145 x 127 x 115 Flight heritage: Flight models of these systems, after successful acceptance tests, were sent to the customer as a part of the EPS and currently they are successfully functioning on board the spacecraft. ## VACCO Propellant Latch Valve — VACCO Industries [tanks-valves] https://newspacemarket.com/products/vacco-latch-valves-spacecraft/ Flight heritage: Boeing HS-702 satellite, various Boeing platforms, vehicles resupplying the International Space Station, leading commercial and scientific satellites Supply voltage: 20-54 Operating pressure (MEOP): 137.8952 bar Material: Titanium Mass: 340 g Envelope (L×W×H): 1.13 MAX x 2.19 MAX x 3.22 ## Additive Tank 100ml 1U — Nammo [tanks-valves] https://newspacemarket.com/products/additive-tank-100ml-1u-3131/ Operating temperature: -5 °C Design lifetime: 5 years Material: Titanium Volume: 0.1 L Media / propellant: Butane, Nitrogen Mass: 180 g Operating pressure (MEOP): 10 bar Envelope (L×W×H): 1U x 1U x 0.2U ## Apogee Engine Valve — Nammo [tanks-valves] https://newspacemarket.com/products/apogee-engine-valve-3131/ model_used: SVS06-02, SVS06-07 Media / propellant: N2O4, MON-3, MMH, Hydrazine (N2H4) Operating pressure (MEOP): 22 bar Supply voltage: 18-27 Supply voltage: 26-35.5 @ (variant 2) Power consumption: 38 W Power consumption: 31.5 W @ (variant 2) Mass: 440 g (max) Material: 316L, 304L, 430, PTFE Connector: Flying leads Operating temperature: -29-102 °C Random vibration: 37.68 Envelope (L×W×H): With straight weld tube. ## High Performance Radiator technology (HiPeR) Flexlinks — Airbus Defence and Space [thermal] https://newspacemarket.com/products/airbus-hiper-flexlinks-thermal-straps/ TRL: 9 Thermal conductance: 3.6 (max) Mass: 120 g @ for typical 1 W/K thermal straps Thermal conductance: 1.5 (min) @ PAR-PAR, 60 mm Thermal conductance: 3.6 (max) @ PAR-PAR, 60 mm Thermal conductance: 1.3 (min) @ PAR-PAR, 80 mm Thermal conductance: 3.3 (max) @ PAR-PAR, 80 mm Thermal conductance: 1.2 (min) @ PAR-PAR, 100 mm Thermal conductance: 3 (max) @ PAR-PAR, 100 mm Thermal conductance: 1.1 (min) @ PAR-PAR, 120 mm Thermal conductance: 2.8 (max) @ PAR-PAR, 120 mm Thermal conductance: 1 (min) @ PAR-PAR, 140 mm Thermal conductance: 2.5 (max) @ PAR-PAR, 140 mm Thermal conductance: 0.9 (min) @ PAR-PAR, 160 mm Thermal conductance: 2.4 (max) @ PAR-PAR, 160 mm Thermal conductance: 1.3 (min) @ PAR-PER, 60 mm Thermal conductance: 2.8 (max) @ PAR-PER, 60 mm Thermal conductance: 1.2 (min) @ PAR-PER, 80 mm Thermal conductance: 2.6 (max) @ PAR-PER, 80 mm Thermal conductance: 1.1 (min) @ PAR-PER, 100 mm Thermal conductance: 2.4 (max) @ PAR-PER, 100 mm Thermal conductance: 1 (min) @ PAR-PER, 120 mm Thermal conductance: 2.3 (max) @ PAR-PER, 120 mm Thermal conductance: 0.9 (min) @ PAR-PER, 140 mm Thermal conductance: 2.1 (max) @ PAR-PER, 140 mm Thermal conductance: 0.8 (min) @ PAR-PER, 160 mm Thermal conductance: 2 (max) @ PAR-PER, 160 mm Thermal conductance: 1.1 (min) @ PER-PER, 60 mm Thermal conductance: 2.3 (max) @ PER-PER, 60 mm Thermal conductance: 1 (min) @ PER-PER, 80 mm Thermal conductance: 2.1 (max) @ PER-PER, 80 mm Thermal conductance: 1 (min) @ PER-PER, 100 mm Thermal conductance: 2 (max) @ PER-PER, 100 mm Thermal conductance: 0.9 (min) @ PER-PER, 120 mm Thermal conductance: 1.9 (max) @ PER-PER, 120 mm Thermal conductance: 0.8 (min) @ PER-PER, 140 mm Thermal conductance: 1.8 (max) @ PER-PER, 140 mm Thermal conductance: 0.8 (min) @ PER-PER, 160 mm Thermal conductance: 1.7 (max) @ PER-PER, 160 mm Flight heritage: Flight proven ## Silicone Rubber Heaters — Minco Products, Inc [thermal] https://newspacemarket.com/products/silicone-rubber-heaters/ Operating temperature: -45 °C (min) @ foil Operating temperature: -38.2 °C (max) @ foil Envelope (L×W×H): 560 mm x 2285 mm ## PTFE (Teflon) Heaters — Minco Products, Inc [thermal] https://newspacemarket.com/products/ptfe-teflon-heaters/ Operating temperature: -200 °C (min) Operating temperature: -123.1 °C (max) Envelope (L×W×H): 10"×40" ## Dawn Aerospace Thrusters (B1, B5, B20, B200) — Dawn Aerospace [propulsion] https://newspacemarket.com/products/dawn-b20-green-bipropellant-thruster/ Envelope (L×W×H): 190 x 87 x 82 mm Mass: 695 g Operating temperature: -5 °C (min) Operating temperature: 30 °C (max) Survival temperature: -30 °C (min) Survival temperature: 40 °C (max) Thrust: 6460 mN (min) Thrust: 18110 mN (max) Specific impulse: 271 (min) Min impulse bit: 980 mN·s @ Bi-prop Min impulse bit: 10 mN·s @ Cold-gas Propulsion type: chemical Propellant: Nitrous oxide (N2O) and Propylene (C3H6) Power consumption: 14.67 W @ Hit (per valve) Power consumption: 0.76 W @ Hold (per valve) Power consumption: 4.56 W (max) @ Igniter Flight heritage: 96 in space since 2021. Proven on 16 different spacecrafts. ## AAC Clyde Space PM200 Bi-Propellant Propulsion Module — AAC Clyde Space [propulsion] https://newspacemarket.com/products/aac-clyde-pm200-propulsion-module/ Propulsion type: chemical Thrust: 500 mN @ Nominal Specific impulse: 285 (min) Min impulse bit: 35 mN·s @ Minimum Total impulse: 5 N·s @ Maximum impulse bit Power at thrust: 12 W (max) @ firing Power consumption: 0.1 W (max) @ sleep Design lifetime: 5 years (min) @ Storability Data interface: I2C Data interface: RS-422 @ (variant 2) Data interface: RS-485 @ (variant 3) Total impulse: 850 N·s (min) Thrust: 500 mN Specific impulse: 285 (min) @ vac Operating temperature: -5 to +35 Supply voltage: 5 and 12 Power consumption: 12 W (max) @ during firing Power consumption: 0.1 W (max) @ sleep (variant 2) Envelope (L×W×H): 97.7 x 95.4 x 95.4 mm Feed/tank pressure: 45 bar @ Nom. propellant storage pressures (Ox) Feed/tank pressure: 9 bar @ Nom. propellant storage pressures (Fuel) Mass: 1100 g @ Dry mass (excluding propellant) Propellant mass: 310 g Propellant: nitrous oxide and propene ## WaterCube Propulsion Unit — Capsule Corporation [propulsion] https://newspacemarket.com/products/capsule-watercube/ Propulsion type: water Propellant: demineralised water Mass: 900 g Mass: 1900 g (max) Power consumption: 21 W (max) Specific impulse: 95-110 Total impulse: 150-1100 N·s Thrust: 4 mN Power at thrust: 24 W @ peak (3 minutes) Power at thrust: 21 W @ maximum Power at thrust: 6-17 W @ pulsed Mass: 900-2000 g Supply voltage: 12 V or 28 V Data interface: CAN Data interface: RS-422 @ (variant 2) Connector: 1 power connector micro D-sub Connector: 1 signal connector micro D-sub @ (variant 2) Propellant mass: 170 g @ 0.7U Mass: 900 g @ Margined Wet Mass, 0.7U Total impulse: 158 N·s @ 0.7U @ 95 s Isp Total impulse: 183 N·s @ 0.7U @ 110 s Isp Propellant mass: 430 g @ 1U Mass: 1210 g @ Margined Wet Mass, 1U Total impulse: 401 N·s @ 1U @ 95 s Isp Total impulse: 464 N·s @ 1U @ 110 s Isp Propellant mass: 830 g @ 1.5U Mass: 1740 g @ Margined Wet Mass, 1.5U Total impulse: 771 N·s @ 1.5U @ 95 s Isp Total impulse: 895 N·s @ 1.5U @ 110 s Isp Propellant mass: 1050 g @ 1.8U Mass: 2000 g @ Margined Wet Mass, 1.8U Total impulse: 975 N·s @ 1.8U @ 95 s Isp Total impulse: 1129 N·s @ 1.8U @ 110 s Isp Specific impulse: 95.1 Power at thrust: 20.3 W @ at 95.1 s Isp Specific impulse: 100.8 @ (variant 2) Power at thrust: 22.7 W @ at 100.8 s Isp Specific impulse: 106.2 @ (variant 3) Power at thrust: 25.2 W @ at 106.2 s Isp Specific impulse: 110.7 @ (variant 4) Power at thrust: 27.6 W @ at 110.7 s Isp Thrust: 1-3 mN @ Average Thrust (pulsed mode) Min impulse bit: 3 mN·s @ at 4 mN thrust/unit Lead time: 3.25 ## ASET Air-Scooping Electric Thruster — Viridian Space [propulsion] https://newspacemarket.com/products/viridian-aset-air-scooping-electric-thruster/ Propulsion type: electric @ general Propellant: atmospheric gas @ general Power at thrust: 1300 W @ orbit-averaged available power Propellant: air @ optimized Specific impulse: 2000 @ operating with xenon Specific impulse: 4643 @ minimum requirement with Cd=3.5 and scoop efficiency=0.3 ## Dawn Aerospace Green Chemical Propulsion Thrusters (B1, B5, B20, B200) — Dawn Aerospace [propulsion] https://newspacemarket.com/products/dawn-b20-thruster/ Envelope (L×W×H): 190 × 87 × 82 mm Mass: 695 g Operating temperature: -5-30 °C Survival temperature: -30-40 °C Thrust: 6460-18110 mN Specific impulse: 271 (min) Min impulse bit: 980 mN·s @ Bi-prop Min impulse bit: 10 mN·s @ Cold-gas Power consumption: 14.67 W @ Valve power Hit Power consumption: 0.76 W @ Valve power Hold Power consumption: 4.56 W @ Igniter max Propellant: Nitrous oxide (N2O) and Propylene (C3H6) Flight heritage: 96 in space since 2021. Proven on 16 different spacecrafts. ## CHIPS — CubeSat High Impulse Propulsion System — CU Aerospace [propulsion] https://newspacemarket.com/products/cua-chips/ Propulsion type: electric @ resistojet Envelope (L×W×H): 10 cm x 9 cm x 6 cm Total impulse: 180 N·s Propellant: R134a Propellant mass: 277 g Mass: 1027 g Power consumption: 20 W @ thrusting Thrust: 15 mN @ warm gas Thrust: 15 mN @ cold gas Specific impulse: 67 @ warm gas Specific impulse: 45 @ cold gas Total impulse: 176 N·s @ warm gas Total impulse: 118 N·s @ cold gas Min impulse bit: 0.1 mN·s (max) Time to thrust: 600 s @ max continuous thrust time Design lifetime: 3 years (min) @ from propellant load Propellant: R236fa @ alternate ## Thrusters for very small satellites (Engines for ultra-small spacecraft) — D-Start [propulsion] https://newspacemarket.com/products/dstart-micro-propulsion-engine/ Propulsion type: chemical Propellant: аммиак Mass: 10 g (min) @ космического аппарата ## Green mono-propellant Micro Propulsion System (MiPS) — VACCO Industries [propulsion] https://newspacemarket.com/products/vacco-green-mips-3u-propulsion/ Propulsion type: chemical Thrust: 100 mN Total impulse: 3320 N·s @ total @10°C Propellant: ADN green (LMP-103S/LT) Propellant: Air Force green (AF-M315E) @ (variant 2) Propellant mass: 2000 g Feed/tank pressure: 5.17 bar @ Propellant MDP Feed/tank pressure: 29.1 bar @ GHe MDP Power consumption: 1 W @ health and status monitoring Power consumption: 10 W (max) @ Standby Power Power consumption: 1 W @ Warmup Power Power consumption: 15 W (max) @ Thruster Operating Power (4 thrusters) Mass: 3000 g (max) @ Dry Mass Mass: 5000 g (max) @ Wet Mass 95% Fill @ 10°C Envelope (L×W×H): 8.860 in (225.0 mm) x 4.080 in (103.6 mm) x 5.784 in (146.9 mm) Supply voltage: 5±0.25 VDC @ Operating Voltage For Telemetry Supply voltage: 9.5-12.6 VDC @ Operating Voltage For Heaters & Valves Data interface: RS-422 Operating temperature: 10°C to 40°C Survival temperature: -34°C to 60°C Flight heritage: Flight systems currently in production. ## Standard Micro Propulsion System (MiPS) — VACCO Industries [propulsion] https://newspacemarket.com/products/vacco-standard-mips-cold-gas/ Propulsion type: cold-gas Thrust: 25 mN @ per thruster Total impulse: 82 N·s @ X19039000-01 Total impulse: 219 N·s @ X19039000-02 Total impulse: 336 N·s @ X19039000-03 Total impulse: 515 N·s @ X19039000-04 Propellant: R236fa Propellant mass: 209 g @ X19039000-01 Propellant mass: 557 g @ X19039000-02 Propellant mass: 857 g @ X19039000-03 Propellant mass: 1314 g @ X19039000-04 Feed/tank pressure: 6.89 bar @ MEOP/MDP Mass: 639 g @ dry mass, X19039000-01 Mass: 799 g @ dry mass, X19039000-02 Mass: 956 g @ dry mass, X19039000-03 Mass: 1144 g @ dry mass, X19039000-04 Envelope (L×W×H): 100 x 100 x 36 (X19039000-01) Envelope (L×W×H): 100 x 100 x 70 (X19039000-02) @ (variant 2) Envelope (L×W×H): 100 x 100 x 100 (X19039000-03) @ (variant 3) Envelope (L×W×H): 100 x 100 x 144 (X19039000-04) @ (variant 4) Supply voltage: 9-12.6 @ Operating Power consumption: 1 W @ Standby, Max. Power consumption: 12 W @ Warmup, Max. Power consumption: 12 W @ Thruster Operating (4 thrusters), Max. Power consumption: 1 W (max) @ communication and health monitoring Data interface: RS-422 Operating temperature: -15-55 °C Survival temperature: -30-55 °C ## NASA C-POD Micro Propulsion System — VACCO Industries [propulsion] https://newspacemarket.com/products/vacco-nasa-c-pod-propulsion/ Propulsion type: cold-gas Propellant: R236fa Feed/tank pressure: 6.8948 bar @ MDP Thrust: 10 mN @ Nominal Continuous Thrust Specific impulse: 40 Total impulse: 174 N·s Min impulse bit: 0.5 mN·s Mass: 1330 g @ with Propellant Supply voltage: 9-12.6 Power consumption: 0.25 W @ Max Standby Power Consumption Power consumption: 5 W @ Max Power (2 Thrusters) Data interface: RS-422 Operating temperature: -20-60 °C Survival temperature: -34-60 °C ## APPMAX3 Deployable Thruster Pointing Mechanism — Beyond Gravity (ex-RUAG Space) [propulsion] https://newspacemarket.com/products/beyond-gravity-appmax3-pointing-mechanism/ Mass: 28000 g @ approx. Envelope (L×W×H): up to 2 m boom length ## BHT-1500 — Busek Co. [propulsion] https://newspacemarket.com/products/busek-bht-1500-hall-effect-thruster/ Propulsion type: electric @ Hall Effect Thruster Propellant: Xenon Propellant: Krypton @ (variant 2) Propellant: Iodine @ (variant 3) Power at thrust: 1500 W @ Discharge Power Power at thrust: 1000 W (min) @ Throttle Range Power at thrust: 2700 W (max) @ Throttle Range Thrust: 101 mN @ Nominal Thrust Specific impulse: 1710 @ Nominal Specific Impulse Total impulse: 6.5 N·s (min) @ Predicted Total Impulse Mass: 6300 g @ Thruster Mass Mass: 300 g @ Cathode Mass Thrust: 120 mN (min) @ orbit-raising mode Specific impulse: 1700 @ orbit-raising mode Power at thrust: 1800 W @ orbit-raising mode Thrust: 100 mN (min) @ station-keeping mode Specific impulse: 1900 @ station-keeping mode Power consumption: 1000 W @ High Thrust Mode Thrust: 68 mN @ High Thrust Mode (1000 W) Specific impulse: 1615 @ High Thrust Mode (1000 W) Power consumption: 1500 W @ High Thrust Mode (variant 2) Thrust: 101 mN @ High Thrust Mode (1500 W) Specific impulse: 1710 @ High Thrust Mode (1500 W) Power consumption: 1800 W @ High Thrust Mode (variant 3) Thrust: 120 mN @ High Thrust Mode (1800 W) Specific impulse: 1740 @ High Thrust Mode (1800 W) Power consumption: 2000 W @ High Thrust Mode (variant 4) Thrust: 134 mN @ High Thrust Mode (2000 W) Specific impulse: 1700 @ High Thrust Mode (2000 W) Power consumption: 2400 W @ High Thrust Mode (variant 5) Thrust: 158 mN @ High Thrust Mode (2400 W) Specific impulse: 1735 @ High Thrust Mode (2400 W) Power consumption: 2700 W @ High Thrust Mode (variant 6) Thrust: 179 mN @ High Thrust Mode (2700 W) Specific impulse: 1865 @ High Thrust Mode (2700 W) Power consumption: 1000 W @ High Isp Mode Thrust: 58 mN @ High Isp Mode (1000 W) Specific impulse: 1860 @ High Isp Mode (1000 W) Power consumption: 1500 W @ High Isp Mode (variant 2) Thrust: 87 mN @ High Isp Mode (1500 W) Specific impulse: 1895 @ High Isp Mode (1500 W) Power consumption: 1800 W @ High Isp Mode (variant 3) Thrust: 103 mN @ High Isp Mode (1800 W) Specific impulse: 1940 @ High Isp Mode (1800 W) Power consumption: 2000 W @ High Isp Mode (variant 4) Thrust: 118 mN @ High Isp Mode (2000 W) Specific impulse: 1915 @ High Isp Mode (2000 W) Power consumption: 2400 W @ High Isp Mode (variant 5) Thrust: 143 mN @ High Isp Mode (2400 W) Specific impulse: 2045 @ High Isp Mode (2400 W) Power consumption: 2700 W @ High Isp Mode (variant 6) Thrust: 154 mN @ High Isp Mode (2700 W) Specific impulse: 2035 @ High Isp Mode (2700 W) ## Paladin — Magdrive [propulsion] https://newspacemarket.com/products/magdrive-paladin/ Propulsion type: electric Thrust: 1 mN Specific impulse: 1000 Propellant: iodine Mass: 250 g Envelope (L×W×H): 40 x 40 x 50 mm Supply voltage: 3.3 (nominal) Design lifetime: 15 years ## FireStar Fusion Drive — Miles Space / RocketStar [propulsion] https://newspacemarket.com/products/miles-space-firestar-fusion-drive/ Propulsion type: electric @ fusion-enhanced pulsed plasma Propellant: water (boronated for fusion) ## Redundant SmallSat Propulsion Controller — VACCO Industries [propulsion] https://newspacemarket.com/products/vacco-redundant-propulsion-controller/ Propulsion type: chemical Envelope (L×W×H): 5.750 x 5.000 x 3.000 Supply voltage: 9-13 @ option 1 Supply voltage: 24-32 @ option 2 Power consumption: 1 W @ Standby power Data interface: RS-422 Operating temperature: -20-60 °C Survival temperature: -30-70 °C Radiation tolerance (TID): 22 krad Design lifetime: 5 years Flight heritage: LEO (NanoACE) to Mars (MarCO) ## Micro R³ — ENPULSION GmbH [propulsion] https://newspacemarket.com/products/micro-r%c2%b3/ Propulsion type: electric Total impulse: 26000 N·s @ at 2,700 s Isp at nominal thrust Specific impulse: 2700 @ at nominal thrust Thrust: 0.5 mN @ precision Specific impulse: 2700 (min) Specific impulse: 3600 (max) Propellant: indium Propellant mass: 1250 g Thrust: 0.5 mN (min) @ DYNAMIC THRUST RANGE Thrust: 1 mN (max) @ DYNAMIC THRUST RANGE Thrust: 1 mN @ NOMINAL THRUST Specific impulse: 2700 @ AT 1mN Propellant mass: 1250 g @ (variant 2) Total impulse: 26000 N·s @ AT 1mN Power at thrust: 64 W (min) @ TOTAL SYSTEM POWER AT THRUST RANGE Power at thrust: 120 W (max) @ TOTAL SYSTEM POWER AT THRUST RANGE Power consumption: 110 W @ AT NOMINAL THRUST incl. neutralizer Envelope (L×W×H): 140 x 120 x 126.5 mm @ Excluding protrusions Envelope (L×W×H): 140 x 120 x 131.5 mm @ Including protrusions Mass: 2700 g @ DRY INCLUDING PPU Mass: 3950 g @ WET INCLUDING PPU Power consumption: 12 W (min) @ HOT STANDBY POWER Power consumption: 18 W (max) @ HOT STANDBY POWER Data interface: RS422 Data interface: RS485 @ (variant 2) Supply voltage: 28 ## AIS-VAT0-DEMO Educational DIY Micro Vacuum Arc Thruster Kit — Applied Ion Systems [propulsion] https://newspacemarket.com/products/applied-ion-systems-ais-vat0-demo/ Power consumption: 2.5 W Lead time: 4 Propulsion type: electric Power at thrust: 2.5 W Envelope (L×W×H): 50x50x21mm Propellant: Bismuth Supply voltage: 5 @ Input ## MT-B — VENG S.A. [propulsion] https://newspacemarket.com/products/veng-mca2/ Propulsion type: chemical Propellant: LOX/RP1 Specific impulse: 366 @ en VAC ## MOTOR MT-B — VENG S.A. [propulsion] https://newspacemarket.com/products/veng-m150-series/ Propulsion type: chemical Propellant: LOX/RP1 Specific impulse: 366 @ in VAC ## NANO Dragsail — Frond Space Systems [propulsion] https://newspacemarket.com/products/frond-nano-dragsail/ Mass: 250 g Connector: 5-way Molex Picoblade Data interface: I2C Data interface: CAN @ (variant 2) Operating temperature: -30 °C Supply voltage: 3.3 ## GEM3 Green Electric Monopropellant — Digital Solid State Propulsion [propulsion] https://newspacemarket.com/products/dssp-gem3-monopropellant-2/ Propellant: Hydroxylammonium Nitrate/2,2'-dipyridyl/Ammonium Nitrate/Water/1,2,4-triazole/1H-pyrazole Propulsion type: chemical ## SRS-3 Full-duplex S-band Transceiver — Satlab A/S [radios] https://newspacemarket.com/products/satlab-srs-3/ Frequency band: S @ TX Frequency band: S @ RX Frequency: 2200-2290 MHz @ TX Frequency: 2025-2110 MHz @ RX TX power: 0.1-1 W RX sensitivity: -107 @ <1 % PER, 128 kBd, BT=0.5 Modulation: GMSK Mass: 190 g Envelope (L×W×H): 87.0 mm × 93.0 mm × 17.0 mm Supply voltage: 5-40 Power consumption: 0.55 W @ Idle/Awaiting frames Power consumption: 5 W @ Full-duplex transmit and receive Data interface: CAN Data interface: RS-422 @ (variant 2) Data interface: Ethernet @ (variant 3) Operating temperature: -40-85 °C @ RX Operating temperature: -40-70 °C @ TX Survival temperature: -40-85 °C Radiation tolerance (TID): 20 krad @ board level Flight heritage: 2018 Connector: Amphenol coaxial SMP Connector: Harwin Gecko @ (variant 2) Power consumption: 0.185 W @ Additional input power for Ethernet enabled Power consumption: 0.11 W @ Additional input power for RS-422 enabled ## NewSpace S-Band Transceiver — Rakon Limited [radios] https://newspacemarket.com/products/rakon-ns-sband-transceiver/ Frequency band: S @ TX Frequency band: S @ RX Frequency: 2200-2290 MHz @ TX Frequency: 2000-2100 MHz @ RX TX power: 2 W @ max TX power: 1.995 W @ max (variant 2) Data rate: 5000 kbps @ TX, max Data rate: 5000 kbps @ RX, max Data rate: 5000 kbps @ max baud rate Modulation: BPSK / QPSK / GMSK Mass: 250 g @ Short missions Mass: 300 g @ Long missions Envelope (L×W×H): 95 x 95 x 50 mm @ Short missions Envelope (L×W×H): 95 x 95 x 60 mm @ Long missions Supply voltage: 5-28 Supply voltage: 6 @ Supply voltage, Short missions Supply voltage: 5 @ Power amplifier, Short missions Supply voltage: 22-37 @ Power amplifier input range, Long missions Power consumption: 12 W @ TX, max Power consumption: 1.2 W @ Receiving mode, @6V, Short missions Power consumption: 0.05 W @ Receiving mode, @5V, Short missions Power consumption: 1.2 W @ Transmitting mode (CW), @6V, Short missions Power consumption: 10 W @ Transmitting mode (CW), @5V, Short missions Data interface: CAN Data interface: RS-422 @ (variant 2) Connector: SMA or MMCX @ RF, Short missions Connector: CSP @ CAN, Short missions Connector: Molex or Harwin @ RS 485, Short missions Operating temperature: -20-60 °C Survival temperature: -30-70 °C Radiation tolerance (TID): 50 krad @ Long missions Design lifetime: 1 years @ min, Short missions Design lifetime: 12 years @ Long missions ## AAC Clyde Space PULSAR-XTX X-Band Transmitter — AAC Clyde Space [radios] https://newspacemarket.com/products/aac-clyde-pulsar-xtx/ Frequency band: X @ TX Frequency: 8025-8375 MHz TX power: 2 W TX power: 1.995 W @ (variant 2) Data rate: 10000-50000 kbps @ TX Modulation: OQPSK or QPSK Mass: 130 g (max) Envelope (L×W×H): 96 mm x 90 mm x 11.7 mm Supply voltage: 6.2-17 Power consumption: 15 W (max) Data interface: SPI Data interface: LVDS @ (variant 2) Connector: 50 Ω SMP connector Operating temperature: -25-61 °C Design lifetime: 2 years Design lifetime: 2 years @ LEO ## W-Band Transmitter Module — celtonn [radios] https://newspacemarket.com/products/celtonn-w-band-transmitter/ Frequency band: Ka @ TX TX power: 0.032 W @ nominal output power TX power: 0.2 W @ maximum output power Supply voltage: 5 @ typical Supply voltage: 7 @ max ## RADIOSAT Ka-Band Datalink Transmitter — PicoSaTs [radios] https://newspacemarket.com/products/picosats-radiosat-ka-band-datalink-transmitter/ Frequency band: Ka @ Downlink Frequency: 25500-27000 MHz @ Downlink TX power: 5 W (max) Data rate: 4000000 kbps (max) @ transmission Modulation: DVB-S2X with ACM (up to 256 APSK) Mass: 500 g (max) Supply voltage: 12-24 Power consumption: 70 W (max) Data interface: CAN @ System telemetry and control Data interface: Ethernet @ System telemetry and control (opt.) Data interface: RS-422 @ System telemetry and control (opt.) (variant 2) Data interface: SpaceWire @ Data over SpaceFibre (opt.) Data interface: Ethernet @ Data over SpaceFibre (opt.) (variant 2) Data interface: other @ Data over SpaceFibre Connector: SMP gold plated RF connectors Connector: Space qualified data and power connectors @ (variant 2) Operating temperature: -20-70 °C Survival temperature: -30-90 °C ## Pulsar HSTX — AAC Clyde Space [radios] https://newspacemarket.com/products/aac-pulsar-hstx/ Frequency band: S @ TX Frequency: 2400-2450 MHz @ amateur Frequency: 2400-2450 MHz @ PULSAR-HSTX-A TX power: 0.251-1 W TX power: 1 W @ max Data rate: 10000 kbps @ TX (HSTX-A) Data rate: 10000 kbps @ TX (HSTX-A) (variant 2) Modulation: OQPSK Modulation: QPSK @ (variant 2) Mass: 100 g (max) Envelope (L×W×H): 96 mm x 90 mm x 17.41 mm Supply voltage: 6-12 Supply voltage: 5 @ alternative Power consumption: 5 W (max) @ maximum RF power output Power consumption: 5 W (max) Data interface: I2C @ Low-speed (telemetry and control) Data interface: SPI @ High-speed (payload data) Connector: 50 Ω SMA connector Operating temperature: -25-61 °C Design lifetime: 2 years @ LEO ## Pulsar STX — AAC Clyde Space [radios] https://newspacemarket.com/products/aac-pulsar-stx/ Frequency band: S @ commercial Frequency band: S @ amateur Frequency: 2200-2300 MHz @ PULSAR-STX-C Frequency: 2400-2450 MHz @ PULSAR-STX-A TX power: 0.251-1 W Data rate: 2000 kbps (max) @ TX Modulation: O/QPSK Modulation: QPSK @ (variant 2) Modulation: OQPSK @ (variant 3) Mass: 100 g (max) Envelope (L×W×H): 96 mm (Length) x 90 mm (Width) x 16.9 mm (Height) Supply voltage: 6-12 Supply voltage: 5 @ alternative Power consumption: 5 W (max) @ maximum RF power output Power consumption: 5 W (max) Data interface: I2C @ telemetry and control Data interface: SPI @ payload data Connector: 50 Ω SMA connector Operating temperature: -25-51 °C Design lifetime: 2 years @ in LEO Flight heritage: UKube-1 mission Design lifetime: 2 years @ LEO ## Pulsar-VUTRX — AAC Clyde Space [radios] https://newspacemarket.com/products/aac-pulsar-vutrx/ Frequency band: VHF @ uplink Frequency band: UHF @ downlink Frequency: 140-150 MHz @ VHF Frequency: 400-420 MHz @ UHF, VUTRX-C Frequency: 430-440 MHz @ UHF, VUTRX-A TX power: 0.501-1.995 W Data rate: 9.6 kbps @ GMSK Data rate: 1.2 kbps @ AFSK RX sensitivity: -117 @ for 12 dB SINAD Modulation: GMSK Modulation: AFSK @ (variant 2) Mass: 100 g (max) Envelope (L×W×H): 96 mm (Length) x 90 mm (Width) x 16.51 mm (Height) Supply voltage: 3.3-5 Power consumption: 3-5.5 W @ TX Power consumption: 0.162 W @ RX Power consumption: 0.162 W (max) @ low-power receiver Data interface: I2C Operating temperature: -25-61 °C ## Ka-Band Frequency Agile Transceiver TR400 — ReliaSat [radios] https://newspacemarket.com/products/arralis-tr400-ka-band-frequency-agile-transceiver/ Frequency band: Ka @ TX Frequency band: Ka @ RX Frequency: 17300-20700 MHz @ TX output Frequency: 27500-30500 MHz @ RX input TX power: 0.316-0.501 W @ TX Output Power, P1dB Supply voltage: 6-60 @ Upconverter Supply Voltage Range Power consumption: 10 W @ Upconverter at 28 VDC Operating temperature: -40-85 °C @ Upconverter Operating Temperature Range Supply voltage: 6-60 @ Downconverter Supply Voltage Range Power consumption: 6 W @ Downconverter at 28 VDC Operating temperature: -40-85 °C @ Downconverter Operating Temperature Range Envelope (L×W×H): 95.89 x 90.17 x 38.14 mm @ Mechanical Enclosure Dimensions Mass: 1000 g (max) @ Total Mass Connector: SMPM edge mount @ RF Connector Types for Receiver Connector: SMP edge mount @ RF Connector Types for Transmitter Connector: Harwin 4-pin Connector @ DC Connector Types Connector: SMP edge mounts @ IF Signal Connector Types Connector: Harwin 12-pin Connector @ Current Sensor, Temperature Sensor, Frequency Synthesiser Lock & DC Power Enable Connections, MC ## Ka-Band Satellite Transponder TR500 — ReliaSat [radios] https://newspacemarket.com/products/arralis-tr500-ka-band-satellite-transponder/ Frequency band: Ka @ RX Frequency band: Ka @ TX Frequency: 17000-21000 MHz @ RX input Frequency: 27000-31000 MHz @ TX output TX power: 0.501 W @ saturated Connector: SMP Connector: SMPM RF connectors @ (variant 2) Connector: DC Flying Leads @ DC power Connector: 6-Pin Pico-Lock @ DC power enable, PLL lock, current and temperature sensor Frequency: 17000-21000 MHz @ TX Output (variant 2) TX power: 0.501 W @ Saturated (Pin=-15 dBm) TX power: 0.398 W @ at P1dB Compression (Pin=-14 dBm) Supply voltage: 7-42 Power consumption: 11.5 W (max) @ TX, @ 12 VDC Frequency: 27000-30000 MHz @ RX Input (variant 2) Supply voltage: 7-42 @ (variant 2) Power consumption: 6 W (max) @ RX, @ 12 VDC Mass: 2000 g (max) Connector: SMPM edge mount @ RF Connector: DC flying leads @ DC Connector: SMP edge mounts @ IF Signal Connector: 6-pin Pico-Lock Connector @ Current Sensor, Temperature Sensor, Frequency Synthesiser Lock & DC Power Enable Connections Operating temperature: -40-85 °C Radiation tolerance (TID): 50 krad ## K/Ka-Band Uplink Transceiver UDC300 — ReliaSat [radios] https://newspacemarket.com/products/arralis-udc300-k-ka-uplink-transceiver/ Frequency band: Ka @ TX Frequency band: K @ RX Frequency: 27000-30000 MHz @ TX output Frequency: 17000-21000 MHz @ RX input TX power: 0.1 W @ TX Output Linear Power Mass: 430 g Envelope (L×W×H): 95.89 x 90.17 x 38.15 mm @ Mechanical Enclosure Dimensions Supply voltage: 7-42 @ TX Supply voltage: 7-42 @ RX Power consumption: 12 W (max) @ TX Power consumption: 7.5 W (max) @ RX Connector: SMPM edge mount @ RF Connector Types Connector: DC flying leads @ DC Connector Types Connector: SMP edge mounts @ IF Signal Connector Types Connector: 6-pin Pico-Lock Connector @ Current Sensor, Temperature Sensor, Frequency Synthesiser Lock & DC Power Enable Connections Operating temperature: -40-85 °C ## Ka-Band Integrated Transceiver Module UDC400 — ReliaSat [radios] https://newspacemarket.com/products/arralis-udc400-ka-band-integrated-transceiver-module/ Frequency band: Ka @ TX Frequency band: Ka @ RX Frequency: 17000-21000 MHz @ TX Output Frequency: 27000-30000 MHz @ RX Input TX power: 0.501 W @ Saturated Output Power TX power: 0.398 W @ P1dB Compression Mass: 430 g (typical) Envelope (L×W×H): 95.89 x 90.17 x 38.15 mm @ Mechanical Enclosure Supply voltage: 7-42 @ TX Supply voltage: 7-42 @ RX Power consumption: 11.5 W (max) @ TX, @ 12 VDC Power consumption: 6 W (max) @ RX, @ 12 VDC Connector: SMP and SMPM RF connectors Connector: DC Flying Leads @ (variant 2) Connector: 6-Pin Pico-Lock connectors @ (variant 3) Operating temperature: -40-85 °C Flight heritage: Rocket Labs Mission 18, OHB SatComm ## TA1017 — Triad RF Systems [radios] https://newspacemarket.com/products/triad-rf-ta1017/ Frequency: 1700 MHz (min) @ Operating Frequency: 2400 MHz (max) @ Operating TX power: 1.585 W @ 64QAM Power Output, 20 MHz BW, -27 dB EVM Limit TX power: 25.119 W @ BPSK Power Output, 20 MHz BW, -7 dB EVM Limit TX power: 31.623 W @ Saturated Power Output, CW Sweep at Design Limit Supply voltage: 10 (min) Supply voltage: 30 (max) Envelope (L×W×H): 125.1 x 64.3 x 17.8 in (mm) Mass: 113 g Connector: SMA-F / SMA-F @ RF Connectors (Input / Output) Connector: MDM-15SH034B @ Power / Signal Connector Operating temperature: -40 °C (min) Operating temperature: 85 °C (max) Survival temperature: -55 °C (min) Survival temperature: 85 °C (max) ## RFX-400 — Tiger Innovations, Inc. [radios] https://newspacemarket.com/products/tiger-innovations-rfx-400-uhf-transceiver/ Frequency band: UHF @ TX and RX Frequency: 387-464 MHz TX power: 8.1 W (max) TX power: 0.001 W (min) Data rate: 1.2-500 kbps RX sensitivity: -122 Modulation: 2-FSK, GFSK, MSK, OOK, and flexible ASK shaping Mass: 53 g @ approx. Envelope (L×W×H): 1.8”Lx2.8”Wx0.75”H Supply voltage: 7.5-18 Power consumption: 0.2 W @ Receive Data interface: RS-232 Data interface: RS-422 @ (variant 2) Data interface: LVDS @ (variant 3) Data interface: other @ TTL Connector: SMA ## MCR4 High Performance SCPC Receiver — SpaceBridge Inc. [radios] https://newspacemarket.com/products/mcr4-high-performance-scpc-receiver/ Modulation: DVB-S2X, GSE encapsulation, QPSK up to 256APSK LDPC/BCH @ RX Frequency band: L @ RX Frequency: 950 MHz (min) @ satellite / band independent Frequency: 2400 MHz (max) @ satellite / band independent Connector: F-type/75 Ω @ IFL input Connector: N-type/50 Ω @ IFL input, option RX sensitivity: -5 @ Max composite allowed over entire L-band RX sensitivity: -65 @ over 36MHz transponder, min RX sensitivity: -20 @ over 36MHz transponder, max Data interface: Ethernet @ user data ports Data rate: 2000000 kbps @ RX, max Envelope (L×W×H): 17” x 1.72” x 18” W x H x D (435 x 45 x 457) Mass: 5440 g Supply voltage: 100 (min) @ universal power supply Supply voltage: 240 (max) @ universal power supply Power consumption: 70 W @ Consumption Operating temperature: 0 °C (min) Operating temperature: 50 °C (max) ## RGTR-A — RevGo [radios] https://newspacemarket.com/products/revgo-rgtr-a-10w/ Frequency band: Ka @ TX Frequency: 29000-30000 MHz @ TX RF Frequency TX power: 10 W @ Output Power TX power: 10 W @ Rated/Saturated Frequency band: Ka @ RX Frequency: 17700-18700 MHz @ Rx Frequency Quad-band Frequency: 18450-19450 MHz @ Rx Frequency Quad-band (variant 2) Frequency: 19200-20200 MHz @ Rx Frequency Quad-band (variant 3) Frequency: 20200-21200 MHz @ Rx Frequency Quad-band (variant 4) Frequency: 18200-20200 MHz @ Rx Frequency Dual-Band Frequency: 19200-21200 MHz @ Rx Frequency Dual-Band (variant 2) Mass: 1400 g Envelope (L×W×H): 150x140x58 mm Envelope (L×W×H): 5.90*5.51*1.97 inches @ (variant 2) Envelope (L×W×H): 150x140x58 mm @ (variant 3) Supply voltage: 18-55 @ TX Power Supply Power consumption: 10 W @ TX Power Consumption Power consumption: 60 W @ Prated (including Fan) typ. Power consumption: 70 W @ Prated (including Fan) max Supply voltage: 12-24 @ RX Power Supply Power consumption: 6 W @ RX Power Consumption Data interface: RS422 Data interface: RS485 @ (variant 2) Connector: N-Type @ IF Connector Connector: F-Type @ IF Connector optional Connector: 4-Pin @ MS Connector for Power supply Connector: TE T4130012081-000 4-pin @ for M&C Operating temperature: -40-60 °C ## VSAT Satellite Beacon Receiver BR400L — C-COM Satellite Systems [radios] https://newspacemarket.com/products/br-400l-beacon-receiver/ Frequency: 950 MHz (min) @ input Frequency: 2200 MHz (max) @ input RX sensitivity: -105 (min) @ Input Power Level RX sensitivity: -20 (max) @ Input Power Level Mass: 5000 g Envelope (L×W×H): 4.5 cm (1.75”) H; 34 cm (13.5”) D 48 cm (19“) W Supply voltage: 100 (min) Supply voltage: 240 (max) Power consumption: 2.5 W @ max Data interface: RS-232 @ M&C Data rate: 19200 kbps @ M&C Connector: Type F, Female STD @ Input Connector: N-type Female @ Input (Optional) Connector: DB-9, Male @ M & C Connector: DB-9, Female @ Streaming (optional) Operating temperature: -20 °C (min) Operating temperature: 60 °C (max) Survival temperature: -40 °C (min) Survival temperature: 80 °C (max) ## AAC SpaceQuest STS-300 CubeSat AIS Receiver — AAC Clyde Space [radios] https://newspacemarket.com/products/aac-clyde-sts-300-ais-receiver/ Frequency band: VHF @ RX Frequency: 156-163 MHz @ Tunable in 1 kHz Steps RX sensitivity: -95 @ at 90% Throughput Mass: 180 g @ Including Aluminum Enclosure Envelope (L×W×H): 95.9mm x 90.2mm x 20mm @ Cubesat Configuration Envelope (L×W×H): 80mm x 85mm x 20mm @ Samtec FT5 Configuration Supply voltage: 2.5-5 Power consumption: 0.4-0.65 W Data interface: other @ 115 kHz Asynchronous Serial, 3.3 Volt TTL Connector: 104-pin CubeSat Standard Connector: 60-pin Samtec FT5 @ (variant 2) Flight heritage: Flight proven ## AAC SpaceQuest RX-2000 S-Band Receiver — AAC Clyde Space [radios] https://newspacemarket.com/products/aac-clyde-rx-2000-s-band-receiver/ Frequency band: S Frequency: 2000-2400 MHz Data rate: 9.6-153.6 kbps Modulation: FM, GFSK RX sensitivity: -117 @ @ 9600bps RX sensitivity: -110 @ @128Kbps Supply voltage: 6-16 Power consumption: 1.5 W @ 6 -16 VDC @ 200mA Mass: 200 g Envelope (L×W×H): 135 mm x 50 mm x 25 mm Operating temperature: -30-75 °C Survival temperature: -40-85 °C Data interface: other @ Received Data Output Data interface: other @ Recovered Data Clock Output (Differential or Single Ended) Data interface: other @ Receiver Control Input & Output Connector: 15 Pin Micro Miniature Military D @ Data/Power Connector: SMA Female @ RF Flight heritage: in operation on-orbit for over 30 years for our own satellite and for a wide range of blue-chip clients around the globe. ## Model 4426 2U/3U Digital RF Receiver Dual / Quad Channel — GDP Space Systems [radios] https://newspacemarket.com/products/gdp-model-4426-rf-telemetry-receiver/ Frequency band: S @ RX Frequency: 2185-2485 MHz @ S-Band (Std) Frequency band: L @ RX (variant 2) Frequency: 1700-1850 MHz @ UL-Band (Std) Frequency band: L @ RX (variant 3) Frequency: 1427-1545 MHz @ LL-Band (Std) Frequency band: C @ RX (optional) Frequency: 4400-5250 MHz @ C-Band (optional) Frequency band: UHF @ RX (optional) (variant 2) Frequency: 100-1150 MHz @ CIF (P) -Band (optional) Frequency: 100-1100 MHz @ CIF (P)-Band (optional) Data rate: 0.05-0.01 kbps @ BPSK (Std) Data rate: 20000 kbps @ BPSK (Optional) Data rate: 0.005-0.01 kbps @ PCM/FM (Std) Data rate: 20000 kbps @ PCM/FM (Optional) Data rate: 0.05-0.02 kbps @ QPSK (Std) Data rate: 40000 kbps @ QPSK (Optional) Data rate: 0.01-0.01 kbps @ PCM/FM (Std) (variant 2) Data rate: 20000 kbps @ PCM/FM (Optional) (variant 2) Data rate: 0.05-0.01 kbps @ PCM/FM & BPSK (Std) Data rate: 20000 kbps @ PCM/FM & BPSK (Optional) Data rate: 0.1-0.02 kbps @ QPSK/SOQPSK (Std) Data rate: 40000 kbps @ QPSK/SOQPSK (Optional) Envelope (L×W×H): 2U Rack-Mountable Chassis Envelope (L×W×H): 1U* @ Optional Modulation: PCM/FM (ARTM Tier 0) @ Std Modulation: SOQPSK (ARTM Tier 1) @ Std (variant 2) Modulation: CPM (ARTM Tier 2) @ Optional Modulation: BPSK/QPSK/OQPSK Modulation: UQPSK* @ Optional (variant 2) Modulation: AQPSK* @ Optional (variant 3) Modulation: BPSK @ (variant 2) Modulation: QPSK @ (variant 3) Modulation: OQPSK @ (variant 4) Modulation: UQPSK @ (variant 5) Modulation: AQPSK @ (variant 6) Modulation: GMSK @ (variant 7) Modulation: SOQOSK ARTM Tier 1 @ (variant 8) Operating temperature: 10-40 °C Survival temperature: -40-70 °C Data interface: Ethernet Data interface: other @ TTL Data interface: RS-422 @ (variant 2) Data interface: Ethernet @ Data Output Data interface: Ethernet @ Control Interface ## Model 4460 Portable Digital RF/IF Receiver — GDP Space Systems [radios] https://newspacemarket.com/products/gdp-model-4460-portable-rf-receiver/ Envelope (L×W×H): 10.75 x 12 x 1.75 inch chassis Frequency band: S @ RF Frequencies Frequency: 2185-2485 MHz @ RF Frequencies S Band Frequency band: L @ RF Frequencies Upper L Band Frequency: 1700-1850 MHz @ RF Frequencies Upper L Band Frequency band: L @ RF Frequencies Lower L Band Frequency: 1427-1545 MHz @ RF Frequencies Lower L Band Frequency: 550-1100 MHz @ RF Frequencies, optional Modulation: BPSK Modulation: QPSK @ (variant 2) Modulation: OQPSK @ (variant 3) Modulation: UQPSK @ optional Modulation: AQPSK @ optional (variant 2) Modulation: SOQPSK (ARTM Tier 1) @ optional (variant 3) Modulation: Analog FM & PCM/FM @ optional (variant 4) Modulation: GMSK @ optional (variant 5) Modulation: PM / PSK @ optional (variant 6) Data rate: 50-10000 kbps @ BPSK Data rate: 20000 kbps @ BPSK, optional Data rate: 100-20000 kbps @ QPSK Data rate: 40000 kbps @ QPSK, optional Data interface: Ethernet @ Byte Aligned Data Output, optional Data interface: TTL Data interface: RS-422 @ (variant 2) Data interface: VME/PCI Bus @ Remote Control, optional Data interface: RS232 @ Remote Control, optional (variant 2) Data interface: RS-485 @ Remote Control, optional (variant 3) Data interface: Ethernet @ Remote Control, optional (variant 4) Frequency: 2185-2485 MHz @ RF S Band Frequency: 1700-1850 MHz @ RF Upper L Band Frequency: 1427-1545 MHz @ RF Lower L Band Data rate: 10-10000 kbps @ PCM/FM Demodulator, standard Data rate: 20000 kbps @ PCM/FM Demodulator, optional Data rate: 50-10000 kbps @ PCM/FM & BPSK Bit Synchronizer(s) Data rate: 20000 kbps @ PCM/FM & BPSK Bit Synchronizer(s), optional Data rate: 100-20000 kbps @ QPSK/SOQPSK Bit Synchronizer(s) Data rate: 40000 kbps @ QPSK/SOQPSK Bit Synchronizer(s), optional Data interface: TTL @ Data Output, Standard Data interface: RS-422 @ Data Output, Standard (variant 2) Data interface: Ethernet @ Data Output, optional Data interface: Ethernet @ Control Interface, Standard Operating temperature: 10-40 °C Survival temperature: -40-70 °C ## Model RDM207 Digital RF Receiver — GDP Space Systems [radios] https://newspacemarket.com/products/gdp-model-rdm207-pci-rf-receiver/ Frequency: 2185-2485 MHz @ RF Frequency Frequency: 1700-1850 MHz @ RF Frequency (variant 2) Frequency: 1427-1545 MHz @ RF Frequency (variant 3) Frequency: 100-1100 MHz @ RF Frequency (* optional) Frequency: 4400-5250 MHz @ RF Frequency (* optional) (variant 2) Modulation: BPSK @ PSK Demodulators Modulation: QPSK @ PSK Demodulators (variant 2) Modulation: OQPSK @ PSK Demodulators (variant 3) Modulation: UQPSK * @ PSK Demodulators (variant 4) Modulation: AQPSK * @ PSK Demodulators (variant 5) Modulation: GMSK * @ PSK Demodulators (variant 6) Modulation: SOQOSK @ PSK Demodulators (variant 7) Modulation: ARTM Tier 0/1* @ PSK Demodulators (variant 8) Data rate: 1000-10000000 kbps @ PCM/FM Demodulator Data Rate Data rate: 20000 kbps @ PCM/FM Demodulator Data Rate (* optional) Data rate: 0.05-10 kbps @ Bit Synchronizer PCM/FM & BPSK Data rate: 20000 kbps @ Bit Synchronizer PCM/FM & BPSK (* optional) Data rate: 0.1-20 kbps @ Bit Synchronizer QPSK/SOQPSK Data rate: 40000 kbps @ Bit Synchronizer QPSK/SOQPSK (* optional) Data interface: TTL @ Data Output Data interface: RS-422 @ Data Output (variant 2) Data interface: Ethernet @ Data Output (IRIG 218, IRIG-106 Ch-10*, HDLC/AX.25*) Data interface: other @ PCI Bus (Control Interface) Data interface: Ethernet @ Control Interface (* optional) Envelope (L×W×H): PCI Single Slot @ Form Factor Operating temperature: 10-40 °C @ Operational Survival temperature: -40-85 °C @ Storage ## ODALISS TTC — Emxys [radios] https://newspacemarket.com/products/emxys-ttc/ Frequency band: VHF @ TX and RX Frequency band: UHF @ TX and RX (variant 2) TX power: 1.259 W @ maximum TX power: 1.25 W @ maximum (variant 2) Data rate: 1.2 kbps (min) @ selectable Data rate: 115.2 kbps (max) @ selectable Data rate: 0.05 kbps @ Beacon mode RX sensitivity: -110 @ BER <10-5 Modulation: 2FSK @ output radio frequency Modulation: 3FSK @ alternatively Modulation: 4FSK @ alternatively (variant 2) Modulation: GMFSK @ alternatively (variant 3) Modulation: 2FSK Radioteletype (RTTY) ASCII-8 @ Beacon mode Mass: 41 g Envelope (L×W×H): 87mm x 87mm x 9.3mm Supply voltage: 5.8 (min) Supply voltage: 8.4 (max) Supply voltage: 7.6 (nominal) Data interface: UART Data interface: I2C @ (variant 2) Connector: One 80-pin high-speed backplane connector Operating temperature: -45 °C (min) Operating temperature: 85 °C (max) ## W-Band Receiver Module (WB-RX-9296-LN) — celtonn [radios] https://newspacemarket.com/products/celtonn-w-band-receiver/ Frequency band: Ka @ RX Frequency: 91000 MHz (min) @ RF Input Frequency: 97000 MHz (max) @ RF Input RX sensitivity: -100 (max) @ minimum usable sensitivity Supply voltage: 5 (nominal) Supply voltage: 7 (max) ## Audio Management Systems (Orion™, ADAMS NexGen, Radio Gateway) — Orbit Communication Systems [radios] https://newspacemarket.com/products/orion-airborne-audio-management-system/ Envelope (L×W×H): 146 x 85 x 165 mm @ per CCP Mass: 1950 g @ per CCP Power consumption: 24 W @ per CCP Supply voltage: 28 (nominal) @ per CCP Operating temperature: -15-55 °C @ continuous Operating temperature: -40-70 °C @ short-time Survival temperature: -55-85 °C Data interface: Ethernet ## TTRM2005DR — Triad RF Systems [radios] https://newspacemarket.com/products/triadrf-ttrm2005dr-2200-2500-dual-mimo-bda/ Frequency band: S @ TX Frequency band: S @ RX Frequency: 2200 MHz (min) @ TX Frequency: 2500 MHz (max) @ TX TX power: 25.119 W @ PSat Data rate: 54000 kbps @ OFDM, 64QAM modulation, 20 MHz BW Data rate: 36000 kbps @ OFDM, 16QAM modulation, 20 MHz BW Data rate: 12000 kbps @ OFDM, QPSK modulation, 20 MHz BW Data rate: 9000 kbps @ OFDM, BPSK modulation, 20 MHz BW Modulation: 3-4G telecom, WLAN, OFDM, DVB, CW/AM/FM Envelope (L×W×H): 3.25 x 3.75 x 1.9 in Supply voltage: 12 (min) Supply voltage: 28 (nominal) Supply voltage: 30 (max) Connector: TNC-F / TNC-F (RF) Connector: Circular Locking (DC / Control) @ (variant 2) Operating temperature: -20 °C (min) Operating temperature: 85 °C (max) ## THPR1060 Triad High Power Radio — Triad RF Systems [radios] https://newspacemarket.com/products/triadrf-thpr1060-s-band-120w-mimo-radio/ Frequency: 2200-2500 MHz Frequency band: S @ TX/RX TX power: 120 W TX power: 30 W @ per channel TX power: 50 W @ Per MIMO Stream (5 Mbps) TX power: 10 W @ Per MIMO Stream (20+ Mbps) Supply voltage: 22-32 Supply voltage: 22-32 @ (variant 2) Power consumption: 25.2 W @ Idle, 28V supply Power consumption: 126 W @ Average Operating, 5 Mbps, 28V supply Power consumption: 112 W @ Average Operating, 20+ Mbps, 28V supply Data interface: USB Data interface: USB @ (variant 2) Data interface: RS232 @ (variant 3) Data interface: Ethernet @ (variant 4) Connector: TNC-F @ Antenna RF Connectors Connector: 801-011-07M10-2PA @ DC Connector Connector: 801-011-07M13-37PA @ Signal Connector Operating temperature: -40-55 °C Envelope (L×W×H): 233.93 x 146.55 x 135.89 mm Mass: 3912 g ## Compact Frequency Converters and Receivers for FSS/BSS Payloads — Beyond Gravity (ex-RUAG Space) [radios] https://newspacemarket.com/products/beyond-gravity-compact-frequency-converters-receivers-fss-bss/ Frequency band: C @ input Frequency: 5800-7000 MHz @ input, C-band Frequency band: Ku @ input (variant 2) Frequency: 12750-14800 MHz @ input, Ku-band Frequency band: K @ input (variant 3) Frequency: 17300-18400 MHz @ input, K-band Frequency band: C @ output Frequency: 3400-4800 MHz @ output, C-band Frequency band: Ku @ output (variant 2) Frequency: 10700-12750 MHz @ output, Ku-band Frequency: 13400-13650 MHz @ output, Ku-band (variant 2) Operating temperature: -20-70 °C Supply voltage: 28-100 Power consumption: 10 W @ nominal Mass: 700 g @ Converter Mass: 780 g @ Receiver Envelope (L×W×H): 140 x 50 x 92 mm @ Converter Envelope (L×W×H): 160 x 50 x 112 mm @ Receiver Connector: SMA @ RF input Connector: Waveguide (WR75/WR62) @ RF input (variant 2) Connector: SMA @ RF output Connector: MDM-25 @ DC & TM/TC Design lifetime: 15 years Flight heritage: 1300 FSS/BSS Units delivered Flight heritage: 700 Ka-band Channels delivered @ (variant 2) Flight heritage: 10 000 years accumulated operational time in orbit @ (variant 3) ## Ka-band Compact Frequency Receiver and Converter — Beyond Gravity (ex-RUAG Space) [radios] https://newspacemarket.com/products/beyond-gravity-ka-band-compact-frequency-receiver-converter/ Frequency band: Ka @ input Frequency band: Ka @ output Frequency: 24500 MHz (min) @ input, 24/17 Converter/Receiver Frequency: 25500 MHz (max) @ input, 24/17 Converter/Receiver Frequency: 27500 MHz (min) @ input, 30/20 Converter/Receiver Frequency: 31000 MHz (max) @ input, 30/20 Converter/Receiver Frequency: 17300 MHz (min) @ output, 24/17 Converter/Receiver Frequency: 17800 MHz (max) @ output, 24/17 Converter/Receiver Frequency: 17700 MHz (min) @ output, 30/20 Converter/Receiver Frequency: 21200 MHz (max) @ output, 30/20 Converter/Receiver RX sensitivity: -20 (nominal) @ Converter RX sensitivity: -50 (nominal) @ Receiver Mass: 770 g Envelope (L×W×H): 142 x 104 x 54 mm Supply voltage: 28 (min) Supply voltage: 100 (max) Power consumption: 10 W @ consumption Operating temperature: -20 °C (min) Operating temperature: 70 °C (max) Flight heritage: Beyond Gravity Space has been supplying high performance and highly reliable microwave communication equipment for telecom satellites for more than 35 years. > 1300 FSS/BSS Units delivered > 700 Ka-band Channels delivered > 10 000 years accumulated operat ## C band SSPAs & BUCs — TTI Norte [radios] https://newspacemarket.com/products/tti-norte-c-band-sspa-buc/ Frequency band: C @ Outdoor Frequency: 5.850- 6.425 GHz @ Outdoor TX power: 800 W @ Outdoor SSPA/BUC Standalone Frequency band: C @ Indoor Frequency: 5.850- 6.425 GHz @ Indoor TX power: 800 W @ Indoor SSPA/BUC Standalone ## Cryogenic LNA portfolio — TTI Norte [radios] https://newspacemarket.com/products/tti-norte-cryogenic-lna/ Frequency band: X Frequency: 8400-8500 MHz Power consumption: 0.065 W @ @P1dB 5 dBm Envelope (L×W×H): 48 x 48 x 77 mm Mass: 108 g Connector: RF input: WR112 (UBR84) Connector: RF sample: SMA (f) / SMA (m) @ (variant 2) Connector: RF output: SMA (f) / SMA (m) @ (variant 3) Connector: DC: Micro D 9-P @ (variant 4) Operating temperature: -271.2--258.2 °C ## TA1007 — Triad RF Systems [radios] https://newspacemarket.com/products/triad-rf-ta1007/ Frequency: 500 MHz Frequency: 2800 MHz @ (variant 2) Frequency: 500-2800 MHz TX power: 5 W @ P1dB Power consumption: 22.8 W @ Typical operating (12V, 1.9A) Power consumption: 12 W @ Typical quiescent (12V, 1.0A) Envelope (L×W×H): 5 x 2.5 x 0.553 in Mass: 7 g @ without heatsink Mass: 17 g @ with heatsink Connector: SMA-F / SMA-F (RF Input / Output) Connector: Feedthru Pins (DC / Control) @ (variant 2) ## TA1029 — Triad RF Systems [radios] https://newspacemarket.com/products/triad-rf-ta1029/ Frequency: 6400-7100 MHz TX power: 25.119 W @ PSat Supply voltage: 9-36 Envelope (L×W×H): 6 x 2.5 x 1.06 in Connector: SMA-F / SMA-F @ RF Connectors (Input / Output) Connector: 7W2 Male @ DC / Control Connector Operating temperature: -40-85 °C ## TA1049 — Triad RF Systems [radios] https://newspacemarket.com/products/triad-rf-ta1049/ Frequency: 700 MHz (min) @ Operating Frequency Frequency: 6000 MHz (max) @ Operating Frequency TX power: 0.355 W (min) @ 64QAM Power Output, 20 MHz BW, -27 dB EVM Limit TX power: 3.162 W (min) @ BPSK Power Output, 20 MHz BW, -7 dB EVM Limit TX power: 10 W (typical) @ Saturated Power Output, CW Sweep at Design Limit Modulation: any signal type and modulation format Mass: 227 g Envelope (L×W×H): 95.3 x 50.8 x 27 Supply voltage: 9 (min) @ Supply Voltage Range Supply voltage: 36 (max) @ Supply Voltage Range Connector: SMA-F / SMA-F @ RF Connectors (Input / Output) Connector: DA7W2PA00LF @ Power / Signal Connector Operating temperature: -40 °C (min) @ Housing Temp. Operating temperature: 85 °C (max) @ Housing Temp. Survival temperature: -55 °C (min) Survival temperature: 85 °C (max) ## TA1056 SISO Power Amplifier — Triad RF Systems [radios] https://newspacemarket.com/products/triad-rf-ta1056/ Frequency: 20 MHz (min) Frequency: 1000 MHz (max) TX power: 5.012 W @ 64QAM Power Output, 20 MHz BW, -27 dB EVM Limit TX power: 25.119 W @ BPSK Power Output, 20 MHz BW, -7 dB EVM Limit TX power: 39.811 W @ Saturated Power Output CW Sweep at Design Limit Modulation: any signal type and modulation format Mass: 198 g Envelope (L×W×H): 101.3 x 58.4 x 21.6 mm Supply voltage: 27 (min) Supply voltage: 30 (max) Data interface: other @ Temperature Monitor Output Connector: SMA-F / SMA-F @ RF Connectors (Input / Output) Connector: M80-5401042 @ Power / Signal Connector Operating temperature: -40 °C (min) Operating temperature: 85 °C (max) Survival temperature: -55 °C (min) Survival temperature: 85 °C (max) ## TA1140 — Triad RF Systems [radios] https://newspacemarket.com/products/triad-rf-ta1140/ Frequency: 400 MHz (min) Frequency: 450 MHz (max) TX power: 50.119 W @ PSat Power Output Supply voltage: 11 (min) Supply voltage: 13 (max) Operating temperature: -40 °C (min) @ Housing Temp. Operating temperature: 85 °C (max) @ Housing Temp. Envelope (L×W×H): 3.15 x 2.58 x 0.7 in ## TA1160 — Triad RF Systems [radios] https://newspacemarket.com/products/triad-rf-ta1160/ Frequency band: C @ TX Frequency: 5500 MHz @ Operating TX power: 1.995 W (min) @ 64QAM Power Output, 20 MHz BW, -27 dB EVM Limit TX power: 5.012 W (min) @ BPSK Power Output, 20 MHz BW, -7 dB EVM Limit TX power: 19.953 W @ Saturated Power Output, CW Sweep at Design Limit Envelope (L×W×H): 152.4 x 63.5 x 27 Mass: 482 g Supply voltage: 12 Connector: SMA-F / SMA-F @ RF Input / Output Connector: DA7W2PA00LF @ Power / Signal Operating temperature: -40 °C Survival temperature: -55 °C ## TA1165 5500-8500 MHz 20 W Power Amplifier — Triad RF Systems [radios] https://newspacemarket.com/products/triad-rf-ta1165/ Frequency band: C @ Tx Frequency: 5500 MHz (min) @ Operating Frequency: 8500 MHz (max) @ Operating TX power: 1.995 W @ 64QAM Power Output, 20 MHz BW, -27 dB EVM Limit TX power: 5.012 W @ BPSK Power Output, 20 MHz BW, -7 dB EVM Limit TX power: 19.953 W @ Saturated Power Output, CW Sweep at Design Limit Supply voltage: 12 (min) Supply voltage: 30 (max) Envelope (L×W×H): 152.4 x 63.5 x 27.9 Mass: 482 g Connector: SMA-F / SMA-F @ RF Input / Output Connector: DA7W2PA00LF @ Power / Signal Connector Operating temperature: -40 °C (min) Operating temperature: 85 °C (max) Survival temperature: -55 °C (min) Survival temperature: 85 °C (max) Flight heritage: extensive flight heritage ## TA1216 — Triad RF Systems [radios] https://newspacemarket.com/products/triad-rf-ta1216/ Frequency: 300-6000 MHz TX power: 1 W @ 64QAM Power Output, 20 MHz BW, -27 dB EVM Limit TX power: 15.849 W @ BPSK Power Output, 20 MHz BW, -7 dB EVM Limit TX power: 31.623 W @ Saturated Power Output, CW Sweep at Design Limit Mass: 269 g Envelope (L×W×H): 95.4 x 58.4 x 24.1 mm Supply voltage: 12-30 Data interface: other @ Temperature Monitor Output, Temp in DegC = (Vout - 0.5V) * 100 Connector: SMA-F / SMA-F (RF Connectors) Connector: MDM-21SCBRP (Power / Signal Connector) @ (variant 2) Operating temperature: -40-85 °C Survival temperature: -55-85 °C ## TTRM1116 — Triad RF Systems [radios] https://newspacemarket.com/products/triad-rf-ttrm1116/ Frequency: 1200 MHz (min) @ Operating Frequency: 1400 MHz (max) @ Operating TX power: 39.811 W @ PSat Power Output Supply voltage: 10 (min) @ Operating Supply voltage: 28 (max) @ Operating Envelope (L×W×H): 4.93 x 2.53 x 0.7 in Connector: SMA-F / SMA-F @ RF Connectors (Input / Output) Connector: 15 Pin Micro-D @ DC / Control Connector Operating temperature: -40 °C (min) Operating temperature: 85 °C (max) Data rate: 54000 kbps @ TX, 64QAM OFDM Data rate: 36000 kbps @ TX, 16QAM OFDM Data rate: 12000 kbps @ TX, QPSK OFDM Data rate: 9000 kbps @ TX, BPSK OFDM Modulation: OFDM, 64QAM Modulation: OFDM, 16QAM @ (variant 2) Modulation: OFDM, QPSK @ (variant 3) Modulation: OFDM, BPSK @ (variant 4) ## TTRM1123D — Triad RF Systems [radios] https://newspacemarket.com/products/triad-rf-ttrm1123d/ Frequency: 2200 MHz (min) Frequency: 2500 MHz (max) TX power: 63.096 W @ PSat, per channel Supply voltage: 27 (min) Supply voltage: 30 (max) Envelope (L×W×H): 4.95 x 8.35 x 1.31 in Connector: TNC / TNC @ RF Input / Output Connector: Circular Locking @ DC / Control Operating temperature: -40 °C (min) @ Housing Temp. Operating temperature: 85 °C (max) @ Housing Temp. Data rate: 54000 kbps @ 64QAM, 20 MHz BW TX power: 10 W (min) @ 64QAM, 20 MHz BW Data rate: 36000 kbps @ 16QAM, 20 MHz BW TX power: 20 W (min) @ 16QAM, 20 MHz BW Data rate: 12000 kbps @ QPSK, 20 MHz BW TX power: 35 W (min) @ QPSK, 20 MHz BW Data rate: 9000 kbps @ BPSK, 20 MHz BW TX power: 50 W (min) @ BPSK, 20 MHz BW ## TTRM2002 — Triad RF Systems [radios] https://newspacemarket.com/products/triad-rf-ttrm2002/ Frequency band: S @ TX/RX Frequency: 2200-2500 MHz TX power: 10 W @ PSat Power Output Data rate: 54000 kbps @ OFDM MODULATION 64QAM Data rate: 36000 kbps @ OFDM MODULATION 16QAM Data rate: 12000 kbps @ OFDM MODULATION QPSK Data rate: 9000 kbps @ OFDM MODULATION BPSK Modulation: 3-4G telecom, WLAN, OFDM, DVB, CW/AM/FM Envelope (L×W×H): 2.3 x 2.3 x 0.45 in Supply voltage: 10-30 Data interface: other @ DC / Control Connector, TTL signals Connector: SMP-M / SMP-M @ RF Connectors (Input / Output) Connector: 12 Pin Rectangular Locking @ DC / Control Connector Operating temperature: -40-85 °C ## TTRM4005QR — Triad RF Systems [radios] https://newspacemarket.com/products/triad-rf-ttrm4005qr/ Frequency band: C @ TX and RX Frequency: 4400-5000 MHz TX power: 25.119 W @ PSat Power Output (PER CHANNEL) TX power: 5 W @ 64QAM, 54 Mbps TX power: 10 W @ 16QAM, 36 Mbps TX power: 16 W @ QPSK, 12 Mbps TX power: 20 W @ BPSK, 9 Mbps Data rate: 54000 kbps @ 64QAM Data rate: 36000 kbps @ 16QAM Data rate: 12000 kbps @ QPSK Data rate: 9000 kbps @ BPSK Modulation: any signal type and modulation format, including but not limited to 3-4G telecom, WLAN, OFDM, DVB, and CW/AM/FM Modulation: 64QAM @ (variant 2) Modulation: 16QAM @ (variant 3) Modulation: QPSK @ (variant 4) Modulation: BPSK @ (variant 5) Envelope (L×W×H): 11.02 x 4.77 x 2.5 in Supply voltage: 12-28 Connector: TNC-F / TNC-F @ RF Connectors (Input / Output) Connector: Circular Locking @ DC / Control Connector Operating temperature: -40-85 °C ## TTRM4310 — Triad RF Systems [radios] https://newspacemarket.com/products/triad-rf-ttrm4310/ Frequency: 5000-6000 MHz @ Operating Frequency TX power: 39.811 W @ PSat Power Output Supply voltage: 10-30 @ Operating Voltage Data rate: 54000 kbps @ OFDM modulation 64QAM Data rate: 36000 kbps @ OFDM modulation 16QAM Data rate: 12000 kbps @ OFDM modulation QPSK Data rate: 9000 kbps @ OFDM modulation BPSK Operating temperature: -40-85 °C @ Housing Temp. Envelope (L×W×H): 5.3 x 3.25 x 0.6 in ## TTRM4402R — Triad RF Systems [radios] https://newspacemarket.com/products/triad-rf-ttrm4402r/ Frequency: 5000-5300 MHz @ Operating TX power: 10 W @ PSat Power Output Supply voltage: 10-14 @ Operating Envelope (L×W×H): 2.73 x 2.53 x 1.313 in Connector: SMA-F / SMA-F (RF Input / Output) Connector: 10 Pin Circular Locking (DC / Control) @ (variant 2) Operating temperature: -40-85 °C @ Housing Temp. Modulation: OFDM, 64QAM Data rate: 54000 kbps @ 64QAM TX power: 2 W @ 64QAM (802-11G) Modulation: OFDM, 16QAM @ (variant 2) Data rate: 36000 kbps @ 16QAM TX power: 4 W @ 16QAM (802-11G) Modulation: OFDM, QPSK @ (variant 3) Data rate: 12000 kbps @ QPSK TX power: 6 W @ QPSK (802-11G) Modulation: OFDM, BPSK @ (variant 4) Data rate: 9000 kbps @ BPSK TX power: 10 W @ BPSK (802-11G) ## TTRM4510 — Triad RF Systems [radios] https://newspacemarket.com/products/triad-rf-ttrm4510/ Frequency band: C @ TX Frequency band: C @ RX Frequency: 5300-5900 TX power: 50 W Modulation: any signal type and modulation format, including but not limited to 3-4G telecom, WLAN, OFDM, DVB, and CW/AM/FM Mass: 13 g Envelope (L×W×H): 5.3 x 3.25 x 0.6 in Supply voltage: 10-14 Power consumption: 7 W @ TX max current Power consumption: 100 W @ RX current Data interface: other @ RF Input / Output Connector: SMA-F / SMA-F @ RF Input / Output Data interface: other @ DC / Control Connector: 21 Pin Micro-D @ DC / Control Operating temperature: -40-+85 Data rate: 54000 kbps @ 64QAM Data rate: 36000 kbps @ 16QAM Data rate: 12000 kbps @ QPSK Data rate: 9000 kbps @ BPSK ## RGUC-A Mid Power — RevGo [radios] https://newspacemarket.com/products/revgo-rguc-a-mid-power-20w/ Frequency band: Ka @ TX Frequency: 27500-31000 MHz @ TX Frequency: 950-1950 MHz @ IF TX power: 20 W Mass: 3300 g Envelope (L×W×H): 206*136*88 Supply voltage: 36-72 Power consumption: 135 W @ PLin Output Power consumption: 180 W @ Rated Output Connector: WR28-G (Grooved) @ RF Output Connector: N-Type Female @ IF Connector: ACS02E10SL-4P @ Power Connector: PT06E-12-14P @ M&C Operating temperature: -40-60 °C ## RGUC-A Classic — RevGo [radios] https://newspacemarket.com/products/revgo-rguc-a-classic-40w/ wrong_class: Block Up Converter Power consumption: 40 W Envelope (L×W×H): 259*136*136 mm Mass: 6000 g TX power: 40 W ## RGUC-A mPower — RevGo [radios] https://newspacemarket.com/products/revgo-rguc-a-mpower-40w-80w/ Frequency band: Ka @ TX Frequency: 27500000 MHz (min) Frequency: 31000000 MHz (max) TX power: 39.811 W @ Rated/Saturated TX power: 31.623 W @ PLin1 TX power: 25.119 W @ PLin2 TX power: 19.953 W @ PLin Mass: 5800 g Envelope (L×W×H): 269*136*156 mm Supply voltage: 36 (min) Supply voltage: 60 (max) Power consumption: 225 W @ @ PLin Output Power consumption: 300 W @ @ Rated Output Data interface: Ethernet Data interface: RS485/232 @ (variant 2) Connector: WR28-G (Grooved) @ RF Output Connector: N-Type Female @ IF Connector: AMPHENOL C01610C00600012 @ Power Connector: RJ45 @ M&C Operating temperature: -40 °C (min) Operating temperature: 60 °C (max) ## RGUC-A High Power — RevGo [radios] https://newspacemarket.com/products/revgo-rguc-a-high-power-300w/ Frequency band: Ka @ TX Frequency: 27500-30000 MHz @ RF Frequency Frequency: 27500-31000 MHz @ RF Frequency (optional) TX power: 301.995 W @ Rated TX power: 239.883 W @ PLin1 TX power: 190.546 W @ PLin2 TX power: 151.356 W @ PLin3 Supply voltage: 200-240 @ Input Power Power consumption: 1800 W @ @ Plin3 Output Power consumption: 2800 W @ @ Rated Output Data interface: RS-232 Data interface: RS-485 @ (variant 2) Data interface: Ethernet @ (variant 3) Connector: WR34-G (Grooved) @ RF Output Connector: WR28-G (Grooved) @ RF Output (optional) Connector: N-Type Female @ IF Connector: 2.9mm SMA Female @ RF Sample Connector: ACS02E-16-10P @ Power Connector: PT02E-14-19P @ M&C Connector: RJ45 @ Ethernet Connector: PT02E-12-14S @ Redundancy Link Connector: PT02E-12-14P @ Redundancy Switch Envelope (L×W×H): 450x400x230 Mass: 30000 g Operating temperature: -40-60 °C ## uLCT 2 OHA Laser Communication Terminal (Dual Aperture) — Voyager Technologies [radios] https://newspacemarket.com/products/ulct-2-oha-laser-communication-terminal-dual-aperture/ Envelope (L×W×H): 294 X 294 X 274 @ OHA (Single Aperture, for 10 Gbps Quad Head Laser Communication System) Mass: 13000 g @ OHA (Single Aperture, for 10 Gbps Quad Head Laser Communication System) Power consumption: 25 W @ OHA (Single Aperture, for 10 Gbps Quad Head Laser Communication System) ## ST 4000 — Orbcomm [radios] https://newspacemarket.com/products/orbcomm-skywave-st-4000/ Frequency band: L @ Satellite TX power: 1 W @ Satellite Supply voltage: 3.8 (nominal) Supply voltage: 3 (min) Supply voltage: 4.5 (max) Data interface: UART Data interface: USB @ (variant 2) Data interface: I2C @ (variant 3) Envelope (L×W×H): 16.0 x 26.0 x 2.4 mm Mass: 3 g (max) Operating temperature: -40 °C (min) Operating temperature: 85 °C (max) ## ST 9100 — Orbcomm [radios] https://newspacemarket.com/products/orbcomm-skywave-st-9100/ Envelope (L×W×H): 148 x 113 x 47 mm @ excluding mounting feet Envelope (L×W×H): 181 x 113 x 47 mm @ including mounting feet Frequency band: L @ OGx Rx Frequency: 1525-1559 MHz @ OGx Rx Frequency band: L @ OGx Tx Frequency: 1626.5-1660.5 MHz @ OGx Tx Frequency band: L @ IsatData Pro Rx Frequency: 1525-1559 MHz @ IsatData Pro Rx Frequency band: L @ IsatData Pro Tx Frequency: 1626.5-1660.5 MHz @ IsatData Pro Tx Data interface: RS-232 @ Serial Data interface: RS-485 @ Serial (variant 2) Data interface: other @ Serial J1708 Data interface: CAN @ Serial (variant 3) Data interface: other @ Serial 1-Wire Supply voltage: 9-32 Operating temperature: -40-85 °C @ Transceiver and antenna Operating temperature: -20-75 °C @ Back-up battery ## SC 1000 — Orbcomm [radios] https://newspacemarket.com/products/orbcomm-skywave-sc-1000/ Envelope (L×W×H): 224 x 76 x 28 mm Operating temperature: -30 °C (min) @ battery Operating temperature: 70 °C (max) @ battery Survival temperature: -40 °C (min) @ battery Survival temperature: 85 °C (max) @ battery ## ST 6100 — Orbcomm [radios] https://newspacemarket.com/products/orbcomm-skywave-st-6100/ Frequency band: L @ OGx RX Frequency: 1525-1559 MHz @ OGx RX Frequency band: L @ OGx TX Frequency: 1626.5-1660.5 MHz @ OGx TX Frequency band: L @ IsatData Pro RX Frequency: 1525-1559 MHz @ IsatData Pro RX Frequency band: L @ IsatData Pro TX Frequency: 1626.5-1660.5 MHz @ IsatData Pro TX RX sensitivity: -148 @ GPS/Glonass/Beidou/Galileo Acquisition RX sensitivity: -163 @ GPS/Glonass/Beidou/Galileo Tracking Envelope (L×W×H): 12.6 cm x 12.6 cm x 4.9 cm Supply voltage: 9-32 Data interface: RS-232 Data interface: RS-485 @ (variant 2) Operating temperature: -40-85 °C ## ST 2100 — Orbcomm [radios] https://newspacemarket.com/products/orbcomm-skywave-st-2100/ Frequency band: L @ Rx Frequency: 1525-1559 MHz @ Rx Frequency band: L @ Tx Frequency: 1626.5-1660.5 MHz @ Tx Envelope (L×W×H): 12.5 cm x 8.5 cm x 3.6 cm Supply voltage: 9-32 Data interface: RS-232 @ Serial Operating temperature: -40-85 °C ## HIGH POWER GaN C SSPA 1.5kW PHASED COMBINED – Outdoor/Indoor — TTI Norte [radios] https://newspacemarket.com/products/high-power-gan-c-sspa-1-5kw-phased-combined-outdoor-indoor/ Frequency band: C Frequency: 5850000-6425000 MHz TX power: 1318.257 W @ Output power (PSAT (typical)) TX power: 794.328 W @ Linear output power (PLINEAR*) Envelope (L×W×H): 1200 x 1200 x 1000 mm @ Outdoor Envelope (L×W×H): 19” rack cabinet 44 U (H), 1 m (D) @ Indoor Supply voltage: 90-264 Power consumption: 4600 W (max) @ @ PSAT Data interface: RS-485 Data interface: USB @ M&C capability Data interface: Ethernet @ (variant 2) Connector: N (f) @ RF input Connector: CPR-137 Groveed @ RF output Connector: SMA @ RF sample Connector: Ethernet @ M&C Connector: 19-pin MIL circular @ M&C (outdoor) Connector: 15-pin D-Sub @ M&C (indoor) Operating temperature: -30-55 °C @ outdoor Operating temperature: 0-50 °C @ indoor Survival temperature: -40-85 °C ## HIGH POWER GaN C SSPA 2.7kW PHASED COMBINED – Outdoor/Indoor — TTI Norte [radios] https://newspacemarket.com/products/high-power-gan-c-sspa-2-7kw-phased-combined-outdoor-indoor/ Frequency band: C Frequency: 5850 MHz (min) Frequency: 6425 MHz (max) TX power: 2691.535 W @ PSAT (typical) 2.7 kW TX power: 2137.962 W @ PLINEAR* 2.7 kW Modulation: DVB-S, 4Mbaud, Roll-off: 0.25, ModCod QPSK-3/4 @ For single carrier Envelope (L×W×H): 1200 x 1200 x 2000 mm @ Outdoor (2.7 kW) Envelope (L×W×H): 19” rack cabinet 44 U (H), 1 m (D) Qty x1 @ Indoor (2.7 kW) Supply voltage: 90 (min) Supply voltage: 264 (max) Data interface: RS-485 Data interface: USB @ (variant 2) Data interface: Ethernet @ (variant 3) Data interface: other @ Dry-Contacts Data interface: other @ Web user interfaces Connector: N (f) @ RF input Connector: CPR-137 Groveed @ RF output Connector: SMA @ RF sample Connector: Ethernet @ M&C outdoor Connector: 19-pin MIL circular @ M&C outdoor (variant 2) Connector: Ethernet @ M&C indoor Connector: 15-pin D-Sub @ M&C indoor (variant 2) Operating temperature: -30 °C (min) @ outdoor Operating temperature: 55 °C (max) @ outdoor Operating temperature: 0 °C (min) @ indoor Operating temperature: 50 °C (max) @ indoor Survival temperature: -40 °C (min) Survival temperature: 85 °C (max) Power consumption: 2.7 W Power consumption: 2.7 W @ (variant 2) Power consumption: 10 W (max) ## HIGH POWER GaN C SSPA 4.8kW PHASED COMBINED – Outdoor/Indoor — TTI Norte [radios] https://newspacemarket.com/products/high-power-gan-c-sspa-4-8kw-phased-combined-outdoor-indoor/ Power consumption: 4.8 W Power consumption: 4.8 W @ (variant 2) Power consumption: 20 W (max) Frequency band: C @ operating Frequency: 5850000 MHz (min) @ operating Frequency: 6425000 MHz (max) @ operating TX power: 4786.301 W @ PSAT (typical) TX power: 3801.894 W @ PLINEAR Modulation: DVB-S, QPSK-3/4 @ single carrier Envelope (L×W×H): 1200 x 1600 x 2000 mm @ Outdoor Envelope (L×W×H): 19” rack cabinet 44 U (H), 1 m (D), Qty x2 @ Indoor Supply voltage: 90 (min) @ Input Supply voltage: 264 (max) @ Input Data interface: RS-485 Data interface: Ethernet @ (variant 2) Data interface: USB @ (variant 3) Connector: N (f) @ RF input Connector: CPR-137 Groveed @ RF output Connector: SMA @ RF sample Connector: 19-pin MIL circular @ M&C outdoor Connector: 15-pin D-Sub @ M&C indoor Operating temperature: -30 °C (min) @ outdoor Operating temperature: 55 °C (max) @ outdoor Operating temperature: 0 °C (min) @ indoor Operating temperature: 50 °C (max) @ indoor Survival temperature: -40 °C (min) Survival temperature: 85 °C (max) ## RADIOSAT K/Ka-Band Transponder — PicoSaTs [radios] https://newspacemarket.com/products/picosats-radiosat-k-ka-band-transponder/ Frequency band: Ka @ Downlink Frequency band: Ka @ Uplink TX power: 5 W (max) Mass: 700 g Envelope (L×W×H): 93.5 x 114.2 x 45.6 mm Power consumption: 40 W (max) Data interface: RS422 @ telemetry and control Data interface: RS232 @ additional control Connector: 2.92 mm RF connectors Connector: Space qualified data and power connectors @ (variant 2) ## RADIOSAT Ku-Band Transponder — PicoSaTs [radios] https://newspacemarket.com/products/picosats-radiosat-ku-band-transponder/ Frequency band: Ku @ downlink Frequency band: Ku @ uplink Frequency: 10700-12750 MHz @ downlink Frequency: 12750-13250 MHz @ uplink, band 1 Frequency: 13750-14800 MHz @ uplink, band 2 TX power: 5 W (max) Modulation: Fixed Gain Mode (FGM) and Automatic Gain Control mode (AGC) Mass: 1000 g (max) Envelope (L×W×H): 93.5 x 114.2 x 62.1 mm Supply voltage: 12-24 Power consumption: 40 W (max) Data interface: RS-422 @ telemetry and control Data interface: RS-485 @ debug and FW update Connector: 2.92 mm RF connectors Connector: Space qualified data and power connectors @ (variant 2) Operating temperature: -20-70 °C Survival temperature: -30-90 °C ## NanoCom Link IS1 — GomSpace [radios] https://newspacemarket.com/products/nanocom-link-is1/ Frequency band: S @ Inter Satellite Communication Frequency: 2200-2290 MHz @ TDD Modulation: BPSK Data rate: 100 kbps TX power: 0.1 W @ ITU regulation TX power: 1 W @ possible to increase output power Survival temperature: -40-85 °C Supply voltage: 12-32 @ SDR MK3 supply voltage Supply voltage: 8-18 @ ANT2150-ISL main supply voltage Data interface: CAN @ Control Plane Data interface: RS-422 @ Data Plane Data interface: SpaceWire @ Data Plane (variant 2) Connector: Gecko G125-MH10605L1R @ SDR MK3 power supply Connector: PicoLock, 504050-0791 @ ANT2150-ISL power Connector: Gecko G125-MH12005L1R @ SDR MK3 main communication interface Connector: Gecko G125-MH11005L1R @ SDR MK3 SpaceWire interfaces Connector: Picoblade, 53261-0971 @ SDR MK3 debug connector Connector: Picoblade, 53261-0971 @ TR600 AFE CTRL connectors Connector: PicoLock, 504050-1091 @ ANT2150-ISL S-CTRL connector Connector: SMPM Amphenol / 925-126J-51P @ TR600 RF connectors Power consumption: 15 W (max) ## NanoCom ADS-B — GomSpace [radios] https://newspacemarket.com/products/nanocom-ads-b/ Operating temperature: -40 °C Supply voltage: 3.3 Operating temperature: -60 °C @ (variant 2) Survival temperature: -65 °C Supply voltage: -0.3 @ (variant 2) RX sensitivity: -103 @ NB RX sensitivity: -99 @ WB Power consumption: 0.5 W Envelope (L×W×H): 92.0 x 88.9 x 6.2 mm @ without stack connector Connector: SSMCX antenna connector Data interface: I2C Data interface: UART @ console interface Connector: SSMCX @ (variant 2) Connector: PicoBlade @ (variant 3) RX sensitivity: -10 (max) Power consumption: 170 W @ RX, typical Power consumption: 400 W @ RX, max Flight heritage: GOMX-1 mission ## High-Power Amplifiers — ETL Systems [radios] https://newspacemarket.com/products/high-power-amplifiers/ Frequency band: Ku @ KU1 Frequency: 13.75 – 14.50 GHz @ KU1 Frequency band: Ku @ KU2 Frequency: 12.75 – 14.50 GHz @ KU2 Frequency band: Ku @ KU3 Frequency: 13.75 – 14.80 GHz @ KU3 Frequency band: Ku @ KU4 Frequency: 12.75 – 13.25 GHz @ KU4 TX power: 56.0 dBm @ TWT Power, PEAK TX power: 400 W @ TWT Power, PEAK (variant 2) TX power: 55.4 dBm @ Rated (flange) typical TX power: 350 W @ Rated (flange) typical (variant 2) TX power: 49.5 dBm @ Linear, PLIN TX power: 90 W @ Linear, PLIN (variant 2) TX power: 52.5 dBm @ with optional linearizer TX power: 180 W @ with optional linearizer (variant 2) Data interface: RS-485 Data interface: other @ RS232 Data interface: Ethernet @ (variant 2) Envelope (L×W×H): 52cm deep x 26 cm width x 26 cm height Mass: 21KG @ typical Supply voltage: 99-265 VAC @ single phase Power consumption: 1300 VA @ typical Power consumption: 1450 VA @ maximum Operating temperature: -40˚C to +60˚C ## BPBS44 – 100 W 1:1 Redundant S-band Outdoor Power Amplifier — Bonn Hungary Electronics Ltd. [radios] https://newspacemarket.com/products/bpbs44-100-w-11-redundant-s-band-outdoor-power-amplifier/ Power consumption: 100 W Frequency band: S Frequency: 2025-2120 MHz TX power: 100 W @ @ P3dB Supply voltage: 110-240 Data interface: Ethernet Data interface: RS-485 @ Optional Connector: AC: MS3102E18-10P Connector: Ethernet: Amphenol MS3112E12-10S @ (variant 2) Connector: RF IN: N–female @ (variant 3) Connector: Sample: N–female @ (variant 4) Connector: RF OUT: N–female @ (variant 5) Mass: 52500 g Envelope (L×W×H): 873 x 610 x 204 mm Operating temperature: -40-60 °C ## LEOLINK64 Ka-Band Active Beam Steering Antenna — ReliaSat [antennas] https://newspacemarket.com/products/arralis-leolink64-ka-band-active-beam-steering-antenna/ Frequency band: Ka Frequency: 27500000-30000000 MHz @ Transmit Frequency: 17700000-20200000 MHz @ Receive Gain: 22 @ Transmit, 0 degree scan Gain: 18.6 @ Transmit, 60 degree scan Gain: 21.9 @ Receive, 0 degree scan Gain: 18.4 @ Receive, 60 degree scan Beamwidth: 13.6 @ Transmit, 0 degree scan Beamwidth: 22.4 @ Transmit, 60 degree scan Beamwidth: 14.2 @ Receive, 0 degree scan Beamwidth: 23.2 @ Receive, 60 degree scan Polarization: circular Polarization: LHCP, RHCP @ Transmit Polarization: LHCP, RHCP @ Receive Antenna type: Beam Steering Antenna Envelope (L×W×H): 110.5 x 90.5 mm @ Transmit board size Envelope (L×W×H): 120 x 90.5 mm @ Receive board size Power consumption: 9.6 W @ DC Power Consumption, Transmit Power consumption: 6.4 W @ DC Power Consumption, Receive Connector: 2.92 (K) mm @ Transmit Connector: 2.92 (K) mm @ Receive ## LEOLINK200 Ka-Band High-Capacity Beam Steering Antenna — ReliaSat [antennas] https://newspacemarket.com/products/arralis-leolink200-ka-band-beam-steering-antenna/ Frequency band: Ka Frequency: 27500-31000 MHz @ Transmit Frequency: 17700-21200 MHz @ Receive Gain: 34 @ Transmit, 0O scan Gain: 30 @ Transmit, 60O scan Gain: 34 @ Receive, 0O scan Gain: 30 @ Receive, 60O scan Beamwidth: 3.4 @ HPBW, Transmit, 0O scan Beamwidth: 5.9 @ HPBW, Transmit, 60O scan Beamwidth: 3.6 @ HPBW, Receive, 0O scan Beamwidth: 6.2 @ HPBW, Receive, 60O scan Polarization: circular Polarization: LHCP, RHCP @ Transmit Polarization: LHCP, RHCP @ Receive Antenna type: phased array Mass: 2500 g Envelope (L×W×H): 810 x 320 x 50 mm Supply voltage: 12-50 Data interface: other @ NMEA Data interface: other @ UBX Data interface: other @ Asynchronous Connector: Rugged SMA @ RF Transmit Connector: 2.92 (K) mm @ RF Receive Connector: RG45 @ Interface Operating temperature: -60-120 °C ## Ka-Band Flat Panel Array Antenna PAN-5151-64-KA — ReliaSat [antennas] https://newspacemarket.com/products/arralis-pan-5151-64-ka-ka-band-flat-panel-array-antenna/ Frequency band: Ka Frequency: 27000 MHz (min) Frequency: 31000 MHz (max) Polarization: LHCP Polarization: RHCP @ (variant 2) Antenna type: Flat Panel Array Frequency: 27000 MHz (min) @ Matching Frequency Range Frequency: 31000 MHz (max) @ Matching Frequency Range Polarization: LHCP @ (variant 3) Polarization: RHCP @ (variant 4) Gain: 20 Beamwidth: 13 Connector: K (rear mounted) Envelope (L×W×H): 51 x 51 mm ## Antenna Feeder System — TTI Norte [antennas] https://newspacemarket.com/products/tti-norte-antenna-feeder-system/ Frequency band: X Frequency: 8200 MHz (min) Frequency: 12400 MHz (max) Gain: 13.5 Polarization: linear Antenna type: horn Connector: SMA (f) ## Mobile Satcom Antennas — ThinKom Solutions, Inc. [antennas] https://newspacemarket.com/products/thinkom-thinsat-300/ Frequency band: Ku Frequency: 13750-14500 MHz @ Tx Frequency: 10700-12750 MHz @ Rx Polarization: linear Antenna type: Phased Array Envelope (L×W×H): 59”L x 39”W x 4.3”H Supply voltage: 110 Supply voltage: 220 @ (variant 2) Power consumption: 600 W @ Max Power Operating temperature: -30-60 °C Survival temperature: -40-70 °C ## Portable Satcom Antennas (ThinPack family) — ThinKom Solutions, Inc. [antennas] https://newspacemarket.com/products/thinkom-thinpack/ Frequency band: Ku Frequency band: Ka @ (variant 2) Frequency band: X @ (variant 3) Operating temperature: -40-60 °C Survival temperature: -40-70 °C ## AHP5354A Active Multiband L1/L5 GNSS High Precision Patch Antenna — Taoglas [antennas] https://newspacemarket.com/products/taoglas-ahp5354a-gnss-l1-l5-patch-antenna/ Antenna type: Active Multiband GNSS Patch Frequency: 1166-1186 MHz @ GPS L5 Frequency: 1559-1563 MHz @ BeiDou_B1 Frequency: 1563-1587 MHz @ GPS_L1 Frequency: 1569-1610 MHz @ GLONASS_G1 Gain: 2.07 @ GPS L5, Peak Gain: 2.61 @ BeiDou_B1, Peak Gain: 2.61 @ GPS_L1, Peak Gain: 2.06 @ GLONASS_G1, Peak Polarization: RHCP Supply voltage: 1.8-5.5 Mass: 34.5 g Envelope (L×W×H): 70 x 70 x 9mm @ Total Dimension (Including Shielding Case) Connector: IPEX MHFI (U.FL) Operating temperature: -40-85 °C Survival temperature: -40-85 °C ## AHP54510 Active L1/L5/L-Band GNSS High Precision Antenna — Taoglas [antennas] https://newspacemarket.com/products/taoglas-ahp54510-levity-gnss-antenna/ Frequency band: L Frequency: 1166-1186 MHz Frequency: 1525-1559 MHz @ (variant 2) Frequency: 1559-1563 MHz @ (variant 3) Frequency: 1563-1587 MHz @ (variant 4) Frequency: 1593-1610 MHz @ (variant 5) Gain: 4.82 Gain: 4.94 @ (variant 2) Gain: 5.06 @ (variant 3) Gain: 5.08 @ (variant 4) Gain: 4.15 @ (variant 5) Polarization: RHCP Antenna type: Stacked Patch Mass: 70 g Envelope (L×W×H): 60x60x15mm Supply voltage: 1.8-5.5 Connector: IPEX MHFI (U.FL) Operating temperature: -40-85 °C Survival temperature: -40-85 °C ## CGSP457.A GNSS SatCom 1542-1643 MHz 45 x 45 x 7 mm Patch Antenna — Taoglas [antennas] https://newspacemarket.com/products/taoglas-cgsp457a-gnss-iridium-satcom-antenna/ Antenna type: Patch Antenna Envelope (L×W×H): 45 x 45 x 7mm Frequency: 1525-1559 MHz @ L-Band Gain: 5.93 @ L-Band Frequency: 1565-1586 MHz @ L1 Gain: 5.92 @ L1 Frequency: 1559-1565 MHz @ B1I Gain: 5.97 @ B1I Frequency: 1596-1610 MHz @ G1/L1OC Gain: 5.93 @ G1/L1OC Frequency: 1616-1626 MHz @ Iridium Gain: 5.93 @ Iridium Polarization: RHCP Envelope (L×W×H): 45 x 45 x 7mm @ (variant 2) Mass: 32 g Operating temperature: -40-85 °C Survival temperature: -40-85 °C ## MAT.500A 6-in-1 Integrated Antenna Board — Taoglas [antennas] https://newspacemarket.com/products/taoglas-mat500a-6in1-antenna-board-iridium/ Envelope (L×W×H): 157.32*103.19*30mm Antenna type: Embedded Antenna Board Frequency: 1575.42 MHz (nominal) @ GPS Frequency: 1602 MHz (nominal) @ GLONASS Gain: -1.2 @ Average Gain (GPS) Gain: -1.6 @ Average Gain (GLONASS) Gain: 5.47 @ Peak Gain (GPS) Gain: 4.9 @ Peak Gain (GLONASS) Polarization: RHCP Connector: IPEX standard, fully customizable Frequency: 1621 MHz (nominal) @ Satellite L-Band Gain: -1.52 @ Average Gain (Satellite L-Band) Gain: 5.11 @ Peak Gain (Satellite L-Band) Polarization: RHCP @ (variant 2) Connector: IPEX standard, fully customizable @ (variant 2) Gain: -3.58 @ Average Gain (MIMO_1 LTE700) Gain: -3.04 @ Average Gain (MIMO_1 GSM850) Gain: -5.7 @ Average Gain (MIMO_1 GSM900) Gain: -1.67 @ Average Gain (MIMO_1 DCS) Gain: -1.74 @ Average Gain (MIMO_1 PCS) Gain: -2.55 @ Average Gain (MIMO_1 UMTS1) Gain: -4.78 @ Average Gain (MIMO_1 LTE2600) Gain: -4 @ Average Gain (MIMO_2 LTE700) Gain: -4.6 @ Average Gain (MIMO_2 GSM850) Gain: -5.93 @ Average Gain (MIMO_2 GSM900) Gain: -1.83 @ Average Gain (MIMO_2 DCS) Gain: -2.21 @ Average Gain (MIMO_2 PCS) Gain: -2.51 @ Average Gain (MIMO_2 UMTS1) Gain: -5.34 @ Average Gain (MIMO_2 LTE2600) Gain: 0.28 @ Peak Gain (MIMO_1 LTE700) Gain: 1.7 @ Peak Gain (MIMO_1 GSM850) Gain: 1.7 @ Peak Gain (MIMO_1 GSM900) Gain: 6.79 @ Peak Gain (MIMO_1 DCS) Gain: 7.06 @ Peak Gain (MIMO_1 PCS) Gain: 6.81 @ Peak Gain (MIMO_1 UMTS1) Gain: 1.35 @ Peak Gain (MIMO_1 LTE2600) Gain: 0.55 @ Peak Gain (MIMO_2 LTE700) Gain: 1.07 @ Peak Gain (MIMO_2 GSM850) Gain: -1.42 @ Peak Gain (MIMO_2 GSM900) Gain: 5.23 @ Peak Gain (MIMO_2 DCS) Gain: 5.23 @ Peak Gain (MIMO_2 PCS) Gain: 4.64 @ Peak Gain (MIMO_2 UMTS1) Gain: 1.38 @ Peak Gain (MIMO_2 LTE2600) Polarization: Linear @ (variant 3) Connector: I-PEX standard , fully customizable @ (variant 3) Gain: -2.97 @ Average Gain (MIMO_1 2.4GHz Wi-Fi) Gain: -1.84 @ Average Gain (MIMO_2 2.4GHz Wi-Fi) Gain: -2.1 @ Average Gain (MIMO_1 5.8GHz Wi-Fi) Gain: -2.22 @ Average Gain (MIMO_2 5.8GHz Wi-Fi) Gain: 5.14 @ Peak Gain (MIMO_1 2.4GHz Wi-Fi) Gain: 5.82 @ Peak Gain (MIMO_2 2.4GHz Wi-Fi) Gain: 4.77 @ Peak Gain (MIMO_1 5.8GHz Wi-Fi) Gain: 4.96 @ Peak Gain (MIMO_2 5.8GHz Wi-Fi) Polarization: Linear @ (variant 4) Connector: I-PEX standard , fully customizable @ (variant 4) Mass: 66 g ## 98cm Ka/Ku RxTx Class I Antenna System — SpaceBridge Inc. [antennas] https://newspacemarket.com/products/98cm-ka-ku-rxtx-class-i-antenna-system/ Frequency band: Ka Frequency: 28000000-30000000 MHz @ Tx Frequency: 17800000-20200000 MHz @ Rx Polarization: Circular RH or LH Antenna type: One-piece offset feed prime focus Operating temperature: -50-60 °C ## Satlab SAS-2 dual S-band patch antenna — Satlab A/S [antennas] https://newspacemarket.com/products/satlab-sas-2/ Antenna type: patch Mass: 107 g Envelope (L×W×H): 80.00 x 75.00 x 6.80 mm Frequency band: S Frequency: 2025-2110 MHz @ Port 1 Polarization: RHCP @ Port 1 Gain: 5.5 @ Port 1 Beamwidth: 87 @ Port 1 Connector: SMA @ Port 1 Frequency: 2200-2290 MHz @ Port 2 Polarization: RHCP @ Port 2 Gain: 6.1 @ Port 2 Beamwidth: 85 @ Port 2 Connector: SMA @ Port 2 ## CubeSat Kit™ Cover Plate Assembly for AntS antenna — Pumpkin, Inc. [antennas] https://newspacemarket.com/products/pumpkin-cover-plate-assembly-ants-antenna/ Mass: 29 g @ Standard Cover Plate Mass: 40 g @ Dual Switch Cover Plate ## 2.4 Meter Ring Focus VSAT Antenna (FS240) — ALL-SEEING TECHNOLOGY CO., LTD [antennas] https://newspacemarket.com/products/ast-fs240-2-4m-vsat-antenna/ Frequency band: C Frequency band: Ku @ (variant 2) Frequency: 3400 MHz (min) @ Receive, C-Band Frequency: 4200 MHz (max) @ Receive, C-Band Frequency: 5850 MHz (min) @ Transmit, C-Band Frequency: 6725 MHz (max) @ Transmit, C-Band Frequency: 10950 MHz (min) @ Receive, Ku-Band Frequency: 12750 MHz (max) @ Receive, Ku-Band Frequency: 13750 MHz (min) @ Transmit, Ku-Band Frequency: 14500 MHz (max) @ Transmit, Ku-Band Gain: 38 @ Receive, C-Band Gain: 41.5 @ Transmit, C-Band Gain: 47.8 @ Receive, Ku-Band Gain: 49.1 @ Transmit, Ku-Band Polarization: Linear/ Circular @ C-Band Polarization: Linear @ Ku-Band Antenna type: Ring Focus Beamwidth: 2 @ Receive, C-Band Beamwidth: 1.38 @ Transmit, C-Band Beamwidth: 0.67 @ Receive, Ku-Band Beamwidth: 0.59 @ Transmit, Ku-Band Operating temperature: -40 °C (min) Operating temperature: 60 °C (max) ## 0.9 Meter Satcom On-The-Move Antenna (V900) — ALL-SEEING TECHNOLOGY CO., LTD [antennas] https://newspacemarket.com/products/ast-v900-satcom-on-the-move/ Frequency band: Ku Frequency: 10950000-12750000 MHz @ Receive Frequency: 13750000-14500000 MHz @ Transmit Gain: 38.5+ 20lg(f/12.5GHz) @ Receive Gain: 39.5+ 20lg(f/14.25GHz) @ Transmit Polarization: linear Antenna type: Prime focus antenna Mass: 98000 g @ Antenna only, excluding BUC Envelope (L×W×H): Φ135×75H(cm) Supply voltage: 48 @ DC Supply voltage: 110-220 @ AC 50/60Hz (Optional) Power consumption: 650 W @ ant. Power consumption: 10 W @ IDU Connector: N @ Electrical Interfaces Connector: WR75 @ Electrical Interfaces (variant 2) ## Patch Antennas — IQ Spacecom [antennas] https://newspacemarket.com/products/iq-spacecom-x-band-antenna/ Antenna type: patch Frequency: 8025000-8400000 MHz Frequency: 7145000-7250000 MHz @ (variant 2) Polarization: RHCP Gain: 10 Beamwidth: 40 Mass: 20 g Envelope (L×W×H): 60 x 40 x 1.8 mm³ Connector: SMA (f) Operating temperature: -30-60 °C Flight heritage: TRL 9 has been achieved with various successful LEO missions ## Fixed LEO/MEO Antenna Systems — Kratos Defense & Security Solutions [antennas] https://newspacemarket.com/products/kratos-fixed-leo-meo-antenna-systems/ Frequency band: Ka Polarization: linear Polarization: circular @ (variant 2) Antenna type: reflector Operating temperature: -40 °C (min) Operating temperature: 52 °C (max) Survival temperature: -54 °C (min) Survival temperature: 71 °C (max) Supply voltage: 110 (min) Supply voltage: 220 (max) Frequency: 19400 MHz (min) Frequency: 19600 MHz (max) Frequency: 925 MHz (min) @ (variant 2) Frequency: 2400 MHz (max) @ (variant 2) Frequency band: Ka @ (variant 2) Polarization: CP @ (variant 3) Frequency: 17700 MHz (min) @ (variant 3) Frequency: 21200 MHz (max) @ (variant 3) Frequency: 17800 MHz (min) @ (variant 4) Frequency: 20200 MHz (max) @ (variant 4) Frequency: 21400 MHz (min) @ (variant 5) Frequency: 22000 MHz (max) @ (variant 5) Frequency: 27000 MHz (min) @ (variant 6) Frequency: 30050 MHz (max) @ (variant 6) Frequency: 27500 MHz (min) @ (variant 7) Frequency: 31000 MHz (max) @ (variant 7) Frequency: 28300 MHz (min) @ (variant 8) Frequency: 30000 MHz (max) @ (variant 8) ## Transportable Antenna Systems — Kratos Defense & Security Solutions [antennas] https://newspacemarket.com/products/kratos-transportable-antenna-systems/ Frequency: 225 - 400 MHz @ UHF-band Polarization: circular @ UHF-band Frequency band: UHF Frequency: 3.625 - 4.2 GHz @ C-band Polarization: circular @ C-band Frequency band: C @ (variant 2) Frequency: 3.4 - 4.2 GHz @ C-band (variant 2) Polarization: circular @ C-band (variant 2) Frequency band: C @ (variant 3) Frequency: 3.625 - 4.2 GHz @ C-band (variant 3) Polarization: linear @ C-band (variant 3) Frequency band: C @ (variant 4) Frequency: 3.4 - 4.2 GHz @ C-band (variant 4) Polarization: dual @ C-band (variant 4) Frequency band: C @ (variant 5) Frequency: 4.5 - 4.8 GHz @ C-band (variant 5) Polarization: linear @ C-band (variant 5) Frequency band: C @ (variant 6) Frequency: 5.850 - 6.425 GHz @ C-band (variant 6) Polarization: circular @ C-band (variant 6) Frequency band: C @ (variant 7) Frequency: 5.725 - 6.650 GHz @ C-band (variant 7) Polarization: dual @ C-band (variant 7) Frequency band: C @ (variant 8) Frequency: 5.725 - 6.725 GHz @ C-band (variant 8) Polarization: linear @ C-band (variant 8) Frequency band: C @ (variant 9) Frequency: 6.725 - 7.025 GHz @ C-band (variant 9) Polarization: linear @ C-band (variant 9) Frequency band: C @ (variant 10) Frequency: 7.25 - 7.75 GHz @ X-band Polarization: circular @ X-band Frequency band: X @ (variant 11) Frequency: 7.25 - 7.75 GHz @ X-band (variant 2) Polarization: dual @ X-band (variant 2) Frequency band: X @ (variant 12) Frequency: 7.9 - 8.4 GHz @ X-band (variant 3) Polarization: circular @ X-band (variant 3) Frequency band: X @ (variant 13) Frequency: 7.9 - 8.4 GHz @ X-band (variant 4) Polarization: dual @ X-band (variant 4) Frequency band: X @ (variant 14) Frequency: 10.7 - 12.75 GHz @ Ku-band Polarization: linear @ Ku-band Frequency band: Ku @ (variant 15) Frequency: 10.7 - 13.25 GHz @ Ku-band (variant 2) Polarization: linear @ Ku-band (variant 2) Frequency band: Ku @ (variant 16) Frequency: 13.00 - 13.25 GHz @ Ku-band (variant 3) Polarization: linear @ Ku-band (variant 3) Frequency band: Ku @ (variant 17) Frequency: 13.75 - 14.5 GHz @ Ku-band (variant 4) Polarization: linear @ Ku-band (variant 4) Frequency band: Ku @ (variant 18) Frequency: 13.75 - 14.8 GHz @ Ku-band (variant 5) Polarization: linear @ Ku-band (variant 5) Frequency band: Ku @ (variant 19) Frequency: 10.7 - 12.75 GHz @ K-band Polarization: linear @ K-band Frequency band: K @ (variant 20) Frequency: 17.3 - 18.4 GHz @ K-band (variant 2) Polarization: linear @ K-band (variant 2) Frequency band: K @ (variant 21) Frequency: 17.7 - 21.2 GHz @ Ka-band Polarization: dual @ Ka-band Frequency band: Ka @ (variant 22) Frequency: 20.2 - 21.2 GHz @ Ka-band (variant 2) Polarization: circular @ Ka-band (variant 2) Frequency band: Ka @ (variant 23) Frequency: 18.3 - 20.2 GHz @ Ka-band (variant 3) Polarization: linear @ Ka-band (variant 3) Frequency band: Ka @ (variant 24) Frequency: 27.0 - 30.05 GHz @ Ka-band (variant 4) Polarization: linear @ Ka-band (variant 4) Frequency band: Ka @ (variant 25) Frequency: 27.50 - 31.00 GHz @ Ka-band (variant 5) Polarization: circular @ Ka-band (variant 5) Frequency band: Ka @ (variant 26) Frequency: 30.0 - 31.0 GHz @ Ka-band (variant 6) Polarization: circular @ Ka-band (variant 6) Frequency band: Ka @ (variant 27) Frequency: 10.7 - 12.75 GHz @ Ku-band (variant 6) Polarization: linear @ Ku-band (variant 6) Frequency band: Ku @ (variant 28) Frequency: 13.75 - 14.5 GHz @ Ku-band (variant 7) Polarization: linear @ Ku-band (variant 7) Frequency band: Ku @ (variant 29) Frequency: 17.3 - 18.4 GHz @ K-band (variant 3) Polarization: linear @ K-band (variant 3) Frequency band: K @ (variant 30) Operating temperature: -40o to 52oC ## Tactical Antenna Systems — Kratos Defense & Security Solutions [antennas] https://newspacemarket.com/products/kratos-tactical-antenna-systems/ Antenna type: Nomadic Antenna System Mass: 220000 g (max) @ fully motorized versions (including feeds), tactical version Operating temperature: -40 °C (min) Operating temperature: 60 °C (max) Survival temperature: -58 °C (min) Survival temperature: 71 °C (max) Supply voltage: 110 (nominal) @ Indoor Supply voltage: 220 (nominal) @ Indoor (variant 2) Supply voltage: 24 (nominal) @ Outdoor Supply voltage: 120 (nominal) @ Outdoor (variant 2) Data interface: Ethernet Frequency band: L Frequency: 3625000 MHz (min) @ L-band RX Frequency: 4200000 MHz (max) @ L-band RX Frequency: 5850000 MHz (min) @ L-band TX Frequency: 6425000 MHz (max) @ L-band TX Polarization: dual @ L-band CP Polarization: linear @ L-band LP Frequency band: C @ (variant 2) Frequency: 3625000 MHz (min) @ C-band RX Frequency: 4200000 MHz (max) @ C-band RX Frequency: 5850000 MHz (min) @ C-band TX Frequency: 6425000 MHz (max) @ C-band TX Polarization: circular @ C-band CP Polarization: linear @ C-band LP Frequency band: X @ (variant 3) Frequency: 7250000 MHz (min) @ X-band RX Frequency: 7750000 MHz (max) @ X-band RX Frequency: 7900000 MHz (min) @ X-band TX Frequency: 8400000 MHz (max) @ X-band TX Polarization: circular @ X-band CP Polarization: linear @ X-band LP Frequency band: Ku @ (variant 4) Frequency: 10700000 MHz (min) @ Ku-band RX Frequency: 12750000 MHz (max) @ Ku-band RX Frequency: 13750000 MHz (min) @ Ku-band TX Frequency: 14800000 MHz (max) @ Ku-band TX Polarization: linear @ Ku-band LP Polarization: circular @ Ku-band CP Frequency band: Ka @ (variant 5) Frequency: 17700000 MHz (min) @ Ka-band RX Frequency: 21200000 MHz (max) @ Ka-band RX Frequency: 27500000 MHz (min) @ Ka-band TX Frequency: 31000000 MHz (max) @ Ka-band TX Polarization: linear @ Ka-band LP Polarization: circular @ Ka-band CP ## Electronically Steerable Antenna (ESA) OrBeam 5534 — Orbit Communication Systems [antennas] https://newspacemarket.com/products/orbeam-5534-electronically-steerable-antenna/ Frequency band: Ka Frequency: 27500000-31000000 MHz @ Transmit Frequency: 17700000-21200000 MHz @ Receive Polarization: circular @ Electronically selectable (RHCP/LHCP/H/V) Polarization: dual @ Electronically selectable (RHCP/LHCP/H/V) (variant 2) Antenna type: Electronically Steerable Antenna (ESA) ## X-Band Patch Array Antenna — Plan-S (Connecta) [antennas] https://newspacemarket.com/products/x-band-patch-array-antenna-4217/ Frequency band: X Frequency: 8025-8400 MHz Gain: 20.5-20.9 Beamwidth: 18.6 Beamwidth: 9.3 @ (variant 2) Polarization: RHCP Antenna type: patch Envelope (L×W×H): 220 x 110 x 2.17mm, Excluding Connector Connector: Single SMA Connector Flight heritage: Flight heritage demonstrated on 1 satellite ## S-Band Patch Antenna — Plan-S (Connecta) [antennas] https://newspacemarket.com/products/s-band-patch-antenna-4217/ Antenna type: patch Frequency band: S Frequency: 2025-2110 MHz @ Rx Model Frequency: 2200-2290 MHz @ Tx Model Gain: 6 (min) Beamwidth: 96 Beamwidth: 95 @ (variant 2) Polarization: RHCP Polarization: LHCP @ (variant 2) Envelope (L×W×H): 55x55x4.7mm @ RX Envelope (L×W×H): 50x50x4.7mm @ TX Connector: SMA Female Connector: SMP @ (variant 2) Operating temperature: -40-85 °C Flight heritage: Flight Proven Flight heritage: Flight heritage demonstrated on 19 Satellites @ (variant 2) ## S-Band Dual-Band Patch Antenna — Plan-S (Connecta) [antennas] https://newspacemarket.com/products/s-band-dual-band-patch-antenna-4217/ Frequency band: S Frequency: 2025 MHz (min) Frequency: 2110 MHz (max) Frequency: 2200 MHz (min) @ (variant 2) Frequency: 2290 MHz (max) @ (variant 2) Gain: 6.1 Polarization: RHCP Antenna type: Stacked Patch Envelope (L×W×H): 86 x 98 x 3.25 mm, Excluding Connectors Connector: 2 x MMCX Male Operating temperature: -40 °C (min) Operating temperature: 85 °C (max) Flight heritage: Flight heritage demonstrated on 2 satellites ## UHF Deployable Dipole Antenna — Plan-S (Connecta) [antennas] https://newspacemarket.com/products/uhf-deployable-dipole-antenna-4217/ Antenna type: deployable Frequency band: UHF Frequency: 400 MHz (min) Frequency: 403 MHz (max) Gain: 2 @ peak Envelope (L×W×H): 143x86x11 mm (Stowed Length) Envelope (L×W×H): 143x363x11 mm (Deployed Length) @ (variant 2) Polarization: linear Flight heritage: Proven in Orbit Flight heritage demonstrated on 3 Satellites Operating temperature: -40 °C (min) Operating temperature: 85 °C (max) ## BEAMSAT K/Ka-Band Horn Antenna — PicoSaTs [antennas] https://newspacemarket.com/products/picosats-beamsat-k-ka-band-horn-antenna/ Antenna type: horn Frequency band: Ku Frequency: 17300 MHz (min) Frequency: 21200 MHz (max) Gain: 21.5 Beamwidth: 17 Polarization: LHCP Polarization: RHCP @ optional Connector: 2.92 Frequency band: Ka @ (variant 2) Frequency: 27500 MHz (min) @ (variant 2) Frequency: 31000 MHz (max) @ (variant 2) Gain: 24.5 @ (variant 2) Beamwidth: 7.7 @ (variant 2) Polarization: RHCP @ (variant 2) Polarization: LHCP @ optional (variant 2) Connector: 2.92 @ (variant 2) Mass: 569 g Envelope (L×W×H): 88.0 mm x 88.0 mm x 218.0 mm ## BEAMSAT Ku-Band Horn Antenna — PicoSaTs [antennas] https://newspacemarket.com/products/picosats-beamsat-ku-band-horn-antenna/ Frequency band: Ku Frequency: 10700 MHz (min) @ KU - BAND 1 Frequency: 12750 MHz (max) @ KU - BAND 1 Frequency: 13000 MHz (min) @ KU - BAND 2 Frequency: 14800 MHz (max) @ KU - BAND 2 Gain: 16.2 @ KU - BAND 1 Gain: 16.2 @ KU - BAND 2 Beamwidth: 22 @ KU - BAND 1 Beamwidth: 22 @ KU - BAND 2 Polarization: linear @ KU - BAND 1 Polarization: linear @ KU - BAND 2 Antenna type: horn Mass: 633 g Envelope (L×W×H): 109.1 mm x 109.1 mm x 205.3 mm Connector: SMA @ KU - BAND 1 Connector: SMA @ KU - BAND 2 ## BEAMSAT X-Band Patch Antenna — PicoSaTs [antennas] https://newspacemarket.com/products/picosats-beamsat-x-band-patch-antenna/ Frequency band: X Frequency: 8025000-8400000 MHz Gain: 17.1 Beamwidth: 22.6 Polarization: RHCP Antenna type: patch Mass: 100 g @ with enclosure Envelope (L×W×H): 98.0 mm x 98.0 mm x 10.8 mm (with enclosure) Connector: SMP ## CHORUS-01 Deployable Cubesat antenna — 2NDSpace Srl [antennas] https://newspacemarket.com/products/chorus-01-deployable-cubesat-antenna/ Antenna type: Dual Dipole Polarization: 2x Linear Frequency: 140-928 MHz Gain: 0 Supply voltage: 3.3-5 Data interface: I2C Frequency band: UHF Frequency band: VHF @ (variant 2) ## CHORUS-06 Deployable Cubesat antenna — 2NDSpace Srl [antennas] https://newspacemarket.com/products/chorus-06-deployable-cubesat-antenna/ Antenna type: Dual Dipole @ CHORUS-06 LP Antenna type: Turn-style @ CHORUS-06 CP Polarization: linear @ CHORUS-06 LP Polarization: circular @ CHORUS-06 CP Frequency: 140 MHz (min) Frequency: 928 MHz (max) Gain: 0 Supply voltage: 3.3 (min) @ Control System Voltage Supply voltage: 5 (max) @ Control System Voltage Data interface: I2C ## QUASAR-WSANT — AAC Clyde Space [antennas] https://newspacemarket.com/products/aac-quasar-wsant/ Operating temperature: -40-100 °C Survival temperature: -40-85 °C Mass: 68.5 g Design lifetime: 5-6 years Frequency: 2025-2290 MHz Power consumption: 5 W (max) @ RF power Beamwidth: 60 Polarization: RHCP @ port R Polarization: LHCP @ port L Gain: 5 (min) Envelope (L×W×H): 83 mm (length) x 83 mm (width) x 5 mm (height including connectors) Frequency band: S Antenna type: patch antenna Connector: SMP-Female ## SBFM120 1.2m Manual Pointing Flyaway — SpaceBridge Inc. [antennas] https://newspacemarket.com/products/sbfm120-manual-pointing-flyaway/ Frequency band: X Frequency band: Ku @ (variant 2) Frequency band: Kx @ (variant 3) Frequency band: Ka @ (variant 4) Frequency: 7900 MHz (min) @ Tx X-band Frequency: 8400 MHz (max) @ Tx X-band Frequency: 12750 MHz (min) @ Tx App30B-15 Ku-band Frequency: 13250 MHz (max) @ Tx App30B-15 Ku-band Frequency: 13750 MHz (min) @ Tx Kx-band Frequency: 14500 MHz (max) @ Tx Kx-band Frequency: 27500 MHz (min) @ Tx Ka-band Frequency: 31000 MHz (max) @ Tx Ka-band Frequency: 7250 MHz (min) @ Rx X-band Frequency: 7750 MHz (max) @ Rx X-band Frequency: 10700 MHz (min) @ Rx App30B-15 Ku-band Frequency: 11700 MHz (max) @ Rx App30B-15 Ku-band Frequency: 10700 MHz (min) @ Rx Kx-band Frequency: 12750 MHz (max) @ Rx Kx-band Frequency: 18300 MHz (min) @ Rx Ka-band Frequency: 20200 MHz (max) @ Rx Ka-band Polarization: Circular @ X-band Polarization: Linear @ App30B-15 Ku-band Polarization: Linear @ Kx-band Polarization: Circular @ Ka-band Gain: 38.2 (min) @ Tx mid-band X-band Gain: 41.4 (min) @ Tx mid-band App30B-15 Ku-band Gain: 42.1 (min) @ Tx mid-band Kx-band Gain: 49 (min) @ Tx mid-band Ka-band Gain: 37.5 (min) @ Rx mid-band X-band Gain: 40.4 (min) @ Rx mid-band App30B-15 Ku-band Gain: 41 (min) @ Rx mid-band Kx-band Gain: 45.8 (min) @ Rx mid-band Ka-band Antenna type: Ring focus Mass: 16000 g @ Antenna Net Weight (exclude BUC, LNB, packing, accessories) Envelope (L×W×H): 710x410x250 mm @ Backpack 1 packing size Mass: 7400 g @ Backpack 1 Net weight Envelope (L×W×H): 630x510x310 mm @ Backpack 2 packing size Mass: 8600 g @ Backpack 2 Net weight Operating temperature: -40 °C (min) Operating temperature: 60 °C (max) Survival temperature: -50 °C (min) Survival temperature: 70 °C (max) ## piPATCH-AllBand-TC — SkyFox Labs s.r.o. [antennas] https://newspacemarket.com/products/skyfox-labs-pipatch-allband-tc/ Antenna type: patch Mass: 139 g Envelope (L×W×H): 98×98×+13.5/-8 mm Supply voltage: 2.7-5.5 Connector: MCX-F Operating temperature: -40-85 °C Survival temperature: -55-100 °C ## piPATCH-IoT — SkyFox Labs s.r.o. [antennas] https://newspacemarket.com/products/skyfox-labs-pipatch-iot/ Antenna type: Patch antenna Mass: 139 g Envelope (L×W×H): 98×98×+13.5/-8 mm Connector: MCX-F Power consumption: 30 W @ typical, @ 25°C ## NanoCom AM2150-O MK2 — GomSpace [antennas] https://newspacemarket.com/products/gomspace-nanocom-am2150-o/ Antenna type: 1/4-wave sleeved dipole Frequency: 2025-2290 MHz Polarization: linear Gain: -12 (min) Power consumption: 5 W @ max input Operating temperature: -40-85 °C Survival temperature: -40-85 °C Data interface: I2C Connector: Molex 53398-0871 8pin 1.25mm pitch PicoBlade Header Connector: Samtec MCX-J-P-H-ST-TH1 50ohm MCX jack, female socket @ (variant 2) Supply voltage: 3-3.6 @ GSRB Supply Supply voltage: 4.5-5.5 @ VBURN supply 5V option Supply voltage: 24-33.6 @ VBURN supply 32V option Mass: 23.5 g (nominal) ## NanoCom ANT-6F — GomSpace [antennas] https://newspacemarket.com/products/gomspace-nanocom-ant-6f/ Frequency band: UHF Frequency: 340 MHz (min) Frequency: 680 MHz (max) Antenna type: deployable, omnidirectional, canted turnstile antenna system with rigid antenna elements Gain: -7 (min) @ absolute gain, 95% probability Polarization: circular Polarization: RHCP @ Mode 1 (RF module connects to input 1) Polarization: LHCP @ Mode 2 (RF module connects to input 2) Polarization: RHCP @ Mode 3 (RF modules connects to input 1) Polarization: LHCP @ Mode 3 (RF modules connects to input 2) Data interface: I2C Operating temperature: -40 °C (min) Operating temperature: 85 °C (max) Survival temperature: -40 °C (min) Survival temperature: 90 °C (max) Supply voltage: 3.2 (min) @ Supply voltage Supply voltage: 3.4 (max) @ Supply voltage Supply voltage: 4.5 (min) @ Burn resistor voltage Supply voltage: 7 (max) @ Burn resistor voltage Connector: Molex Pico-Lock 504050-0891 (P2, P3) Connector: 50 Ω MCX for edge mounting. Type Samtec MCX-J-P-H-ST-EM1 (J5) @ (variant 2) Connector: 50 Ω SMPM for PCB edge mounting (J3/J4) @ (variant 3) Connector: U.FL-LP-040 connector @ (variant 4) Mass: 90 g @ including antenna rods Envelope (L×W×H): 221.7 x 116.7 x 5.3 mm @ not including antenna rods ## NanoCom ANT2150 DUP and ANT2150 ISL — GomSpace [antennas] https://newspacemarket.com/products/gomspace-nanocom-ant2150-dup-isl/ Antenna type: active antenna Gain: 8 Polarization: circular Polarization: RHCP @ ANT2150-DUP default Polarization: LHCP @ ANT2150-ISL default Frequency: 2200-2290 MHz @ TX band, ANT2150-ISL Frequency: 2200-2290 MHz @ RX band, ANT2150-ISL Frequency: 2200-2290 MHz @ TX band, ANT2150-DUP Frequency: 2025-2120 MHz @ RX band, ANT2150-DUP Frequency band: S Connector: Molex SSMCX 73413-0040 @ RX RF COAXIAL CONNECTOR Connector: Molex SSMCX 73413-0040 @ TX RF COAXIAL CONNECTOR Connector: Molex Pico-Lock 1.50 mm pitch 504050-0791 @ Power Connector Connector: Molex Pico-Lock 1.50 mm pitch 504050-1091 @ Control Connector Connector: Molex Pico-Lock 1.50 mm pitch 504050-0691 @ Debug Connector Supply voltage: 8-18 Data interface: CAN Data interface: I2C @ (variant 2) Data interface: UART @ (variant 3) Supply voltage: 8-18 @ (variant 2) Power consumption: 0.0018 W (max) @ OFF Power consumption: 0.2 W (max) @ IDLE Power consumption: 0.8 W (max) @ RX mode Power consumption: 0.6 W (max) @ TX STANDBY Power consumption: 11.75 W (max) @ TX ACTIVE Mass: 110 g Envelope (L×W×H): 98 x 98 x 20.1 mm Operating temperature: -40-85 °C Survival temperature: -40-85 °C Beamwidth: 64-78 ## NanoCom ANT1090-P — GomSpace [antennas] https://newspacemarket.com/products/gomspace-nanocom-ant1090-p/ Antenna type: patch Frequency: 1090 MHz Gain: 4.5 Polarization: RHCP Mass: 135 g Envelope (L×W×H): 100.0 x 100.0 x 12.0 mm Polarization: RHCP @ with Type B & C backplates Gain: 4.5 (min) @ Realized Gain, centre frequency with Type B & C backplates Beamwidth: 80 (min) @ 3 dB beam width with Type B & C backplates Polarization: RHCP @ with Type A & D backplates Gain: 4.5 (min) @ Realized Gain, centre frequency with Type A & D backplates Beamwidth: 60 (min) @ 3 dB beam width with Type A & D backplates Connector: SSMCX connector ## piPATCH-IoT-TC — SkyFox Labs s.r.o. [antennas] https://newspacemarket.com/products/skyfox-labs-pipatch-iot-tc/ Antenna type: Active GNSS Patch antenna Mass: 139 g Envelope (L×W×H): 98x98x+13.5/-8 mm Operating temperature: -40 °C (min) Operating temperature: 85 °C (max) Connector: MCX-F Supply voltage: 2.7 (min) Supply voltage: 5.5 (max) Operating temperature: -40 °C (min) @ (variant 2) Operating temperature: 85 °C (max) @ (variant 2) Survival temperature: -55 °C (min) Survival temperature: 100 °C (max) Export status: regulated (Dual Use) goods, the export is controlled and needs special Export License approved by the Ministry of Industry and Trade of the Czech Republic ## OceanTRx 4 and OceanTRx 7 Maritime SATCOM Terminals — Orbit Communication Systems [antennas] https://newspacemarket.com/products/oceantrx-7-maritime-satcom/ Antenna type: Dual Offset Gregorian Envelope (L×W×H): D: 1.55 m (61”), H: 1.69 m (67”) Mass: 215000 g Frequency band: Ku Polarization: linear @ HOR/VER Frequency band: Ka @ Wideband Polarization: circular @ RHCP/LHCP Power consumption: 500 W @ ADE system <, W/O BUCs Power consumption: 100 W @ BDE equipment< ## Global Aero Terminal-5530 (GAT-5530) — Viasat, Inc. [antennas] https://newspacemarket.com/products/global-aero-terminal-5530-gat-5530-3363/ Antenna type: Fuselage mount, 2nd generation medium profile dual Ku-/Ka-band Tx/Rx airborne antenna Frequency band: Ka Polarization: circular @ Ka-band Frequency: 27500-31000 MHz @ Ka-band Tx Frequency: 17700-21200 MHz @ Ka-band Rx Frequency band: Ku @ (variant 2) Polarization: linear @ Ku-band Frequency: 14000-14500 MHz @ Ku-band Tx Frequency: 10950-12750 MHz @ Ku-band Rx Mass: 73900 g Operating temperature: -61-70 °C Supply voltage: 115 @ antenna power supply Supply voltage: 28 @ antenna power supply (variant 2) Power consumption: 465 W @ max, antenna power supply Envelope (L×W×H): Ø39.25 x 11.3 in.; Ø99.7 x 28.7 cm @ Swept Volume ## CubeSat Kit™ Chassis Walls — Pumpkin, Inc. [structures] https://newspacemarket.com/products/pumpkin-chassis-walls/ Mass: 132 g @ 1U Solid Structure Mass: 71 g @ 1U Skeleton Structure Mass: 208 g @ 1.5U Solid Structure Mass: 107 g @ 1.5U Skeleton Structure Mass: 286 g @ 2U Solid Structure Mass: 142 g @ 2U Skeleton Structure Mass: 439 g @ 3U Solid Structure Mass: 213 g @ 3U Skeleton Structure ## VERSE CubeSat Structures — 2NDSpace Srl [structures] https://newspacemarket.com/products/2ndspace-verse-structures/ Form factor: 1 Envelope (L×W×H): 100x100x113,5 Mass: 98 g Form factor: 2 @ (variant 2) Envelope (L×W×H): 100x100x227 @ (variant 2) Mass: 204 g @ (variant 2) Form factor: 3 @ (variant 3) Envelope (L×W×H): 100x100x340,5 @ (variant 3) Mass: 310 g @ (variant 3) Form factor: 6 @ (variant 4) Envelope (L×W×H): 100x226,3x366 100x226,3x340,5 @ (variant 4) Mass: 890 g @ Primary mass, screws, switches and 4x stack frames Form factor: 8 @ (variant 5) Envelope (L×W×H): 100x226,3x454 @ (variant 5) Mass: 1120 g @ Primary mass, screws, switches and 4x stack frames (variant 2) Form factor: 12 @ (variant 6) Envelope (L×W×H): 226x226,3x366 226x226,3x340,5 @ (variant 6) Mass: 1915 g @ Primary mass, screws, switches and 2x stack layers Form factor: 16 @ (variant 7) Envelope (L×W×H): 226,3x226,3x454 @ (variant 7) Mass: 2305 g @ Primary mass, screws, switches and 2x stack layers (variant 2) ## VERSE-08 8U Cubesat Structure — 2NDSpace Srl [structures] https://newspacemarket.com/products/verse-08-8u-cubesat-structure/ Form factor: 8 Envelope (L×W×H): 100x226,3x454 Mass: 1120 g ## VERSE-12 12U Cubesat Structure — 2NDSpace Srl [structures] https://newspacemarket.com/products/verse-12-12u-cubesat-structure/ Form factor: 12 Envelope (L×W×H): 226x226,3x366 Envelope (L×W×H): 226x226,3x340,5 @ (variant 2) Mass: 1915 g ## VERSE-16 16U Cubesat Structure — 2NDSpace Srl [structures] https://newspacemarket.com/products/verse-16-16u-cubesat-structure/ Form factor: 16 Envelope (L×W×H): 226,3x226,3x454 Mass: 2305 g ## VERSE-06 6U Cubesat Structure — 2NDSpace Srl [structures] https://newspacemarket.com/products/verse-06-6u-cubesat-structure/ Form factor: 6 Envelope (L×W×H): 100x226,3x366 Envelope (L×W×H): 100x226,3x340,5 @ (variant 2) Mass: 890 g ## VERSE-03 3U Cubesat Structure — 2NDSpace Srl [structures] https://newspacemarket.com/products/verse-03-3u-cubesat-structure/ Form factor: 3 Envelope (L×W×H): 100x100x340,5 Mass: 310 g ## VERSE-02 2U Cubesat Structure — 2NDSpace Srl [structures] https://newspacemarket.com/products/verse-02-2u-cubesat-structure/ Form factor: 2 Envelope (L×W×H): 100x100x227 Mass: 204 g ## Nanostruct 6U — GomSpace [structures] https://newspacemarket.com/products/nanostruct-6u/ Form factor: 6 Material: Alu 7075-T7351 Mass: 665 g @ default structure Envelope (L×W×H): 340.5 x 226.3 x 100.0 mm @ without kill switches Envelope (L×W×H): 340.5 x 226.3 x 100.0 mm Mass: 665 g @ Total mass for default delivered structure, 2x frames and 4x corners, including screw and pin ki Material: EN AW7075-T7351 @ (variant 2) ## FreeForm Microsatellite Platform — U-Space [structures] https://newspacemarket.com/products/uspace-freeform-microsatellite-platform/ Mass: 80000 g Design lifetime: 5 years Envelope (L×W×H): 480x600x800 mm Data interface: UART Data interface: SpaceWire @ (variant 2) Data interface: CAN @ (variant 3) ## 16U CubeSat Platform — U-Space [structures] https://newspacemarket.com/products/uspace-16u-cubesat-platform/ Design lifetime: 5 years Form factor: 16 Mass: 26000 g (max) Envelope (L×W×H): 8U Cube + 2U Data interface: UART Data interface: SpaceWire @ (variant 2) Data interface: CAN @ (variant 3) Power consumption: 150 W @ max Power consumption: 55 W @ Payload Average (LTAN 6h-18h) Power consumption: 25 W @ Payload Average (LTAN 12h-24h) ## Renegade — Terran Orbital [structures] https://newspacemarket.com/products/tyvak-renegade/ Form factor: 12 @ standard point of departure Form factor: 16 @ easily customized Form factor: 12 @ Configuration Form factor: 16 @ option Mass: 25000 g (max) @ Launch Mass (Wet) Supply voltage: 12 @ Unreg Supply voltage: 3.3 @ rail available Supply voltage: 5 @ rail available (variant 2) ## Nebula — Terran Orbital [structures] https://newspacemarket.com/products/tyvak-nebula/ Mass: 250000 g @ Wet Envelope (L×W×H): 82cm x 58cm x 39cm @ without Solar Panels Supply voltage: 66 (nominal) @ system power Flight heritage: Space Development Agency’s Tranche 0 Transport Layer ## 6U CubeSat — Blue Canyon Technologies [structures] https://newspacemarket.com/products/bct-xb6-cubesat-bus/ Form factor: 6 Data interface: UART Data interface: LVDS @ (variant 2) Data interface: RS-422 @ (variant 3) Data interface: RS-485 @ (variant 4) Data interface: SpaceWire @ (variant 5) Design lifetime: 5 years @ LEO Design lifetime: 2 years @ GEO/Lunar/Deep Space ## 1U – 3U Platform — Spacemanic s.r.o. [structures] https://newspacemarket.com/products/spacemanic-corvus-platform-1u-3u/ Form factor: 2 Form factor: 3 @ (variant 2) Data interface: RS-485 Data interface: CAN @ (variant 2) Data interface: I2C @ (variant 3) Data interface: RS-422 @ (variant 4) Data interface: UART @ (variant 5) Data interface: I2C @ (variant 6) Data interface: SPI @ (variant 7) Data interface: other @ ADC Data interface: other @ PWM Data interface: other @ GPIO Design lifetime: 5 years Mass: 1000 g Power consumption: 23 W Mass: 2500 g @ (variant 2) Power consumption: 48 W @ (variant 2) Mass: 4000 g @ (variant 3) Power consumption: 48 W @ (variant 3) ## 12U – 16U Platform — Spacemanic s.r.o. [structures] https://newspacemarket.com/products/spacemanic-corvus-platform-6u-16u/ Design lifetime: 5 years @ up to Form factor: 12 Form factor: 16 @ (variant 2) Mass: 16000 g @ AOCS Mass: 22000 g @ AOCS (variant 2) Power consumption: 48 W (max) @ @ 12 V Supply voltage: 13.6 (min) @ unreg. VBat. Supply voltage: 16.8 (max) @ unreg. VBat. Design lifetime: 5 years ## 6U Platform Kit — GomSpace [structures] https://newspacemarket.com/products/gomspace-nanosat-6u-kit/ Envelope (L×W×H): 6U Form factor: 6 Mass: 450 g @ Star Tracker Mass: 500 g @ additional NanoPower BP8 battery pack Data interface: SpaceWire @ Payload Harness Kit Data interface: CAN @ Control Bus ## ESPAStar — Northrop Grumman Space Systems [structures] https://newspacemarket.com/products/ngc-espastar-bus-family/ Flight heritage: flight-proven @ ESPAStar Flight heritage: Launched April 2018 @ EAGLE (ESPA AUGMENTED GEOSTATIONARY LABORATORY EXPERIMENT) Flight heritage: Launch December 2021 @ LDPE-1 (LONG DURATION PROPULSIVE ESPA) Flight heritage: Launched June 2022 @ ESPAStar-1 Mass: 430000-470000 g Envelope (L×W×H): 157.5 cm dia x 61 cm ht Mass: 1920000 g (min) Mass: 900000 g (max) Mass: 600000 g ## NanoStruct 8U — GomSpace [structures] https://newspacemarket.com/products/nanostruct-8u/ Form factor: 8 Material: Alu 7075-T7351 Mass: 956 g Envelope (L×W×H): 454 x 226.3 x 100.0 mm Material: EN AW7075-T7351 @ (variant 2) Envelope (L×W×H): 454 x 226.3 x 100.0 mm @ With deployment switches stowed Mass: 956 g @ Total mass for 8U Structure including the optional secondary structure, 2x Wall Structure, 2x Se Mass: 148 g @ Total mass of Secondary Structure Material: clear hard anodized, MIL-A-8625F Type III Class 1 @ (variant 3) Material: SurTec 650 chromitAL TCP MIL-DTL-5541F Type II Class 3 @ (variant 4) ## Nanostruct 12U — GomSpace [structures] https://newspacemarket.com/products/nanostruct-12u/ Form factor: 12 Mass: 1496 g @ default structure Mass: 1500 g @ under Envelope (L×W×H): 340.5 x 226.3 x 226.3 mm @ without kill switches Material: Alu 7075-T7351 material Material: Rails – hard anodised Structure – Surtec 650 TCP @ (variant 2) ## Antartix – Computadora OBC — VENG S.A. [obc-computers] https://newspacemarket.com/products/veng-antartix-obc/ Processor: AMD Xilinx Artix-7 FPGA RAM: 4096 MB Storage: 0.125 GB Storage: 0.5 GB @ (variant 2) Envelope (L×W×H): 95.89 mm x 90.17 mm x 15.24 mm ## On-board computer — SPUTNIX [obc-computers] https://newspacemarket.com/products/on-board-computer/ Power consumption: 10 W (max) Supply voltage: 22 (min) Supply voltage: 34 (max) Envelope (L×W×H): 171 x 111 x 51 mm (without fasteners) Mass: 860 g Processor: 32-bit microprocessor based on the SPARC v8 architecture of the Leon4FT core CPU clock: 80 MHz Data interface: CAN Data interface: SpaceWire @ (variant 2) Storage: 0.001 GB @ EEPROM Storage: 0.0156 GB @ MRAM RAM: 16 MB Operating system: RTEMS OS Flight heritage: Tablettsat KP and cubsat projects, Tablettsat-Aurora, Zorkiy ## ST Engineering Spacecraft On-Board Computer (OBC) — ST Engineering Satellite Systems [obc-computers] https://newspacemarket.com/products/stengg-obc/ Processor: Dual-Core LEON3-FT Sparc V8 Processor CPU clock: 40 MHz CPU clock: 80 MHz (max) RAM: 32 MB Storage: 0.0078 GB Operating system: RTEMS Real Time Operating System (RTOS) Mass: 950 g Envelope (L×W×H): 215 x 175 x 30 mm3 Supply voltage: 16 (min) Supply voltage: 40 (max) Power consumption: 4.8 W @ Nominal Data interface: CAN Data interface: SpaceWire @ (variant 2) Data interface: MIL-STD-1553 @ (variant 3) Data interface: RS422 @ (variant 4) Data interface: UART @ (variant 5) Data interface: other @ PPS Data interface: LVDS @ (variant 6) Data interface: other @ JTAG Data interface: Ethernet @ (variant 7) Operating temperature: -30 °C (min) Operating temperature: 70 °C (max) Radiation tolerance (TID): 20 krad (min) Design lifetime: 5 years (min) ## MASTER Cubesat On-Board Computer — 2NDSpace Srl [obc-computers] https://newspacemarket.com/products/master-cubesat-on-board-computer/ Envelope (L×W×H): 97 x 92 x 20 Mass: 130 g Processor: Dual-Core ARM Cortex M7 + Cortex M4 CPU clock: 480 MHz @ Cortex M7 CPU clock: 240 MHz @ Cortex M4 RAM: 32 MB Storage: 0.0156 GB @ NOR flash Storage: 0.001 GB @ FRAM Storage: 32 GB @ Dual µSD slots Operating system: FreeRTOS Operating system: Mbed @ (variant 2) Data interface: CAN Data interface: RS-422 @ (variant 2) Data interface: RS-485 @ (variant 3) Data interface: UART @ (variant 4) Data interface: I2C @ (variant 5) Data interface: SPI @ (variant 6) Data interface: other @ ADC Inputs Supply voltage: 5 Power consumption: 2 W @ Peak ## NanoMind A3200 On-Board Computer — GomSpace [obc-computers] https://newspacemarket.com/products/gomspace-nanomind-a3200-obc/ Processor: AVR32 MCU Processor: Atmel AT32UC3C MCU @ (variant 2) CPU clock: 8 MHz (min) CPU clock: 64 MHz (max) CPU clock: 8 MHz (min) @ (variant 2) CPU clock: 32 MHz (typical) CPU clock: 64 MHz (max) @ (variant 2) RAM: 32 MB RAM: 32 MB @ (variant 2) Storage: 0.125 GB Storage: 0.125 GB @ (variant 2) Operating system: FreeRTOS Mass: 24 g Envelope (L×W×H): 65 x 40 x 7.1 mm Supply voltage: 3.2 (min) Supply voltage: 3.3 (typical) Supply voltage: 3.4 (max) Supply voltage: 0 (min) @ PWM from VAUX Supply voltage: 6 (max) @ PWM from VAUX Power consumption: 0.17 W (min) @ VCC_OBC Power consumption: 0.9 W (max) @ VCC_OBC Data interface: I2C Data interface: UART @ (variant 2) Data interface: CAN @ (variant 3) Data interface: SPI @ (variant 4) Data interface: I2C @ (variant 5) Data interface: CAN @ (variant 6) Data interface: UART @ (variant 7) Data interface: I2C @ (variant 8) Data interface: CAN @ (variant 9) Data interface: UART @ (variant 10) Data interface: I2C @ (variant 11) Data interface: CAN @ (variant 12) Data interface: UART @ (variant 13) Data interface: SPI @ (variant 14) Connector: 2 x 20-position hard-gold plated FSI one-piece connector Connector: Molex PicoBlade 53261-0471 @ P1 - Picoblade USART (debug) Connector Connector: Molex PicoBlade 53261-0871 @ P2 - Picoblade Connector for JTAG Connector: Molex PicoBlade 53261-0671 @ P6 - Picoblade Connector with PWM outputs Connector: Molex PicoBlade 53261-0671 @ P7 - Picoblade Connector with I2C and VBAT Connector: 20-position hard-gold plated FSI one-piece connectors @ X1 and X3 - FSI Main Connectors Operating temperature: -30 °C (min) Operating temperature: 85 °C (max) Operating temperature: -30 °C (min) @ (variant 2) Operating temperature: 85 °C (max) @ (variant 2) Operating temperature: -30 °C (min) @ (variant 3) Operating temperature: 85 °C (max) @ (variant 3) Survival temperature: -30 °C (min) Survival temperature: 85 °C (max) ## MASTER-CHIEF Extended On-Board Computer — 2NDSpace Srl [obc-computers] https://newspacemarket.com/products/master-chief-extended-on-board-computer/ Envelope (L×W×H): 97 x 92 x 20 Mass: 130 g Processor: Dual-Core ARM Cortex M7 + Cortex M4 CPU clock: 480 MHz @ Cortex M7 CPU clock: 240 MHz @ Cortex M4 RAM: 64 MB Storage: 0.0313 GB @ serial SPI NOR flash Storage: Dual µSD slots Operating system: Linux Operating system: FreeRTOS @ (variant 2) Data interface: CAN Data interface: RS422 @ (variant 2) Data interface: RS485 @ (variant 3) Data interface: UART @ (variant 4) Data interface: USART @ (variant 5) Data interface: I2C @ (variant 6) Data interface: SPI @ (variant 7) Supply voltage: 5 (nominal) @ regulated Operating temperature: -40-85 °C ## MASTER, MASTER-CHIEF, MASTER-II Cubesat On-Board Computers — 2NDSpace Srl [obc-computers] https://newspacemarket.com/products/master-on-board-computer/ Envelope (L×W×H): 97 x 92 x 20 Mass: 130 g Processor: Dual-Core ARM Cortex M7 + Cortex M4 CPU clock: 480 MHz @ Cortex M7 CPU clock: 240 MHz @ Cortex M4 RAM: 32 MB @ SDRAM Storage: 0.0156 GB @ NOR flash Storage: 0.001 GB @ FRAM Operating system: FreeRTOS Operating system: Mbed @ (variant 2) Storage: 32 GB @ Dual µSD slots up to Data interface: CAN Data interface: RS422 @ (variant 2) Data interface: RS485 @ (variant 3) Data interface: UART @ (variant 4) Data interface: I2C @ (variant 5) Data interface: SPI @ (variant 6) Data interface: other @ ADC Inputs Supply voltage: 5 (nominal) Power consumption: 2 W @ Peak Power Operating temperature: -40-85 °C ## Next Generation On Board Computer (OBC NG) — Beyond Gravity (ex-RUAG Space) [obc-computers] https://newspacemarket.com/products/beyond-gravity-obc-ng-next-generation-on-board-computer/ Envelope (L×W×H): 283 x 242 x 278 mm Mass: 9000 g Power consumption: 38 W @ max Design lifetime: 20 years RAM: 512 MB Data interface: SpaceWire Data interface: CAN @ (variant 2) Data interface: MIL-STD-1553B @ (variant 3) Supply voltage: 28V, 50V or 100V Processor: SPARC V8 LEON FT CPU clock: 75 MHz RAM: 512 MB @ (variant 2) Storage: 0.0078 GB Data interface: Ethernet @ (variant 4) Operating system: RTEMS Flight heritage: EDRS-C, MTG, ExoMars Rover, Hispasat 36W-1, SARah, Electra, Euclid, JUICE ## Kryten-M3 & Kryten-M3 PLUS — AAC Clyde Space [obc-computers] https://newspacemarket.com/products/aac-kryten-m3/ Processor: Smart Fusion 2 SoC including an ARM Cortex-M3 processor CPU clock: 50 MHz RAM: 16 MB Storage: 4 GB Mass: 61.9 g Envelope (L×W×H): 95.89 mm x 90.17 mm x 5.51 mm Power consumption: 0.4 W @ Nominal Power consumption: 1 W @ max Data interface: I2C Data interface: SPI @ (variant 2) Data interface: UART @ (variant 3) Data interface: RS422 @ (variant 4) Data interface: CAN @ (variant 5) Data interface: DTMF @ (variant 6) Data interface: JTAG @ (variant 7) Data interface: LVDS @ (variant 8) Data interface: QSPI @ (variant 9) Data interface: GPIO @ (variant 10) Operating temperature: -40 °C (min) Operating temperature: 80 °C (max) Radiation tolerance (TID): 20 krad Design lifetime: 5 years Flight heritage: Flight proven across multiple mission applications for a range of customer requirements ## EDDIE — Spacemanic s.r.o. [obc-computers] https://newspacemarket.com/products/spacemanic-eddie/ Processor: MSP430FR5994 mixed-signal microcontroller Mass: 25 g Envelope (L×W×H): 67 x 42 x 7.5 mm Supply voltage: 3.3 @ Power Supply Supply voltage: 5 @ for CAN Power consumption: 0.06 W @ average Power consumption: 0.1 W @ peak Storage: 0.0059 GB @ external FRAM Operating system: FreeRTOS Operating system: Custom @ alternative Data interface: UART @ UART-0 Data interface: I2C @ CSP I2C Data interface: RS-485 @ CSP RS485 Data interface: CAN @ CSP CAN Data interface: I2C @ I2C-SENS Data interface: SPI @ SPI-MEM Data interface: I2C @ I2C-ISOL Data interface: SPI @ SPI-0 Data interface: other @ ADC Data interface: other @ PWM Data interface: other @ GPIO Operating temperature: -40 °C (min) Operating temperature: 85 °C (max) Flight heritage: on 10+ missions (e.g. LASARsat, CroCube, GRBBeta and external customers) ## Deep Thought — Spacemanic s.r.o. [obc-computers] https://newspacemarket.com/products/spacemanic-deep-thought/ Processor: Microchip SAMV71Q21 32-bit Arm Cortex M7 RAM: 3 MB @ FRAM Storage: 0.125 GB @ Flash Operating system: FreeRTOS Mass: 25 g Envelope (L×W×H): 67 x 42 x 7 mm Supply voltage: 3.3 Supply voltage: 3 (min) @ Power Input Supply voltage: 3.6 (max) @ Power Input Power consumption: 0.33 W @ average Power consumption: 0.5 W (max) @ peak Data interface: UART @ UART-0 Data interface: I2C @ CSP I2C Data interface: RS-485 @ CSP RS485 Data interface: CAN @ CSP CAN Data interface: I2C @ I2C-SENS Data interface: SPI @ SPI-MEM Data interface: SPI @ QSPI-MEM Data interface: I2C @ I2C-ISOL Data interface: SPI @ SPI-0 Data interface: other @ ADC Data interface: other @ PWM Data interface: other @ GPIO Data interface: other @ RMII Connector: Molex PicoLock 503763-0691 @ Programming (on module) Connector: Molex PicoLock 503764-0601 @ Programming (on motherboard) Connector: Molex SlimStack 55650-0688 @ Main J1 (on module) Connector: Molex SlimStack 54363-0689 @ Main J1 (on motherboard) Operating temperature: -40 °C (min) Operating temperature: 85 °C (max) Flight heritage: on 10+ missions (e.g. LASARsat, CroCube, Planetum-1 and external customers) ## NanoMind A3200 — GomSpace [obc-computers] https://newspacemarket.com/products/gomspace-nanomind-a3200/ Processor: AVR32 MCU Processor: Atmel AT32UC3C MCU @ (variant 2) CPU clock: 8 MHz (min) CPU clock: 64 MHz (max) CPU clock: 8 MHz (min) @ (variant 2) CPU clock: 64 MHz (max) @ (variant 2) RAM: 32 MB RAM: 32 MB @ (variant 2) Storage: 0.125 GB Storage: 0.125 GB @ (variant 2) Operating system: FreeRTOS Mass: 24 g Envelope (L×W×H): 65 x 40 x 7.1 mm Supply voltage: 3.2 (min) Supply voltage: 3.4 (max) Power consumption: 0.17 W @ VCC_OBC Power consumption: 0.9 W (max) @ VCC_OBC Data interface: I2C Data interface: UART @ (variant 2) Data interface: CAN @ (variant 3) Data interface: SPI @ (variant 4) Data interface: I2C @ (variant 5) Data interface: CAN @ (variant 6) Data interface: SPI @ (variant 7) Data interface: UART @ (variant 8) Data interface: JTAG @ (variant 9) Data interface: I2C @ (variant 10) Data interface: I2C @ (variant 11) Data interface: CAN @ (variant 12) Data interface: UART @ (variant 13) Data interface: SPI @ (variant 14) Connector: Picoblade Connector: Picoblade @ (variant 2) Connector: Picoblade @ (variant 3) Connector: Picoblade @ (variant 4) Connector: FSI @ (variant 5) Operating temperature: -30 °C (min) Operating temperature: 85 °C (max) Operating temperature: -30 °C (min) @ (variant 2) Operating temperature: 85 °C (max) @ (variant 2) Operating temperature: -30 °C (min) @ (variant 3) Operating temperature: 85 °C (max) @ (variant 3) Survival temperature: -30 °C (min) Survival temperature: 85 °C (max) Flight heritage: flown successfully on several satellites ## NOVI Space Compute and AI Infrastructure — Novi [obc-computers] https://newspacemarket.com/products/novi-space-mission-as-a-service/ Flight heritage: flight heritage @ demonstrated ## NanoMind Z7000 — GomSpace [obc-computers] https://newspacemarket.com/products/nanomind-z7000/ Processor: Xilinx Zynq 7030 Programmable SoC Dual ARM Cortex A9 MPCore CPU clock: 800 MHz (max) RAM: 1024 MB Storage: 32 GB Operating system: Linux Mass: 28.7 g @ PCB Mass: 76.8 g @ total PCB + shield Envelope (L×W×H): 65 x 40 x 6.5 mm Supply voltage: 3 (min) Supply voltage: 3.6 (max) Power consumption: 2.3 W (max) Data interface: I2C Data interface: CAN @ (variant 2) Data interface: RS-422 @ (variant 3) Data interface: UART @ (variant 4) Data interface: SPI @ (variant 5) Data interface: USB @ (variant 6) Data interface: other @ SD Connector: 2x 100 pin Samtec Connector: 1x Samtec LSHM-130-04.0-L-DV-A-S-K-TR @ (variant 2) Operating temperature: -40 °C (min) Operating temperature: 85 °C (max) Flight heritage: flight proven Flight heritage: in space @ (variant 2) ## Leopard — KP Labs [obc-computers] https://newspacemarket.com/products/leopard/ Processor: AMD Zynq UltraScale+ MPSoC ZU6EG | ZU9EG | ZU15EG Quad ARM Cortex-A53 CPU CPU clock: 1200 MHz Processor: Dual ARM Cortex-R5 @ (variant 2) RAM: 16384 MB RAM: 64 MB @ (variant 2) Storage: 4 GB Operating system: 64-bit Linux (Yocto based) Mass: 725 g Envelope (L×W×H): 95.89 x 90.17 x 47.2 mm Supply voltage: 7-14 Power consumption: 5 W @ min Power consumption: 20 W @ max Data interface: CAN Data interface: UART @ (variant 2) Data interface: RS-422 @ (variant 3) Data interface: RS-485 @ (variant 4) Data interface: LVDS @ (variant 5) Data interface: other @ (variant 6) Data interface: other @ (variant 7) Data interface: Ethernet @ (variant 8) Data interface: SpaceWire @ (variant 9) Data interface: CAN @ (variant 10) Data interface: RS-422 @ (variant 11) Data interface: RS-485 @ (variant 12) Data interface: UART @ (variant 13) Data interface: other @ (variant 14) Data interface: other @ (variant 15) Operating temperature: -25-75 °C Radiation tolerance (TID): 20 krad ## CP400.85 — AAC Clyde Space [obc-computers] https://newspacemarket.com/products/aac-cp400-85/ RAM: 512 MB Storage: 0.5 GB Mass: 7 g Power consumption: 1 W (max) @ peak Envelope (L×W×H): 20 x 50 x 10 mm Processor: ARMv7-A Radiation tolerance (TID): 25 krad Flight heritage: The CP400 has been flying in LEO since 2018 on CubeSat missions and is at TRL 9. CPU clock: 500 MHz RAM: 512 MB @ (variant 2) Storage: 0.5 GB @ (variant 2) Envelope (L×W×H): 50 x 20 x 10 mm @ (variant 2) Mass: 7 g @ (variant 2) Power consumption: 0.55 W @ nominal TRL: 9 Lead time: 16 Operating system: Linux-based ## Q7 Processor — Xiphos Technologies [obc-computers] https://newspacemarket.com/products/xiphos-q7-processor/ Envelope (L×W×H): 78 mm x 43 mm x 9 mm @ without RJ45 connector Mass: 24 g @ excluding connectors Power consumption: 2 W @ typical applications Processor: Dual ARM Cortex A9 MPCore processors Data interface: Ethernet Data interface: USB @ (variant 2) Data interface: LVDS @ (variant 3) Data interface: RS-232 @ (variant 4) Data interface: RS-422 @ (variant 5) Data interface: RS-485 @ (variant 6) Data interface: CAN @ (variant 7) RAM: 1048576 MB @ DDR3L DRAM RAM: 512 MB @ with EDAC Storage: 0.125 GB Storage: 32 GB @ (variant 2) Processor: Xilinx Zynq 7020 @ (variant 2) Processor: Dual core ARM Cortex A9 MPCore processor @ (variant 3) CPU clock: 766 MHz Operating system: Yocto Linux BSP (LTS distribution) Power consumption: 2 W @ typ. Supply voltage: 6 (min) Supply voltage: 15 (max) Supply voltage: 5 (min) @ option Supply voltage: 28 (max) @ option Mass: 32 g @ with RJ45 connector Mass: 24 g @ without RJ45 connector Envelope (L×W×H): 78 mm x 43 mm x 19 mm @ with RJ45 connector Envelope (L×W×H): 78 mm x 43 mm x 9 mm @ without RJ45 connector (variant 2) Operating temperature: -40 °C (min) Operating temperature: 60 °C (max) Data interface: Ethernet @ (variant 8) Connector: RJ45 Data interface: USB @ (variant 9) Connector: Micro AB @ (variant 2) Data interface: CAN @ (variant 10) Data interface: LVDS @ (variant 11) Data interface: RS-232 @ (variant 12) Data interface: RS-422 @ (variant 13) Data interface: RS-485 @ (variant 14) ## Q8 Low SWaP Computer-on-Module — Xiphos Technologies [obc-computers] https://newspacemarket.com/products/xiphos-q8-processor/ Processor: Xilinx Zynq UltraScale+ XCZU7EG (Quad core ARM Cortex A53, Dual core ARM Cortex R5) CPU clock: 1200 MHz @ ARM Cortex A53 CPU clock: 500 MHz @ ARM Cortex R5 RAM: 4096 MB Storage: 0.25 GB @ QSPI Flash Storage: 128 GB @ eMMC each Operating system: Yocto Linux BSP (LTS distribution) Mass: 64 g @ with RJ45 and power connectors Mass: 56 g @ without connectors Envelope (L×W×H): 85.8 mm x 80 mm x 22.6 mm @ with RJ45 and power connectors Envelope (L×W×H): 80 mm x 80 mm x 11.2 mm @ without connectors Supply voltage: 5-15 @ Supply Power consumption: 5 W @ typical Data interface: Ethernet Data interface: USB @ (variant 2) Data interface: RS-232 @ (variant 3) Data interface: RS-422 @ (variant 4) Data interface: RS-485 @ (variant 5) Data interface: CAN @ (variant 6) Data interface: LVDS @ (variant 7) Data interface: other @ (variant 8) Data interface: other @ (variant 9) Data interface: other @ (variant 10) Data interface: other @ (variant 11) Connector: RJ45 Connector: USB Type-C Host port @ (variant 2) Operating temperature: -40-60 °C @ derated Flight heritage: The Q8S, the Flight Model (FM) version of the Q8, has been flying since September 2020. ## Q8J Low SWaP with GTH Computer-on-Module — Xiphos Technologies [obc-computers] https://newspacemarket.com/products/xiphos-q8j-processor/ Processor: quad core ARM Cortex A53 Application Processing Unit; dual core ARM Cortex R5 Real Time Processing Unit; ARM Mali 400 GPU CPU clock: 1200 MHz (max) @ ARM Cortex A53 CPU clock: 500 MHz (max) @ ARM Cortex R5 CPU clock: 600 MHz (max) @ ARM Mali-400 GPU RAM: 4096 MB Storage: 0.25 GB @ QSPI Flash Storage: 128 GB @ eMMC Operating system: Yocto Linux BSP (LTS distribution) Mass: 56 g @ without connectors Envelope (L×W×H): 80 mm x 80 mm x 11.2 mm Supply voltage: 9 Power consumption: 5 W @ typical Data interface: Ethernet Data interface: USB @ (variant 2) Data interface: GPIO @ (variant 3) Data interface: LVDS @ (variant 4) Data interface: other @ Gigabit transceivers Data interface: other @ JESD204B Data interface: other @ PCIe Data interface: RS-232 @ (variant 5) Data interface: RS-422 @ (variant 6) Data interface: RS-485 @ (variant 7) Data interface: CAN @ (variant 8) Data interface: other @ 1-Wire Data interface: other @ analog inputs Data interface: other @ analog outputs Data interface: JTAG @ (variant 9) Data interface: Ethernet @ (variant 10) Data interface: USB @ (variant 11) Data interface: CAN @ (variant 12) Data interface: PCIe @ (variant 13) Data interface: GPIO @ (variant 14) Data interface: LVDS @ (variant 15) Data interface: other @ PL GTH transceivers Data interface: other @ PS GTR transceiver Data interface: RS-232 @ (variant 16) Data interface: RS-422 @ (variant 17) Data interface: RS-485 @ (variant 18) Connector: RJ45 Connector: mezzanine connector @ (variant 2) Connector: RJ45 @ (variant 3) Connector: USB Type-C Host port @ (variant 4) Connector: Mezzanine connector @ (variant 5) Flight heritage: The Q8JS, the Flight Model (FM) version of the Q8J, has been flying since September 2023 ## Xiphos Q9 Versal Computer-on-Module — Xiphos Technologies [obc-computers] https://newspacemarket.com/products/xiphos-q9-versal-computer-on-module/ Processor: AMD Versal AI Core Adaptive System-on-Chip Processor: Dual core ARM Cortex A72 Application Processing Unit @ (variant 2) CPU clock: 1700 MHz (max) @ Application Processing Unit Processor: Dual core ARM Cortex R5F Real-Time Processing Unit @ (variant 3) CPU clock: 750 MHz @ Real-Time Processing Unit RAM: 16384 MB @ LPDDR4 DRAM Storage: 1 GB @ QSPI Flash (NOR) Storage: 1000 GB @ SSD (each) Storage: 0.001 GB @ MRAM Operating system: Yocto Linux BSP (LTS distribution) Mass: 154 g @ without connectors Envelope (L×W×H): 90 mm x 110 mm x 20 mm Supply voltage: 8-14 Power consumption: 30-50 W @ typical Data interface: LVDS Data interface: PCIe Gen 4 @ (variant 2) Data interface: Ethernet @ (variant 3) Data interface: JESD204b @ (variant 4) Data interface: SSD @ (variant 5) Data interface: SERDES @ (variant 6) Data interface: USB 2.0 @ (variant 7) Data interface: CAN @ (variant 8) Operating temperature: -40-60 °C Flight heritage: cumulative time on orbit stands at more than 568 years (As of July 2025), no on-orbit product failures, more than 260 boards in space ## Xiphos Q8RF Family — Xiphos Technologies [obc-computers] https://newspacemarket.com/products/xiphos-q8rf-family/ Storage: 32 GB @ NAND Flash Envelope (L×W×H): 100 mm x 100 mm x 20 mm Mass: 200 g Power consumption: 20 W (min) @ typ. Power consumption: 30 W (max) @ typ. Supply voltage: 5 (min) Supply voltage: 9 (max) RAM: 4096 MB @ PS LPDDR4 DRAM (with EDAC) RAM: 4096 MB @ PL DDR4 DRAM Storage: 0.25 GB @ QSPI Flash (NOR) Processor: Quad-core ARM Cortex A53 Application Processing Unit CPU clock: 1200 MHz @ Application Processing Unit Processor: Dual-core ARM Cortex-R5 @ Real-Time Processing Unit CPU clock: 500 MHz @ Real-Time Processing Unit Operating temperature: -40 °C (min) Operating temperature: 60 °C (max) Operating system: Yocto Linux BSP (LTS distribution) Data interface: LVDS Data interface: GPIO @ 1.8V Data interface: GPIO @ 3.3V Data interface: PCIe Gen 3 @ (variant 2) Data interface: Ethernet @ 100G Data interface: PCIe Gen 2 @ (variant 3) Data interface: other @ SATA Radiation tolerance (TID): 30 krad Connector: 8x Transmit + 8x Receive RF; Ext Ref Clock(s) In, Ref Clock Out ## Pluggable Socketed Processor Module B (PSPM B) — Pumpkin, Inc. [obc-computers] https://newspacemarket.com/products/pumpkin-pluggable-socketed-processor-module-b-pspm-b/ Storage: 128 GB CPU clock: 100 MHz Processor: Silicon Labs® C8051F120 8-bit microcontroller (MCU) RAM: 0.125 MB @ static RAM: 0.125 MB @ external 1Mbit static RAM Operating system: Pumpkin's Salvo™ RTOS Mass: 68 g Envelope (L×W×H): 90 x 96 x 19 mm Supply voltage: 3.3 @ Operating Voltage Supply voltage: 3.3 @ SD Card Voltage Data interface: I2C Data interface: SPI @ (variant 2) Data interface: UART @ (variant 3) Data interface: USB @ (variant 4) Connector: 100-pin clamshell ZIF socket Connector: 100-pin hermaphroditic LSS-150-02-L-DV @ (variant 2) Connector: 10-pin 2x5 0.100" pitch dual-inline header J1 @ (variant 3) Connector: 6-pin 1x6 0.100" pitch inline header J2 @ (variant 4) ## Pluggable Processor Module B1 (PPM B1) — Pumpkin, Inc. [obc-computers] https://newspacemarket.com/products/pumpkin-pluggable-processor-module-b1-ppm-b1/ Processor: Silicon Labs® C8051F120 8-bit microcontroller CPU clock: 100 MHz RAM: 0.125 MB @ program memory RAM: 0.0083 MB @ on-chip RAM RAM: 0.125 MB @ external static RAM RAM: 0.125 MB @ external static RAM (variant 2) RAM: 0.125 MB @ high-speed XRAM Operating system: Salvo™ RTOS Mass: 16 g Envelope (L×W×H): 89.5 x 54.6 x 6 mm Supply voltage: 3.3 @ Operating Voltage Supply voltage: 3.3 @ SD Card Voltage Power consumption: TBD mA @ Typical operation Power consumption: TBD µA @ All control outputs inactive, PPM asleep Data interface: UART Data interface: SPI @ (variant 2) Data interface: I2C @ (variant 3) Data interface: JTAG @ (variant 4) Connector: 100-pin, hermaphroditic Connector: 8-pin FPC connector J1 @ (variant 2) Connector: 6-pin FPC connector J2 @ (variant 3) Storage: 128 GB ## Pluggable Processor Module A1 (PPM A1), with TI’s MSP430F1612 — Pumpkin, Inc. [obc-computers] https://newspacemarket.com/products/pumpkin-pluggable-processor-module-a1-ppm-a1/ Storage: 55 GB Processor: TI's MSP430F1612 16-bit microcontroller (MCU) CPU clock: 7.4 MHz (max) RAM: 0 MB Operating system: Pumpkin's Salvo™ RTOS Mass: 11 g Envelope (L×W×H): 54.6 W x 53.4 L x 1.6 T mm Supply voltage: 5 (max) @ on +5V_USB bus Supply voltage: 5 (max) @ on +5V_SYS bus Supply voltage: 3.6 (max) @ on VCC bus Supply voltage: 3.6 (max) @ on VCC_SD bus Supply voltage: 3.6 (max) @ on any MSP430 I/O pin Data interface: UART Data interface: SPI @ (variant 2) Data interface: I2C @ (variant 3) Connector: LSS-150-01-L-DV Connector: 8-pin FPC @ (variant 2) Operating temperature: -40 °C (min) Operating temperature: 85 °C (max) ## Pluggable Processor Module A2 (PPM A2), with TI’s MSP430F1611 — Pumpkin, Inc. [obc-computers] https://newspacemarket.com/products/pumpkin-pluggable-processor-module-a2-ppm-a2/ Processor: TI's MSP430F1611 16-bit microcontroller (MCU) CPU clock: 7.4 MHz (max) RAM: 0 MB Operating system: Salvo™ RTOS Mass: 11 g Envelope (L×W×H): 54.6 mm x 53.4 mm Supply voltage: 3.3 (nominal) Power consumption: 0.0099 W @ LPM0, MCLK = DCO Power consumption: 0 W @ LMP4, all control outputs inactive, I2C isolator U5 fitted Data interface: I2C Data interface: SPI @ (variant 2) Data interface: UART @ (variant 3) Connector: LSS-150-01-L-DV Operating temperature: -40 °C (min) Operating temperature: 85 °C (max) Storage: 48 GB ## Pluggable Processor Module A3 (PPM A3), with TI’s MSP430F2618 — Pumpkin, Inc. [obc-computers] https://newspacemarket.com/products/pumpkin-pluggable-processor-module-a3-ppm-a3/ Storage: 116 GB Processor: TI's MSP430F2618 16-bit microcontroller (MCU) CPU clock: 7.3728 MHz @ HFXTAL CPU clock: 16 MHz @ MSP430 operating frequency rated RAM: 0.008 MB Operating system: Pumpkin's Salvo™ RTOS Mass: 11 g Envelope (L×W×H): 53.4 x 54.6 mm Supply voltage: 3.3 @ Operating Voltage VCC Supply voltage: 3.3 @ SD Card Voltage VCC_SD Data interface: UART Data interface: SPI @ (variant 2) Data interface: I2C @ (variant 3) Connector: 100-pin, hermaphroditic Samtec LSS-150-01-L-DV Connector: 8-pin FPC connector J1 (for FET) @ (variant 2) Operating temperature: -40-85 °C ## CSP CubeSat Space Processor — Voyager Technologies [obc-computers] https://newspacemarket.com/products/csp-cubesat-space-processor/ Processor: Xilinx Zynq-7020 System on Chip (SOC) Dual Arm Core and Reconfigurable 7-Series FPGA Fabric CPU clock: 766 MHz Storage: 32 GB @ Rad Tolerant NAND Flash RAM: 8192 MB @ DDR3 SDRAM RAM: 4096 MB @ DDR3 SDRAM when EDAC is active Power consumption: 1.6 W (min) Power consumption: 2.85 W (max) Envelope (L×W×H): 8.81 cm x 8.95 cm Envelope (L×W×H): 1.73 cm (tallest component) @ FM Mass: 74 g @ FM Data interface: USB Data interface: Ethernet @ (variant 2) Data interface: SpaceWire @ (variant 3) Data interface: UART @ (variant 4) Data interface: SPI @ (variant 5) Data interface: I2C @ (variant 6) Data interface: other @ (variant 7) Data interface: RS-422 @ (variant 8) Operating temperature: 0 °C (min) @ FM Operating temperature: 70 °C (max) @ FM Connector: Samtec SEAF-RA 4x40 Connector Radiation tolerance (TID): 30 krad Operating system: Bare Metal Operating system: Linux @ (variant 2) Operating system: ThreadX @ (variant 3) ## ODALISS DIPP — Emxys [obc-computers] https://newspacemarket.com/products/emxys-dipp/ Connector: 80-pins high-speed interface backplane connector. Connector: 10-pin Pogo-style for program and debug without mechanical stress. @ (variant 2) Connector: 10-pin Pogo-style for NAND flash data access. @ (variant 3) Envelope (L×W×H): 87 mm x 87 mm x 10 mm. Mass: 60 g Power consumption: 1650 W Processor: dual-core ARM® A9 + FPGA 28k LGs Fabric Storage: 256 GB (max) Operating system: Linux OS Data interface: Ethernet Data interface: SPI @ (variant 2) Data interface: I2C @ (variant 3) Data interface: UART @ (variant 4) Data interface: RS-485 @ (variant 5) Data interface: RS-422 @ (variant 6) Data interface: USB @ (variant 7) ## Q7 Computer-on-Module — Xiphos Technologies [obc-computers] https://newspacemarket.com/products/xiphos-q7/ Radiation tolerance (TID): 25 krad Processor: Dual core ARM Cortex A9 MPCore processor Processor: Xilinx Zynq 7020 @ (variant 2) CPU clock: 766 MHz RAM: 1024 MB RAM: 512 MB @ with EDAC Storage: 0.125 GB Storage: 32 GB @ (variant 2) Operating system: Yocto Linux BSP (LTS distribution) Mass: 24 g @ excluding connectors Mass: 32 g @ with RJ45 connector Mass: 24 g @ without RJ45 connector Envelope (L×W×H): 78 mm x 43 mm x 9 mm @ without RJ45 connector Envelope (L×W×H): 78 mm x 43 mm x 19 mm @ with RJ45 connector Envelope (L×W×H): 78 mm x 43 mm x 9 mm @ without RJ45 connector (variant 2) Supply voltage: 6-15 Supply voltage: 5-28 @ option Power consumption: 2 W @ typical applications Power consumption: 2 W @ typ. Data interface: Ethernet Data interface: USB @ (variant 2) Data interface: LVDS @ (variant 3) Data interface: RS-232 @ (variant 4) Data interface: RS-422 @ (variant 5) Data interface: RS-485 @ (variant 6) Data interface: CAN @ (variant 7) Data interface: RS-232 @ (variant 8) Data interface: RS-422 @ (variant 9) Data interface: RS-485 @ (variant 10) Data interface: other @ 1-Wire Data interface: other @ GPIO Data interface: other @ JTAG Data interface: Ethernet @ (variant 11) Data interface: USB @ (variant 12) Data interface: CAN @ (variant 13) Data interface: other @ GPIO (variant 2) Data interface: LVDS @ (variant 14) Data interface: RS-232 @ (variant 15) Data interface: RS-422 @ (variant 16) Data interface: RS-485 @ (variant 17) Connector: RJ45 connector Connector: Micro AB @ USB 2.0 Host port Connector: Mezzanine connector @ (variant 2) Operating temperature: -40-60 °C Flight heritage: The Q7S, the Flight Model (FM) of the Q7, has been operating in orbit since June 2016. Flight heritage: The Q7S is certified for manned space flight and is used on the International Space Station @ (variant 2) ## Q8 Computer-on-Module — Xiphos Technologies [obc-computers] https://newspacemarket.com/products/xiphos-q8/ Processor: quad core ARM Cortex A53 Application Processing Unit Processor: dual core ARM Cortex R5 Real Time Processing Unit @ (variant 2) Processor: Xilinx Zynq UltraScale+ XCZU7EG @ (variant 3) Processor: Microchip ProASIC3 @ Control FPGA CPU clock: 1200000 MHz @ ARM Cortex A53 CPU clock: 500 MHz @ ARM Cortex R5 RAM: 4096 MB Storage: 0.25 GB @ QSPI Flash (NOR) Storage: 128 GB @ eMMC Operating system: Yocto Linux BSP (LTS distribution) Mass: 64 g @ with RJ45 and power connectors Mass: 56 g @ without connectors Envelope (L×W×H): 85.8 mm x 80 mm x 22.6 mm @ with RJ45 and power connectors Envelope (L×W×H): 80 mm x 80 mm x 11.2 mm @ without connectors Supply voltage: 5-15 Supply voltage: 6-15 @ Input voltage range Supply voltage: 4.5 @ Startup voltage Supply voltage: 4 @ Brownout voltage Power consumption: 5 W @ typical Data interface: Gigabit Ethernet Data interface: USB @ USB 2.0/USB 3.1 Gen 1 Host port Data interface: other @ GPIO Data interface: other @ MIO Data interface: LVDS @ (variant 2) Data interface: RS-232 @ (variant 3) Data interface: RS-422 @ (variant 4) Data interface: RS-485 @ (variant 5) Data interface: CAN @ (variant 6) Data interface: CAN @ (variant 7) Data interface: USB @ USB Type-C Host port (USB 2.0 & USB 3.1 Gen 1) Data interface: RS-232 @ (variant 8) Data interface: RS-422 @ (variant 9) Data interface: RS-485 @ (variant 10) Data interface: other @ GPIO (variant 2) Data interface: other @ MIO (variant 2) Data interface: LVDS @ (variant 11) Data interface: USB @ USB 2.0 Data interface: other @ Gigabit transceivers (SATA, PCI express) Data interface: RS-422 @ Serial port configuration Connector: RJ45 @ Gigabit Ethernet Connector: mezzanine connector Connector: RJ45 @ Gigabit Ethernet (variant 2) Connector: USB Type-C @ (variant 2) Connector: Mezzanine connector @ (variant 3) Operating temperature: -40-60 °C Flight heritage: The Q8S, the Flight Model (FM) version of the Q8, has been flying since September 2020. Radiation tolerance (TID): 30 krad ## Q9 Versal Computer-on-Module — Xiphos Technologies [obc-computers] https://newspacemarket.com/products/xiphos-q9/ Envelope (L×W×H): 90 mm x 110 mm x 20 mm Processor: AMD Versal AI Core Adaptive System-on-Chip Processor: Dual core ARM Cortex A72 Application Processing Unit @ (variant 2) CPU clock: 1700 MHz (max) @ Application Processing Unit Processor: Dual core ARM Cortex R5F Real-Time Processing Unit @ (variant 3) CPU clock: 750 MHz @ Real-Time Processing Unit RAM: 16384 MB RAM: 1024 MB @ (variant 2) Storage: 2000 GB RAM: 1 MB @ (variant 3) Operating system: Yocto Linux BSP (LTS distribution) Mass: 154 g @ without connectors Power consumption: 30 W @ typical Power consumption: 50 W @ typical (variant 2) Supply voltage: 8-14 Operating temperature: -40-60 °C Data interface: GPIO Data interface: USB 2.0 @ (variant 2) Data interface: CAN @ (variant 3) Data interface: 10 GbE @ (variant 4) Data interface: PCIe @ (variant 5) Data interface: PCIe Gen 4 @ (variant 6) Data interface: Ethernet @ (variant 7) Data interface: JESD204b @ (variant 8) Data interface: SERDES @ (variant 9) ## Proton2X-Box — ZIN Technologies [obc-computers] https://newspacemarket.com/products/zin-proton2x-box-avionics-platform/ Flight heritage: Flight-proven, space-ready, proven program heritage Processor: Dual Core PowerPC™ Processor RAM: 2048 MB Storage: 256 GB Operating system: Linux Operating system: VxWorks @ (variant 2) Mass: 150 g Mass: 250 g @ (variant 2) Envelope (L×W×H): 8 in x 6 in x depth dependent on slices Supply voltage: 15 (min) Supply voltage: 50 (max) Data interface: RS-422 Data interface: RS-485 @ (variant 2) Data interface: SpaceWire @ (variant 3) Data interface: UART @ (variant 4) Data interface: GPIO @ (variant 5) Data interface: MIL-STD-1553 @ (variant 6) Data interface: CAN @ (variant 7) Data interface: Ethernet @ (variant 8) Operating temperature: -20 °C (min) Operating temperature: 100 °C (max) Radiation tolerance (TID): 30 krad (min) Radiation tolerance (TID): 100 krad (max) ## Proton600K Multi-Core Processor — ZIN Technologies [obc-computers] https://newspacemarket.com/products/zin-proton600k-multi-core-processor/ Processor: Dual Arm Cortex-A72 application cores CPU clock: 1600 MHz Processor: Quad Arm Cortex-A53 application cores @ (variant 2) CPU clock: 1260 MHz @ (variant 2) Processor: Dual Arm Cortex-M4F real-time cores @ (variant 3) CPU clock: 266 MHz @ (variant 3) Processor: Dual ARM Cortex-M4 System Controller Unit @ (variant 4) Processor: Dedicated ARM Cortex-M0+ Security Processor @ (variant 5) Processor: Dual 32-bit Graphics Processing Units and Video Processing Unit @ (variant 6) RAM: 2048 MB RAM: 8192 MB @ (variant 2) Storage: 0.0001 GB Storage: 64 GB @ (variant 2) Operating system: Linux Operating system: VxWorks @ (variant 2) Operating system: Integrity @ (variant 3) Operating system: Green Hills @ (variant 4) Data interface: other @ Backplane Triple Serial RapidIO Fat Pipe (X4) Interfaces Data interface: SpaceWire @ Backplane Dual SpaceWire Thin Pipe (X2) Interfaces Data interface: LVDS @ Backplane Sixteen LVDS Transmitters and Sixteen Receivers Data interface: Ethernet @ Front Panel 10/100/1000Base-T Ethernet Port Data interface: RS-422 @ Front Panel Dual RS422 UART Ports Envelope (L×W×H): 3U Open VPX Mass: 350 g @ per PCBA, estimated Power consumption: 12 W @ Peak Power (Executing Coremark Benchmark) ## ProtonVPX-Box — ZIN Technologies [obc-computers] https://newspacemarket.com/products/zin-protonvpx-box-avionics-platform/ Radiation tolerance (TID): 100 krad Operating temperature: -40-100 °C Envelope (L×W×H): 10.35” L x 5.93” W x 5.7” H Mass: 6000 g Power consumption: 40 W Supply voltage: 28 @ DC Data interface: Ethernet Data interface: LVDS @ (variant 2) Data interface: SpaceWire @ (variant 3) Data interface: RS422 @ (variant 4) Data interface: CAN @ (variant 5) Processor: Proton600K multi-core high-performance space processor ## Sterna — EDGX [obc-computers] https://newspacemarket.com/products/sterna-3697/ Random vibration: 14.14 Processor: 8-Core ARM Cortex-A78AE CPU clock: 2000 MHz RAM: 16384 MB Operating system: A custom, space-hardened Linux operating system. Operating system: Optimized Linux OS ( Yocto / JetPack 6) @ (variant 2) Operating system: FreeRTOS @ (variant 3) Mass: 350 g Envelope (L×W×H): 96 x 90 x 30 mm Supply voltage: 15-30 Supply voltage: 23-30 @ Super Power consumption: 15 W @ avg Power consumption: 30 W @ peak Power consumption: 45 W @ super Power consumption: 10-40 W Data interface: CAN Data interface: CAN @ (variant 2) Data interface: Ethernet @ (variant 3) Data interface: UART @ (variant 4) Data interface: Ethernet @ (variant 5) Data interface: USB @ (variant 6) Data interface: PCIe Gen4 x4 @ (variant 7) Data interface: USB @ (variant 8) Data interface: MIPI CSI-2 @ (variant 9) Data interface: Ethernet @ (variant 10) Data interface: SpaceWire @ (variant 11) Connector: Harwin Gecko-SL Connector: Harwin Gecko-SL @ (variant 2) Connector: Samtec ERF8 @ (variant 3) Operating temperature: -20-65 °C Operating temperature: -25-70 °C @ (variant 2) Survival temperature: -40-80 °C Radiation tolerance (TID): 30 krad ## Pumpkin CubeSat Kit Motherboard Module 2 (MBM2) — Pumpkin, Inc. [obc-computers] https://newspacemarket.com/products/pumpkin-cubesat-kit-motherboard-module-2-mbm2/ Processor: BeagleBone Black (BBB) SBC Operating system: Linux Mass: 34 g Envelope (L×W×H): 90 mm (length) x 96 mm (width) x 11 mm (height of components above PCB) Data interface: UART Data interface: SPI @ (variant 2) Data interface: I2C @ (variant 3) Data interface: GPIO @ (variant 4) Data interface: Ethernet @ (variant 5) Data interface: USB @ (variant 6) Data interface: RS-422 @ (variant 7) Data interface: LVTTL @ (variant 8) Connector: 104-pin CubeSat Kit Bus Connector: 25-pin high-density PHY connector @ (variant 2) Connector: 6-pin DF13 connector @ (variant 3) Connector: 4-pin FPC connector @ (variant 4) Connector: 100BASET / RJ45 @ (variant 5) Connector: USB type A @ (variant 6) Connector: USB micro-B @ (variant 7) Connector: micro-HDMI @ (variant 8) Connector: micro-SD socket @ (variant 9) Connector: 1x6 SIP header @ (variant 10) Connector: 2.1/5.5mm barrel jack @ (variant 11) ## Pumpkin Motherboard Module (MBM) 2 Rev. F — Pumpkin, Inc. [obc-computers] https://newspacemarket.com/products/pumpkin-motherboard-module-mbm-2-rev-f/ Operating system: Linux Mass: 34 g Envelope (L×W×H): 96 mm x 90 mm x 11 mm Data interface: Ethernet Data interface: USB @ (variant 2) Data interface: UART @ (variant 3) Data interface: SPI @ (variant 4) Data interface: I2C @ (variant 5) Data interface: RS-422 @ (variant 6) Data interface: RS-485 @ (variant 7) Supply voltage: -0.3-6 Supply voltage: -0.3-6 @ (variant 2) Supply voltage: -0.3-3.6 @ (variant 3) Supply voltage: -0.3-3.6 @ (variant 4) Connector: 2.54 mm Supply voltage: 6 Supply voltage: 3-3.5 @ (variant 5) CPU clock: 32.768 MHz CPU clock: 400 MHz @ (variant 2) ## FoX Payload Processor — Beyond Gravity (ex-RUAG Space) [obc-computers] https://newspacemarket.com/products/beyond-gravity-fox-payload-processor/ Envelope (L×W×H): 148x128x217 mm3 Random vibration: 15 Mass: 3600 g @ 4-slot Mass: 7600 g @ 9-slot Operating temperature: -20-60 °C Radiation tolerance (TID): 36 krad (max) Design lifetime: 10 years RAM: 4194304 MB Storage: 20 GB ## FoX Electronics Platform — Beyond Gravity (ex-RUAG Space) [obc-computers] https://newspacemarket.com/products/beyond-gravity-fox-electronics-platform-2/ Operating temperature: -20 °C (min) Operating temperature: 60 °C (max) Radiation tolerance (TID): 36 krad (min) Design lifetime: 10 years (min) @ LEO, MEO and GEO Random vibration: 15 ## Lion — KP Labs [obc-computers] https://newspacemarket.com/products/lion/ Processor: Kintex Ultrascale KU060 RAM: 16384 MB Storage: 1 GB Data interface: SpaceWire Data interface: other @ (variant 2) Data interface: CAN @ (variant 3) Supply voltage: 12 (nominal) Power consumption: 30 W @ peak ## iX20 — Unibap Space Solutions AB [obc-computers] https://newspacemarket.com/products/ix20/ Operating system: Aluminium ~5 mm Processor: AMD Ryzen 8000-series ram_gb: 64 Storage: 4096 GB Envelope (L×W×H): 177 x 177 x 45 mm Mass: 1820 g Supply voltage: 9-32 Power consumption: 7 W @ idle Power consumption: 40-50 W @ typical Data interface: LVDS Data interface: USB @ (variant 2) Data interface: CAN @ (variant 3) Data interface: Ethernet @ (variant 4) Data interface: I2C @ (variant 5) Data interface: RS422 @ (variant 6) Data interface: SpaceWire @ (variant 7) Data interface: PCIe @ (variant 8) Operating temperature: -20-55 °C ## HDS6603B 6U OpenVPX, SOSA-aligned, Multiprocessing Board — Mercury Systems [obc-computers] https://newspacemarket.com/products/hds6603b-6u-openvpx-sosa-aligned-multiprocessing-board/ RAM: 65536 MB @ per processor RAM: 131072 MB @ planned, for 256GB total blade memory RAM: 131072 MB @ on-board DRAM CPU clock: 1800 MHz @ E5-2648L v4 CPU clock: 2200 MHz @ E5-2618L v4 RAM: 131072 MB @ with ECC (256GB planned) Storage: 16 GB Power consumption: 75 W @ per processor Power consumption: 200 W @ per blade Processor: Dual Intel 2.2 GHz 10-core or 1.8 GHz 14-core Xeon (Broadwell) server-class processors ## GSC6204 6U OpenVPX GPGPU Coprocessing Board — Mercury Systems [obc-computers] https://newspacemarket.com/products/gsc6204-6u-openvpx-gpgpu-coprocessing-board/ RAM: 32768 MB Processor: 2x embedded NVIDIA Quadro TU104 GPU with the Turing architecture ram_gb: 32 Data interface: PCIe Gen 3 Data interface: NVIDIA NVlink @ (variant 2) Data interface: I2C @ (variant 3) Power consumption: 170 W @ per accelerator ## HDS6605 6U OpenVPX Multiprocessing Board — Mercury Systems [obc-computers] https://newspacemarket.com/products/hds6605-6u-openvpx-multiprocessing-board/ Processor: Intel Xeon SP 6238T 22-core server-class processor with AVX512 acceleration CPU clock: 1900 MHz RAM: 196608 MB Storage: 256 GB Operating system: Linux Data interface: Ethernet Data interface: Ethernet @ (variant 2) Data interface: PCIe Gen3 @ (variant 3) Data interface: Ethernet @ (variant 4) Data interface: Ethernet @ (variant 5) Data interface: USB @ (variant 6) Data interface: SATA @ (variant 7) Data interface: I2C @ (variant 8) Data interface: RS-232 @ (variant 9) Data interface: RS-422 @ (variant 10) Data interface: RS-485 @ (variant 11) ## SCFE6120 6U OpenVPX FPGA Carrier Board — Mercury Systems [obc-computers] https://newspacemarket.com/products/scfe6120-6u-openvpx-fpga-carrier-board/ Envelope (L×W×H): Single Slot 6U OpenVPX form factor Processor: Two Xilinx Virtex® Ultrascale+™ VU9P Prosecutors Processor: One Xilinx Zynq® Ultrascale+™ ZU11EG Governor @ (variant 2) RAM: 20480 MB Storage: 2 GB Storage: 2 GB @ (variant 2) Operating system: embedded Linux Data interface: PCIe Data interface: Ethernet @ (variant 2) Data interface: RS-232 @ (variant 3) Data interface: RS-485 @ (variant 4) Data interface: LVDS @ (variant 5) ## SCFE3820 3U OpenVPX FPGA Carrier Board — Mercury Systems [obc-computers] https://newspacemarket.com/products/scfe3820-3u-openvpx-fpga-carrier-board/ Processor: One Xilinx Zynq® Ultrascale+™ ZU11EG governor RAM: 8192 MB Operating system: embedded Linux ## SCFE3821 3U OpenVPX FPGA Board — Mercury Systems [obc-computers] https://newspacemarket.com/products/scfe3821-3u-openvpx-fpga-board/ RAM: 8192 MB Operating system: embedded Linux Processor: One Xilinx Zynq® Ultrascale+™ ZU11EG governor Processor: One Xilinx Virtex® Ultrascale+™ VU7P prosecutor @ (variant 2) ## SCFE6110 6U OpenVPX FPGA Board — Mercury Systems [obc-computers] https://newspacemarket.com/products/scfe6110-6u-openvpx-fpga-board/ Operating temperature: -25 °C Operating temperature: -40 °C @ (variant 2) Processor: Two Xilinx Kintex UltraScale KU115 Prosecutors Processor: One Xilinx Kintex UltraScale KU115 Governor @ (variant 2) Processor: One Xilinx Zynq UltraScale+ ZU9 System Processor @ (variant 3) RAM: 4096 MB @ per Prosecutor FPGA (512MX64) RAM: 4096 MB @ connected to Governor FPGA (512MX64) RAM: 2048 MB @ connected to System FPGA RAM: 18 MB @ QDR4 SRAM, per Prosecutor FPGA Operating system: Embedded PetaLinux Board Support Package Operating system: embedded Linux @ (variant 2) ## SFM6126 6U OpenVPX Network Switch Board — Mercury Systems [obc-computers] https://newspacemarket.com/products/sfm6126-6u-openvpx-network-switch-board/ Data interface: Ethernet Data interface: other @ PCIe Gen3 Supply voltage: 12V @ payload power Supply voltage: 3.3V @ management power Envelope (L×W×H): 160mm x 233.33mm ## SFM6105 6U OpenVPX Network Switch Board — Mercury Systems [obc-computers] https://newspacemarket.com/products/sfm6105-6u-openvpx-network-switch-board/ Envelope (L×W×H): 160mm x 233.33mm Supply voltage: 12 @ payload power Supply voltage: 3.3 @ management power ## SFM6104 6U OpenVPX, SOSA-aligned, Network Switch Board — Mercury Systems [obc-computers] https://newspacemarket.com/products/sfm6104-6u-openvpx-sosa-aligned-network-switch-board/ Processor: Freescale P3041 @ Fabric manager RAM: 2048 MB @ Fabric manager Processor: Renesas H8S/2166 or Smart Fusion FPGA @ System manager Data interface: Ethernet Data interface: other @ (variant 2) Data interface: Ethernet @ (variant 3) Data interface: other @ (variant 4) Data interface: Ethernet @ (variant 5) Data interface: Ethernet @ (variant 6) Data interface: Ethernet @ (variant 7) Data interface: Ethernet @ (variant 8) Data interface: I2C @ (variant 9) Data interface: Ethernet @ (variant 10) Data interface: other @ (variant 11) Data interface: Ethernet @ (variant 12) Data interface: Ethernet @ (variant 13) Data interface: other @ (variant 14) Data interface: other @ (variant 15) Data interface: other @ (variant 16) Data interface: other @ (variant 17) Data interface: Ethernet @ (variant 18) Data interface: Ethernet @ (variant 19) Data interface: Ethernet @ (variant 20) Data interface: Ethernet @ (variant 21) Data interface: RS-232 @ (variant 22) Data interface: I2C @ (variant 23) Data interface: Ethernet @ (variant 24) Data interface: RS-232 @ (variant 25) Envelope (L×W×H): 6U OpenVPX Connector: RJ45 @ Front-Panel I/O Connector: RJ45 @ Front-Panel I/O (variant 2) Connector: RJ45 @ Front-Panel I/O (variant 3) Connector: QSFP @ Front-Panel I/O (variant 4) ## CCM6020 6U OpenVPX I/O Carrier Board — Mercury Systems [obc-computers] https://newspacemarket.com/products/ccm6020-6u-openvpx-i-o-carrier-board/ Data interface: I2C Data interface: PCI Express @ (variant 2) Data interface: PCI-X @ (variant 3) Data interface: PCI @ (variant 4) Data interface: RS-232 @ (variant 5) ## SCM6010 & CAN6000 6U OpenVPX SSD Storage — Mercury Systems [obc-computers] https://newspacemarket.com/products/scm6010-can6000-6u-openvpx-ssd-storage/ Mass: 48100 g Storage: 24576 GB (max) @ total module storage capability Supply voltage: 12 (nominal) @ payload power Supply voltage: 3.3 (nominal) @ management power ## IOM-300 XMC I/O Interface Board — Mercury Systems [obc-computers] https://newspacemarket.com/products/iom-300-xmc-i-o-interface-board/ RAM: 5120 MB Storage: 0.125 GB Data interface: PCIe Data interface: Ethernet @ (variant 2) Data interface: Fibre Channel @ (variant 3) Data interface: sFPDP @ (variant 4) Data interface: LVDS @ (variant 5) Processor: Gen 2 x8 or Gen 3 x8 Envelope (L×W×H): 6.6" x 2.9" ## CCM3012 3U OpenVPX I/O Carrier Board — Mercury Systems [obc-computers] https://newspacemarket.com/products/ccm3012-3u-openvpx-i-o-carrier-board/ Data interface: PCIe @ Gen-3 interfaces to OpenVPX data plane Data interface: PCIe @ Gen-3 interface to processing modules Data interface: PCIe @ Gen-3 interfaces Data interface: PCIe @ Gen-3, backplane, 16 lanes Data interface: PCIe @ Gen-3, upstream x16 PCIe link Data interface: PCIe @ Gen-3, downstream x8 PCIe link to XMC site Data interface: PCIe @ Gen-3, x4 link to the PCI/PCI-X bridge for PMC site Data interface: PCI-X @ PMC site, up to 133 MHz Data interface: PCIe @ XMC site, x8, x4, and x1 PCIe interfaces Data interface: PCIe @ Gen-1, Gen-2, and Gen-3 PCIe data rates Data interface: I2C @ bus Data interface: I2C @ XMC Data interface: PCIe @ x8 Gen3 Data interface: PCIe @ x4 Gen3 Data interface: PCIe @ x1 Gen2 Data interface: PCI-X @ 64-bit Data interface: PCIe @ x4 Gen1 Data interface: RS-232 @ from IPMC Connector: J15 connector Connector: VITA 61 compliant connectors @ (variant 2) Connector: J16 connector @ (variant 3) Data interface: I2C @ interface to backplane Data interface: RS-232 @ serial interface from IPMC to backplane interface ## IOM-400 XMC I/O Interface Board — Mercury Systems [obc-computers] https://newspacemarket.com/products/iom-400-xmc-i-o-interface-board/ Processor: Xilinx Kintex Ultrascale+ FPGA Processor: Xilinx Ultrascale+ KU11P @ default Processor: KU15P FPGA @ optional RAM: 8192 MB Storage: 0.25 GB Data interface: PCIe Data interface: Ethernet @ (variant 2) Data interface: other @ Fiber links Data interface: other @ XMC P16 ports Operating system: Gen3 x8 via P15 XMC connector ## LDS3517 3U OpenVPX Single Board Computer — Mercury Systems [obc-computers] https://newspacemarket.com/products/lds3517-3u-openvpx-single-board-computer/ Processor: Intel Xeon D family server-class processor Processor: Intel 8-core, 64 bit, Xeon D-1539 @ (variant 2) RAM: 16384 MB RAM: 16384 MB @ (variant 2) Data interface: Ethernet Data interface: PCIe @ (variant 2) Data interface: Ethernet @ control plane Data interface: USB @ (variant 3) Data interface: SATA @ (variant 4) Data interface: Ethernet @ control plane (variant 2) Data interface: PCIe Gen3 x8 @ (variant 5) Data interface: PCIe Gen2 x4 @ (variant 6) Data interface: I2C @ (variant 7) Data interface: Ethernet @ 10/100/1000BASE-T Data interface: RS-422 @ (variant 8) Data interface: RS-232 @ (variant 9) Data interface: USB @ (variant 10) Data interface: SATA @ (variant 11) ## LDS6525 6U OpenVPX Single Board Computer — Mercury Systems [obc-computers] https://newspacemarket.com/products/lds6525-6u-openvpx-single-board-computer/ Processor: Intel Quad-Core i7-4700EQ (Haswell mobile class) CPU clock: 2400000 MHz RAM: 8192 MB Storage: 8 GB Operating system: Linux Data interface: Ethernet Data interface: InfiniBand @ (variant 2) Data interface: PCIe @ (variant 3) Data interface: Ethernet @ (variant 4) Data interface: RS-232 @ (variant 5) Data interface: RS-422 @ (variant 6) Data interface: USB @ (variant 7) Data interface: SATA @ (variant 8) Data interface: I2C @ (variant 9) Data interface: GPIO @ (variant 10) ## LDS6527 6U OpenVPX Single Board Computer — Mercury Systems [obc-computers] https://newspacemarket.com/products/lds6527-6u-openvpx-single-board-computer/ Processor: Intel 12-core, 64 bit, Xeon D-1559 CPU clock: 1500 MHz RAM: 16777216 MB (min) RAM: 33554432 MB (max) Storage: 32 GB @ flash device Operating system: Linux Data interface: Ethernet Data interface: InfiniBand @ (variant 2) Data interface: PCIe @ (variant 3) Data interface: USB @ (variant 4) Data interface: SATA @ (variant 5) Data interface: Ethernet @ (variant 6) Data interface: I2C @ (variant 7) Data interface: Ethernet @ (variant 8) Data interface: Ethernet @ (variant 9) Data interface: Ethernet @ (variant 10) Data interface: Ethernet @ (variant 11) Data interface: UART @ TIA-232 serial port Data interface: USB @ (variant 12) Data interface: USB @ (variant 13) Data interface: SATA @ (variant 14) Data interface: RS-232 @ (variant 15) Data interface: RS-422 @ (variant 16) Data interface: RS-232 @ (variant 17) Data interface: RS-422 @ (variant 18) Data interface: USB @ (variant 19) Data interface: USB @ (variant 20) Data interface: USB @ (variant 21) Data interface: SATA @ (variant 22) ## LDS3507 3U OpenVPX, CMOSS/SOSA-aligned, Single Board Computer — Mercury Systems [obc-computers] https://newspacemarket.com/products/lds3507-3u-openvpx-cmoss-sosa-aligned-single-board-computer/ Processor: Intel Xeon D CPU 12-core CPU clock: 1500000 MHz Processor: Xilinx Zynq Ultrascale+ ZU19 quad core SoC FPGA @ (variant 2) RAM: 16384 MB Operating system: LSP RedHat 7.7 Data interface: Ethernet @ Data Plane Data interface: Ethernet @ Control Plane Data interface: PCIe @ Expansion Plane Data interface: SATA Data interface: USB @ (variant 2) Data interface: UART @ (variant 3) Data interface: I2C @ (variant 4) ## CB3P-6231 3U OpenVPX Network Switch Board and Carrier with BuiltSAFE — Mercury Systems [obc-computers] https://newspacemarket.com/products/cb3p-6231-3u-openvpx-network-switch-board-and-carrier-with-builtsafe/ Power consumption: 7 W @ typical Power consumption: 12 W @ maximum Operating temperature: -55 °C Operating temperature: -40 °C @ (variant 2) ## MFCC-8558 XMC Single Board Computer with BuiltSAFE — Mercury Systems [obc-computers] https://newspacemarket.com/products/mfcc-8558-xmc-single-board-computer-with-builtsafe/ Processor: NXP QorIQ T2080 four dual threaded e6500 cores RAM: 4096 MB Storage: 4 GB @ NAND Flash EPROM Storage: 0.5 GB @ NOR Flash EPROM Operating system: VxWorks®653 (partitioned) Power consumption: 15 W @ typical Power consumption: 20 W (max) Data interface: PCIe Gen2 @ 3x x1 on XMC-P6 Data interface: PCIe Gen2 @ 1x x4 on XMC-P5 Data interface: SGMII @ 1x on XMC-P6 (DAL-C) Data interface: UART @ 2x on XMC-P6 Data interface: Ethernet @ 1x 1000BASE-BX interface on XMC-P6 Data interface: USB @ 1x USB 2.0 HOST on XMC-P6 Data interface: SGMII @ 1x interface on XMC-P6 Data interface: UART @ 4x over USB on XMC-P6 Data interface: USB @ 1x USB 2.0 OTG on XMC-P6 Data interface: SATA @ 1x SATA 2.0 on XMC-P6 Operating temperature: 0-55 °C @ A1 Operating temperature: -40-85 °C @ C4 Survival temperature: -55-105 °C ## ROCK-2 3U OpenVPX Mission Computer, BUILTSAFE™ — Mercury Systems [obc-computers] https://newspacemarket.com/products/rock-2-3u-openvpx-mission-computer-builtsafe/ Processor: Freescale QorIQ™ T2080 Processor: Intel® Core™ i7 @ (variant 2) Processor: Xeon @ (variant 3) Storage: 512 GB Mass: 4000 g (min) Mass: 8000 g (max) Envelope (L×W×H): 124 x 194 x up to 335 mm (W x H x D) Power consumption: 40 W @ Minimum Typical Power consumption: 150 W @ Typical Power consumption: 180 W @ Maximum Data interface: MIL-STD-1553 Data interface: other @ ARINC-429 Data interface: RS-232/422/485 @ (variant 2) Data interface: other @ GPIO Data interface: other @ HD-SDI Data interface: other @ 3G-SDI Data interface: other @ DVI Data interface: other @ DisplayPort Data interface: Ethernet @ Fast Ethernet (100BASE-T) Data interface: Ethernet @ Gigabit Ethernet (1000BASE-T) Data interface: USB @ USB 2.0 HOST Data interface: USB @ USB 2.0 OTG Operating system: VxWorks®653 Operating system: INTEGRITY-178 tuMP® @ (variant 2) Operating system: Linux @ (variant 3) Operating temperature: -40-70 °C Survival temperature: -55-85 °C ## ATLAS Hold Down and Release Actuator — SPACERACE s.r.o. [separation-systems] https://newspacemarket.com/products/spacerace-atlas22-release-actuator/ Preload / holding force: 22 kN @ Max. release preload Mass: 270 g @ without harness and connector Release time: 50 ms (max) @ @ 7A with ATLAS control electronics (ICU) ## UNIKA HDRM Preload Device — SPACERACE s.r.o. [separation-systems] https://newspacemarket.com/products/spacerace-unika-preload-device/ Preload / holding force: 50 kN (max) Mass: 2000 g @ without harness and power source Cycles / reuses: 100 @ guaranteed preloads, SMA element Power consumption: 150 W (max) @ peak ## Deployment System 200 kg — KOSMOLAB Launch Services [separation-systems] https://newspacemarket.com/products/kosmolab-lso-200/ Mass: 13500 g Release time: 1000 ms (max) Operating temperature: -60 °C (min) Operating temperature: 60 °C (max) Lead time: 6 (min) Lead time: 9 (max) ## Deployment System 500 kg — KOSMOLAB Launch Services [separation-systems] https://newspacemarket.com/products/kosmolab-lso-500/ Mass: 17000 g Release time: 1000 ms (max) Operating temperature: -60-60 °C Lead time: 6-9 ## CarboNIX — Exolaunch [separation-systems] https://newspacemarket.com/products/exolaunch-carbonix/ Mass: 230 g @ S-Ring ST, C8 Mass: 340 g @ S-Ring ST, C11.732 Mass: 430 g @ S-Ring ST, C15 Mass: 510 g @ S-Ring ST, C18.25 Mass: 630 g @ S-Ring ST, C24 Mass: 270 g @ S-Ring IM, C8 Mass: 390 g @ S-Ring IM, C11.732 Mass: 510 g @ S-Ring IM, C15 Mass: 590 g @ S-Ring IM, C18.25 Mass: 740 g @ S-Ring IM, C24 Mass: 1520 g @ L-Ring, C8 Mass: 2010 g @ L-Ring, C11.732 Mass: 2520 g @ L-Ring, C15 Mass: 2950 g @ L-Ring, C18.25 Mass: 3640 g @ L-Ring, C24 Release time: 100 ms @ average separation time Supply voltage: 28 @ nominal separation signal for 0.5s Operating temperature: -34 °C @ lower operating limit Operating temperature: 71 °C @ upper operating limit Survival temperature: -55 °C @ lower survival limit Survival temperature: 130 °C @ upper survival limit Release shock: 2000 @ lock mechanism qualification, at 1 kHz Release shock: 5000 @ lock mechanism qualification, at 10 kHz Flight heritage: Since the first CarboNIX demonstration on orbit in 2019, CarboNIX has deployed over 70 customer satellites to orbit. CarboNIX users include the undisputed leaders in the smallsat industry, including Planet, Iceye, Satellogic, NanoAvionics and Loft Orbital ## ATLAS ICU (Initiation Control Unit) — SPACERACE s.r.o. [separation-systems] https://newspacemarket.com/products/spacerace-atlas-icu/ Data interface: USB Operating temperature: 0-40 °C Envelope (L×W×H): 250 x 270 x 100 mm Mass: 2900 g @ without cables ## Deployment System 50 kg — KOSMOLAB Launch Services [separation-systems] https://newspacemarket.com/products/kosmolab-lso-050/ Operating temperature: -60 °C Mass: 4000 g ## Deployment System 100 kg — KOSMOLAB Launch Services [separation-systems] https://newspacemarket.com/products/kosmolab-lso-100/ Mass: 8000 g Operating temperature: -60-60 °C Lead time: 6-9 ## Deployment Sequencer BU-12 — KOSMOLAB Launch Services [separation-systems] https://newspacemarket.com/products/kosmolab-bu-12/ Envelope (L×W×H): 300 × 235 × 145 mm Mass: 4500 g Supply voltage: 28 @ Payload supply voltage Operating temperature: -35-60 °C Lead time: 4-6 Flight heritage: TPK SERIES deployer have been flight-qualified as part of the Angara-A5 launch vehicle (2024 launch). All satellites were successfully deployed into target orbits. ## Deployment Sequencer BU-24 — KOSMOLAB Launch Services [separation-systems] https://newspacemarket.com/products/kosmolab-bu-24/ Envelope (L×W×H): 300 x 235 x 145 mm Mass: 5000 g Supply voltage: 28 (nominal) Operating temperature: -35-60 °C Lead time: 4-6 Flight heritage: flight-qualified as part of the Angara-A5 launch vehicle (2024 launch) ## Deployment Sequencer BU-36 — KOSMOLAB Launch Services [separation-systems] https://newspacemarket.com/products/kosmolab-bu-36/ Envelope (L×W×H): 300 × 235 × 145 mm Mass: 5500 g Operating temperature: -35-60 °C Lead time: 4-6 Flight heritage: TPK SERIES deployer have been flight-qualified as part of the Angara-A5 launch vehicle (2024 launch). All satellites were successfully deployed into target orbits. Supply voltage: 28 ## Electric Lock — KOSMOLAB Launch Services [separation-systems] https://newspacemarket.com/products/kosmolab-electric-lock-28v/ Envelope (L×W×H): 48.7 × 37.4 × 22.4 mm Mass: 100 g (max) Operating temperature: -60-60 °C Lead time: 2-3 ## SAU&RON — UARX Space [separation-systems] https://newspacemarket.com/products/sauron-separation-system/ Mass: 1400 g (min) @ Total mass (without i/f screws and harness) Mass: 350 g (max) @ Ride-On mass (flyaway) Release time: 100 ms (max) @ Actuation response time Supply voltage: 28 (nominal) @ Actuator type and voltage Release time: 1000 ms (nominal) @ Release signal ## Fast-Acting Shockless Separation Nut (FASSN) 30K — Sierra Space [separation-systems] https://newspacemarket.com/products/sierra-lsrm-5k-low-shock-release-mechanism/ Envelope (L×W×H): 127 mm x 127 mm x 127 mm @ Nut Mass: 2900 g (max) @ Nut Preload / holding force: 44.5 kN (min) Preload / holding force: 133.4 kN (max) Release time: 200 ms (max) Release shock: 100 (max) ## Explosive Bolts — PacSci EMC [separation-systems] https://newspacemarket.com/products/pacsci-emc-explosive-bolts/ Operating temperature: -65 °C (min) Operating temperature: -3.1 °C (max) ## Separation Nut PSM 1/2B — Beyond Gravity (ex-RUAG Space) [separation-systems] https://newspacemarket.com/products/beyond-gravity-separation-nut-psm-1-2b/ Random vibration: 50 Preload / holding force: 50 kN @ nominal Mass: 430 g Envelope (L×W×H): 77 mm Height Operating temperature: -68-120 °C Release time: 2 ms ## Separation Nut PSM 3/8B — Beyond Gravity (ex-RUAG Space) [separation-systems] https://newspacemarket.com/products/beyond-gravity-separation-nut-psm-3-8b/ Preload / holding force: 25 kN @ nominal Mass: 230 g Envelope (L×W×H): Height 58.5 mm Release time: 2 ms @ dispersion Random vibration: 50 ## Deployment System 50 kg — KOSMOLAB Launch Services [separation-systems] https://newspacemarket.com/products/deployment-system-50-kg/ Operating temperature: -60 °C Mass: 4000 g ## Electric Lock — KOSMOLAB Launch Services [separation-systems] https://newspacemarket.com/products/electric-lock/ Mass: 100 g (max) Operating temperature: -60-60 °C Lead time: 2-3 Flight heritage: TPK SERIES deployer have been flight-qualified as part of the Angara-A5 launch vehicle (2024 launch). All satellites were successfully deployed into target orbits. Envelope (L×W×H): 48.7 × 37.4 × 22.4 mm ## Deployment System 100 kg — KOSMOLAB Launch Services [separation-systems] https://newspacemarket.com/products/deployment-system-100-kg/ Mass: 8000 g Operating temperature: -60 °C (min) Operating temperature: 60 °C (max) Lead time: 6 (min) Lead time: 9 (max) ## Deployment System 200 kg — KOSMOLAB Launch Services [separation-systems] https://newspacemarket.com/products/deployment-system-200-kg/ Mass: 13500 g Release time: 1000 ms (max) Operating temperature: -60-60 °C Lead time: 6-9 ## Deployment System 500 kg — KOSMOLAB Launch Services [separation-systems] https://newspacemarket.com/products/deployment-system-500-kg/ Mass: 17000 g Release time: 1000 ms (max) Operating temperature: -60-60 °C Lead time: 6-9 ## Alén Space Ground Station Kit (GS-Kit) — Alén Space [ground-stations] https://newspacemarket.com/products/ground-station-kit/ Frequency band: VHF @ uplink/downlink Frequency: 144-146 MHz @ uplink/downlink Frequency band: UHF @ uplink/downlink (variant 2) Frequency: 400-402 MHz @ uplink/downlink (variant 2) Frequency band: UHF @ uplink/downlink (variant 3) Frequency: 430-440 MHz @ uplink/downlink (variant 3) Frequency band: S @ downlink Frequency: 2250-2450 MHz @ downlink Frequency band: S @ downlink (variant 2) Frequency: 2100-2600 MHz @ downlink (variant 2) ## Simulsat 7A Multibeam Earth Station — ATCi [ground-stations] https://newspacemarket.com/products/atci-simulsat-7a/ Frequency band: C @ RX Frequency band: Ku @ RX (variant 2) Frequency: 3400000-4200000 MHz @ C-Band Frequency: 10700000-12750000 MHz @ Ku-Band Antenna diameter: 7 m @ Reflector Size (width) Antenna diameter: 12.8 m @ Reflector Size (length) Mass: 12448000 g @ Shipping Weight Mass: 3063000 g @ Max Weight (Off-Load Ship Crates) Envelope (L×W×H): 13240 (E) x 7020 (D) mm ## Simulsat 5B Multibeam Earth Station — ATCi [ground-stations] https://newspacemarket.com/products/atci-simulsat-5b/ Frequency band: C @ C-Band Frequency band: Ku @ Ku-Band Mass: 2858000 g @ Shipping Weight Mass: 1542000 g @ Max Weight (Off-Load Ship Crates) Envelope (L×W×H): 5.2m x 9.6m @ Reflector Size ## Fixed GEO Earth Stations — Kratos Defense & Security Solutions [ground-stations] https://newspacemarket.com/products/kratos-fixed-geo-earth-station-antennas/ Antenna diameter: 2.4 m @ S-band, min G/T: 10 @ S-band, min Frequency band: S Antenna diameter: 9.3 m @ S-band, max G/T: 26 @ S-band, max Frequency band: S @ (variant 2) Antenna diameter: 2.4 m @ S-band, min (variant 2) EIRP: 45 dBW @ S-band, min Frequency band: S @ (variant 3) Antenna diameter: 9.3 m @ S-band, max (variant 2) EIRP: 75 dBW @ S-band, max Frequency band: S @ (variant 4) Antenna diameter: 2.4 m @ C-band, min G/T: 15 @ C-band, min Frequency band: C @ (variant 5) Antenna diameter: 13.5 m @ C-band, max G/T: 35 @ C-band, max Frequency band: C @ (variant 6) Antenna diameter: 2.4 m @ C-band, min (variant 2) EIRP: 55 dBW @ C-band, min Frequency band: C @ (variant 7) Antenna diameter: 13.5 m @ C-band, max (variant 2) EIRP: 85 dBW @ C-band, max Frequency band: C @ (variant 8) Antenna diameter: 2.4 m @ X-band, min G/T: 20 @ X-band, min Frequency band: X @ (variant 9) Antenna diameter: 13.5 m @ X-band, max G/T: 40 @ X-band, max Frequency band: X @ (variant 10) Antenna diameter: 2.4 m @ X-band, min (variant 2) EIRP: 55 dBW @ X-band, min Frequency band: X @ (variant 11) Antenna diameter: 13.5 m @ X-band, max (variant 2) EIRP: 90 dBW @ X-band, max Frequency band: X @ (variant 12) Antenna diameter: 2.4 m @ Ku-band, min G/T: 25 @ Ku-band, min Frequency band: Ku @ (variant 13) Antenna diameter: 13.5 m @ Ku-band, max G/T: 43 @ Ku-band, max Frequency band: Ku @ (variant 14) Antenna diameter: 2.4 m @ Ku-band, min (variant 2) EIRP: 60 dBW @ Ku-band, min Frequency band: Ku @ (variant 15) Antenna diameter: 13.5 m @ Ku-band, max (variant 2) EIRP: 95 dBW @ Ku-band, max Frequency band: Ku @ (variant 16) Antenna diameter: 2.5 m @ K-band, min G/T: 25 @ K-band, min Frequency band: K @ (variant 17) Antenna diameter: 9.4 m @ K-band, max G/T: 39 @ K-band, max Frequency band: K @ (variant 18) Antenna diameter: 2.5 m @ K-band, min (variant 2) EIRP: 65 dBW @ K-band, min Frequency band: K @ (variant 19) Antenna diameter: 9.4 m @ K-band, max (variant 2) EIRP: 90 dBW @ K-band, max Frequency band: K @ (variant 20) Antenna diameter: 2.4 m @ Ka-band, min G/T: 27 @ Ka-band, min Frequency band: Ka @ (variant 21) Antenna diameter: 13.5 m @ Ka-band, max G/T: 43 @ Ka-band, max Frequency band: Ka @ (variant 22) Antenna diameter: 2.4 m @ Ka-band, min (variant 2) EIRP: 70 dBW @ Ka-band, min Frequency band: Ka @ (variant 23) Antenna diameter: 13.5 m @ Ka-band, max (variant 2) EIRP: 100 dBW @ Ka-band, max Frequency band: Ka @ (variant 24) ## Gaia™ Earth Observation Ground Stations (100, 200, 300, 400 Series) — Orbit Communication Systems [ground-stations] https://newspacemarket.com/products/gaia-100-earth-observation-ground-station/ Antenna diameter: 2.4 m @ Gaia 100 2.4 m Antenna diameter: 3.7 m @ Gaia 100 3.7 m Antenna diameter: 4.5 m @ Gaia 100 4.5 m Antenna diameter: 5.5 m @ Gaia 100 5.5 m Frequency band: S @ S-Band Transmit Frequency: 2025-2120 MHz @ S-Band Transmit Frequency band: S @ S-Band Receive Frequency: 2200-2300 MHz @ S-Band Receive Frequency band: X @ X-Band Receive Frequency: 7900-8400 MHz @ X-Band Receive Frequency band: X @ Optional X-Band Frequency: 7700-8500 MHz @ Optional X-Band Frequency band: S @ Optional S-Band Frequency: 2400-2500 MHz @ Optional S-Band Operating temperature: -25-55 °C Operating temperature: -40--40 °C @ optional Survival temperature: -40-70 °C Mass: 850000 g @ Gaia 100 2.4 m (Including Radome) Mass: 1500000 g @ Gaia 100 3.7 m (Including Radome) Mass: 1900000 g @ Gaia 100 4.5 m (Including Radome) Mass: 2500000 g @ Gaia 100 5.5 m (Including Radome) Envelope (L×W×H): Base Diameter: 4.0 m, Height: 3.6 m @ Gaia 100 2.4 m Radome Envelope (L×W×H): Base Diameter: 4.9 m, Height: 4.6 m @ Gaia 100 3.7 m Radome Envelope (L×W×H): Base Diameter: 6.4 m, Height: 5.6 m @ Gaia 100 4.5 m Radome Envelope (L×W×H): Base Diameter: 7.0 m, Height: 6.6 m @ Gaia 100 5.5 m Radome Supply voltage: 90-130 @ Power Input Supply voltage: 200-250 @ Power Input (variant 2) ## Optical Ground Station (OGS) — Swedish Space Corporation (SSC) [ground-stations] https://newspacemarket.com/products/ssc-optical-ground-station-services/ Data rate: 10000000 kbps @ TX+RX ## BADGER — AeroVironment (Tomahawk Robotics) [ground-stations] https://newspacemarket.com/products/aerovironment-badger/ Frequency band: L @ OPERATIONAL Frequency band: S @ OPERATIONAL (variant 2) Frequency band: C @ OPERATIONAL (variant 3) Operating temperature: -40 °C (min) Operating temperature: 50 °C (max) ## SSC Space Go — Swedish Space Corporation (SSC) [ground-stations] https://newspacemarket.com/products/ssc-go-leo-ground-station/ Antenna diameter: 4 m Frequency band: S @ uplink (TX) Frequency: 2020-2120 MHz @ uplink (TX) EIRP: 50 dBW @ uplink (TX) Frequency band: S @ downlink (RX) Frequency: 2200-2300 MHz @ downlink (RX) G/T: 12.8 @ downlink (RX) Frequency band: X @ downlink (RX) (variant 2) Frequency: 7900-8400 MHz @ downlink (RX) (variant 2) G/T: 26 @ downlink (RX) (variant 2) Frequency band: Ka @ downlink (RX) (variant 3) Frequency: 25500-27000 MHz @ downlink (RX) (variant 3) G/T: 30.5 @ downlink (RX) (variant 3) ## ESTELLA HUB — SpaceBridge Inc. [ground-stations] https://newspacemarket.com/products/estella-hub/ Frequency: 950-2400 MHz @ demodulator RX Data rate: 640000 kbps @ return capacity Data interface: Ethernet @ User Data Interface Data interface: Ethernet @ MGMT Interface Connector: 2x RJ45 (10Gbase-T) @ User Data Interface Connector: 4x RJ45 (100/1000baseT) @ MGMT Interface Connector: 5xSMA : 2x RX, 2x TX, 1x10MHz for LNB Connector: BNC @ 10 MHz Ref Clock Connector: BNC @ 1 PPS Input Mass: 8000 g Envelope (L×W×H): 19 “ x 2 RU x 26” @ WxHxD Supply voltage: 90-130 Supply voltage: 180-260 @ (variant 2) Power consumption: 200 W Operating temperature: 0-50 °C Survival temperature: -20-85 °C ## Satcube Ku — Satcube AB [ground-stations] https://newspacemarket.com/products/satcube-ku/ Mass: 8000 g Envelope (L×W×H): 470 x 300 x 55 mm Frequency band: Ku @ Tx Frequency band: Ku @ Rx EIRP: 46 dBW G/T: 9 Supply voltage: 24 Power consumption: 130 W Data rate: 20000000 kbps Operating temperature: -35 °C ## Satcube Secure — Satcube AB [ground-stations] https://newspacemarket.com/products/satcube-secure/ Mass: 9500 g Envelope (L×W×H): 470 x 320 x 75 mm Frequency band: Ku @ TX Frequency: 13750-14500 MHz @ TX Frequency band: Ku @ RX Frequency: 10950-12750 MHz @ RX EIRP: 46 dBW G/T: 9 Data rate: 20000 kbps @ Up to, via HTS Supply voltage: 24 Power consumption: 130 W Supply voltage: 100-240 @ AC/DC Operating temperature: -35-50 °C ## Satcube Motion — Satcube AB [ground-stations] https://newspacemarket.com/products/satcube-motion/ Mass: 15000 g Envelope (L×W×H): 500 x 500 x 250 mm Frequency: 13750 MHz (min) @ Tx Frequency: 14500 MHz (max) @ Tx Frequency band: Ku @ Tx Frequency: 10950 MHz (min) @ Rx Frequency: 12750 MHz (max) @ Rx Frequency band: Ku @ Rx EIRP: 47.5 dBW G/T: 9 Data rate: 20000 kbps (max) @ Up to 20/20 Mbps via HTS Supply voltage: 11 (min) Supply voltage: 50 (max) Power consumption: 150 W Operating temperature: -20 °C (min) Operating temperature: 50 °C (max) Data interface: Ethernet @ 2x RJ45 ## Skynopy Ground Station Services — Skynopy [ground-stations] https://newspacemarket.com/products/skynopy-ground-station-network/ Frequency band: S @ TX/RX Frequency band: X @ TX/RX (variant 2) Frequency band: Ka @ TX/RX (variant 3) ## Viasat Multi-Mission Terminal (MMT) — Viasat, Inc. [ground-stations] https://newspacemarket.com/products/viasat-multi-mission-terminal-mmt-3363/ Antenna diameter: 0.006 m @ circular aperture Supply voltage: 24 (nominal) @ Shore Power DC Supply voltage: 305 (max) @ Shore Power AC Power consumption: 200 W (max) @ maximum terminal consumption (depends on RF configuration) Mass: 31750 g (max) @ 1 IATA Case Frequency band: X @ RX Frequency: 7250-7750 MHz @ RX Frequency Band X-BAND Frequency band: X @ TX Frequency: 7900-8400 MHz @ TX Frequency Band X-BAND Frequency band: Ku @ RX (variant 2) Frequency: 10950-12750 MHz @ RX Frequency Band KU-BAND Frequency band: Ku @ TX (variant 2) Frequency: 13750-14500 MHz @ TX Frequency Band KU-BAND Frequency band: Ka @ RX (variant 3) Frequency: 20200-21200 MHz @ RX Frequency Band MIL-KA BAND Frequency band: Ka @ TX (variant 3) Frequency: 30000-31000 MHz @ TX Frequency Band MIL-KA BAND Frequency band: Ka @ RX (variant 4) Frequency: 17700-20200 MHz @ RX Frequency Band VIASAT HIGH-CAPACITY KA Frequency band: Ka @ TX (variant 4) Frequency: 27500-30000 MHz @ TX Frequency Band VIASAT HIGH-CAPACITY KA ## HIGH POWER GaN DBS SSPA 1kW/2kW/3.5kW Outdoor/Indoor — TTI Norte [ground-stations] https://newspacemarket.com/products/high-power-gan-dbs-sspa-1kw-2kw-3-5kw-outdoor-indoor/ Envelope (L×W×H): 1370 x 1070 x 1000 mm Envelope (L×W×H): 1370 x 2000 x 1000 mm @ (variant 2) Frequency band: C @ TX Frequency: 5850000-6425000 MHz EIRP: 31.2 dBW @ PSAT (typical) EIRP: 31.8 dBW @ PSAT (typical) (variant 2) EIRP: 34.3 dBW @ PSAT (typical) (variant 3) EIRP: 36.8 dBW @ PSAT (typical) (variant 4) EIRP: 29 dBW @ PLINEAR* EIRP: 30.8 dBW @ PLINEAR* (variant 2) EIRP: 33.3 dBW @ PLINEAR* (variant 3) EIRP: 35.8 dBW @ PLINEAR* (variant 4) Supply voltage: 90-264 @ Input Power consumption: 4600 W (max) @ PSAT Data interface: Ethernet @ M&C outdoor Data interface: Ethernet @ M&C indoor Data interface: RS-485 @ Remote control Data interface: Ethernet @ Remote control (variant 2) Data interface: other @ Remote control (variant 3) Data interface: other @ Remote control (variant 4) Operating temperature: -30-55 °C @ outdoor Operating temperature: 0-50 °C @ indoor Survival temperature: -40-85 °C ## Solar Array Simulator (SAS) — Tiger Innovations, Inc. [solar-panels] https://newspacemarket.com/products/tiger-innovations-solar-array-simulator/ Form factor: 4U, 19” rack mounted Form factor: 6U, 19” rack mounted @ (variant 2) Data interface: Ethernet ## 1U Solar Panel — Aphelion Orbitals [solar-panels] https://newspacemarket.com/products/1u-solar-panel-3474/ Form factor: 1U Cell efficiency: 30.5 Supply voltage: 22 (nominal) Design lifetime: 2 years @ minimum in LEO Connector: 4-pin Hirose 1.25mm @ power Connector: 8-pin Hirose 1.25mm @ data Operating temperature: -40 °C (min) Operating temperature: 125 °C (max) ## SEPTA36 Solar Array Drive Mechanism — Beyond Gravity (ex-RUAG Space) [sadm] https://newspacemarket.com/products/beyond-gravity-septa36-sadm/ Design lifetime: 15 years @ in orbit Supply voltage: 2.5 (min) @ Operating Supply voltage: 12 (max) @ Operating Supply voltage: 5 (nominal) @ Operating Envelope (L×W×H): 162.5 mm (Length from front of flange) (SEPTA36-1) @ (variant 2) Envelope (L×W×H): 212.5 mm (Length from front of flange) (SEPTA36-2) @ (variant 3) Envelope (L×W×H): 262.5 mm (Length from front of flange) (SEPTA36-3) @ (variant 4) Envelope (L×W×H): 202 mm (Length Overall) (SEPTA36-1) @ (variant 5) Envelope (L×W×H): 252.0 mm (Length Overall) (SEPTA36-2) @ (variant 6) Envelope (L×W×H): 302 mm (Length Overall) (SEPTA36-3) @ (variant 7) Mass: 4000 g @ excl. customer-specific harness (SEPTA36-1) Mass: 4600 g @ excl. customer-specific harness (SEPTA36-2) Mass: 5400 g @ excl. customer-specific harness (SEPTA36-3) Survival temperature: 10 °C (min) @ Ground Storage (S/C conductive interface) Survival temperature: 30 °C (max) @ Ground Storage (S/C conductive interface) Survival temperature: 10 °C (min) @ Ground Storage (S/C radiative interface) Survival temperature: 30 °C (max) @ Ground Storage (S/C radiative interface) Survival temperature: 90 °C (max) @ Hot Non-Operational (Survival) (S/C conductive interface) Survival temperature: 65 °C (max) @ Hot Non-Operational (Survival) (S/C radiative interface) Operating temperature: 70 °C (max) @ Hot Operational (S/C conductive interface) Operating temperature: 60 °C (max) @ Hot Operational (S/C radiative interface) Operating temperature: -35 °C (min) @ Cold Operational (S/C conductive interface) Operating temperature: -30 °C (min) @ Cold Operational (S/C radiative interface) Operating temperature: -40 °C (min) @ Cold start-up limit (S/C conductive interface) Operating temperature: -30 °C (min) @ Cold start-up limit (S/C radiative interface) Survival temperature: -40 °C (min) @ Cold Non-Operational (Survival) (S/C conductive interface) Survival temperature: -30 °C (min) @ Cold Non-Operational (Survival) (S/C radiative interface) Wheel speed: 1 (max) Design lifetime: 15 years Max torque: 7000 mN·m @ Unpowered holding torque Max torque: 55000 mN·m (max) @ Powered Holding Torque Max torque: 55000 mN·m @ gt, Delivered Output Torque @ 200 mA Max torque: 55000 mN·m @ gt, Delivered Output Torque @ 300 mA Slip-ring channels: 30 @ SEPTA36-1 Slip-ring channels: 60 @ SEPTA36-2 Slip-ring channels: 90 @ SEPTA36-3 Supply voltage: 120 (max) @ across tracks Supply voltage: 2.5 (min) @ Position Measurement Operating Voltage Supply voltage: 12 (max) @ Position Measurement Operating Voltage Envelope (L×W×H): Max. Outer Diameter mounting flange 144 mm Envelope (L×W×H): Length from front of flange 162.5 mm @ SEPTA36-1 Envelope (L×W×H): Length from front of flange 212.5 mm @ SEPTA36-2 Envelope (L×W×H): Length from front of flange 262.5 mm @ SEPTA36-3 Envelope (L×W×H): Length Overall 202 mm @ SEPTA36-1 (variant 2) Envelope (L×W×H): Length Overall 252.0 mm @ SEPTA36-2 (variant 2) Envelope (L×W×H): Length Overall 302 mm @ SEPTA36-3 (variant 2) Mass: 4000 g @ SEPTA36-1 Mass: 4600 g @ SEPTA36-2 Mass: 5400 g @ SEPTA36-3 Survival temperature: 90 °C (max) @ S/C conductive interface Hot Non-Operational Survival temperature: 65 °C (max) @ S/C radiative interface Hot Non-Operational Operating temperature: 70 °C (max) @ S/C conductive interface Hot Operational Operating temperature: 60 °C (max) @ S/C radiative interface Hot Operational Operating temperature: -35 °C (min) @ S/C conductive interface Cold Operational Operating temperature: -30 °C (min) @ S/C radiative interface Cold Operational Survival temperature: -40 °C (min) @ S/C conductive interface Cold Non-Operational Survival temperature: -30 °C (min) @ S/C radiative interface Cold Non-Operational ## SEPTA36G Solar Array Drive Mechanism — Beyond Gravity (ex-RUAG Space) [sadm] https://newspacemarket.com/products/beyond-gravity-septa36g-sadm/ Wheel speed: 1 (max) Max torque: 7000 mN·m @ Unpowered holding torque Max torque: 55000 mN·m (max) @ Powered Holding Torque Max torque: 55000 mN·m (min) @ Delivered Output Torque @ 200 mA Max torque: 55000 mN·m (min) @ Delivered Output Torque @ 300 mA Slip-ring channels: 30 @ SEPTA36G-1, Number of tracks (all tracks identical and usable for power or signal transfer) Slip-ring channels: 60 @ SEPTA36G-2, Number of tracks (all tracks identical and usable for power or signal transfer) Slip-ring channels: 90 @ SEPTA36G-3, Number of tracks (all tracks identical and usable for power or signal transfer) Power transfer: 9000 W @ SEPTA36G-1, Total Power transfer Power transfer: 18000 W @ SEPTA36G-2, Total Power transfer Power transfer: 27000 W @ SEPTA36G-3, Total Power transfer Supply voltage: 120 @ Max. voltage across tracks Supply voltage: 2.5 @ Position Measurement, Operating Voltage Supply voltage: 12 @ Position Measurement, Operating Voltage (variant 2) Mass: 4200 g @ SEPTA36G-1 (excl. customer-specific harness) Mass: 5200 g @ SEPTA36G-2 (excl. customer-specific harness) Mass: 6200 g @ SEPTA36G-3 (excl. customer-specific harness) Operating temperature: 80 °C @ Hot Operational, S/C conductive interface Operating temperature: 60 °C @ Hot Operational, S/C radiative interface Operating temperature: -35 °C @ Cold Operational, S/C conductive interface Operating temperature: -30 °C @ Cold Operational, S/C radiative interface Operating temperature: -40 °C @ Cold start-up limit, S/C conductive interface Operating temperature: -30 °C @ Cold start-up limit, S/C radiative interface Mass: 4200 g @ SEPTA36G-1, excl. customer-specific harness Mass: 5200 g @ SEPTA36G-2, excl. customer-specific harness Mass: 6200 g @ SEPTA36G-3, excl. customer-specific harness Envelope (L×W×H): 144 mm (Max. Outer Diameter mounting flange), 217 mm (Length Overall) @ SEPTA36G-1 Envelope (L×W×H): 144 mm (Max. Outer Diameter mounting flange), 277.0 mm (Length Overall) @ SEPTA36G-2 Envelope (L×W×H): 144 mm (Max. Outer Diameter mounting flange), 337 mm (Length Overall) @ SEPTA36G-3 Operating temperature: 80 °C (max) @ Hot Operational, S/C conductive interface Operating temperature: 60 °C (max) @ Hot Operational, S/C radiative interface Operating temperature: -35 °C (min) @ Cold Operational, S/C conductive interface Operating temperature: -30 °C (min) @ Cold Operational, S/C radiative interface Operating temperature: -40 °C (min) @ Cold start-up limit, S/C conductive interface Operating temperature: -30 °C (min) @ Cold start-up limit, S/C radiative interface Design lifetime: 15 years @ in orbit ## SEPTA42 Solar Array Drive Mechanism — Beyond Gravity (ex-RUAG Space) [sadm] https://newspacemarket.com/products/beyond-gravity-septa42-sadm/ Design lifetime: 12 years Supply voltage: 25 (max) @ continuous Supply voltage: 70 (max) @ peak Survival temperature: 90 °C (max) @ Hot Non-Operational (Survival) S/C conductive interface Survival temperature: 110 °C (max) @ Hot Non-Operational (Survival) S/A conductive interface Survival temperature: 90 °C (max) @ Hot Non-Operational (Survival) S/C radiative interface Survival temperature: -40 °C (min) @ Cold Non-Operational (Survival) S/C conductive interface Survival temperature: -70 °C (min) @ Cold Non-Operational (Survival) S/A conductive interface Survival temperature: -40 °C (min) @ Cold Non-Operational (Survival) S/C radiative interface Operating temperature: 70 °C (max) @ Hot Operational S/C conductive interface Operating temperature: 100 °C (max) @ Hot Operational S/A conductive interface Operating temperature: 70 °C (max) @ Hot Operational S/C radiative interface Operating temperature: -30 °C (min) @ Cold Operational S/C conductive interface Operating temperature: -50 °C (min) @ Cold Operational S/A conductive interface Operating temperature: -30 °C (min) @ Cold Operational S/C radiative interface Wheel speed: 1 @ Maximum output Mass: 4900 g @ excl. margin & customer-specific harness ## Ra — Spacemanic s.r.o. [solar-panels] https://newspacemarket.com/products/spacemanic-ra-solar-panels/ Flight heritage: 10+ missions (e.g. LASARsat, CroCube, GRBBeta and external customers) Operating temperature: -40 °C (min) Operating temperature: 125 °C (max) Cell efficiency: 30 (min) @ BOL Cell efficiency: 25.7 @ EOL Form factor: 1U Output power (BOL): 2.48 W @ 1U Mass: 30 g @ 1U Form factor: 2U @ (variant 2) Output power (BOL): 4.96 W @ 2U Mass: 70 g @ 2U Form factor: 3U @ (variant 3) Output power (BOL): 8.68 W @ 3U Mass: 110 g @ 3U Form factor: 6U body-mounted @ (variant 4) Deployable: no @ 6U body-mounted Output power (BOL): 17.36 W @ 6U body-mounted Mass: 230 g @ 6U body-mounted Form factor: 6U deployable @ (variant 5) Deployable: yes @ 6U deployable Output power (BOL): 19.84 W @ 6U deployable Mass: 230 g @ 6U deployable Form factor: 8U body-mounted @ (variant 6) Deployable: no @ 8U body-mounted Output power (BOL): 22.32 W @ 8U body-mounted Mass: 300 g @ 8U body-mounted Form factor: 8U deployable @ (variant 7) Deployable: yes @ 8U deployable Output power (BOL): 24.8 W @ 8U deployable Mass: 300 g @ 8U deployable Connector: MOLEX PicoBlade connector (53261-0471) Supply voltage: 0 (min) Supply voltage: 20 (max) ## NanoPower DSP — GomSpace [solar-panels] https://newspacemarket.com/products/nanopower-dsp/ Output power (BOL): 1.2 W @ in LEO Cell efficiency: 28 (min) Cell efficiency: 30 (max) Form factor: 3U or 6U side Deployable: two deployable panels and one body mounted panel Operating temperature: -40 °C (min) @ internal temperature sensor Operating temperature: 85 °C (max) @ internal temperature sensor Operating temperature: -55 °C (min) @ external temperature sensor Operating temperature: -98.2 °C (max) @ external temperature sensor Data interface: I2C Data interface: I2C @ (variant 2) Data interface: I2C @ (variant 3) Data interface: I2C @ (variant 4) Supply voltage: 3.3 (nominal) @ GSSB I2C level Supply voltage: 3 (nominal) @ GSSB_VCC ## NanoPower TSP-45W — GomSpace [solar-panels] https://newspacemarket.com/products/nanopower-tsp-45w/ Form factor: 2x3U Deployable: yes Mass: 750 g @ Total mass Mass: 650 g @ Deployed mass (i.e., the array) Envelope (L×W×H): 330 mm x 208 mm x 9 mm @ Stowed volume Envelope (L×W×H): 930 mm (from rail) @ Deployed length Output power (BOL): 45 W @ up to, per array Cell efficiency: 28 @ gt Data interface: I2C Data interface: other @ Pads for release detection Connector: Harwin Gecko ## XTE+ GEO Solar Cell — Spectrolab [solar-panels] https://newspacemarket.com/products/spectrolab-xte-plus-geo/ Mass: 50-84 g Flight heritage: 25+ years of heritage 3J devices Cell efficiency: 32.6 (nominal) @ BOL Design lifetime: 15 years @ GEO ## XTE+ LEO Solar Cell — Spectrolab [solar-panels] https://newspacemarket.com/products/spectrolab-xte-plus-leo/ Cell efficiency: 32.2 @ BOL Cell efficiency: 30.6 @ EOL, 1E14 1MeV electron Supply voltage: 2.807 Supply voltage: 2.706 @ (variant 2) Mass: 50-84 g ## XTE-SF Solar Cell — Spectrolab [solar-panels] https://newspacemarket.com/products/spectrolab-xte-sf/ Mass: 84-130 g Cell efficiency: 32.2 @ BOL Cell efficiency: 27.9 @ EOL, 1E15 1MeV electron Flight heritage: 20+ years of heritage 3J devices ## XTE-HF Solar Cell — Spectrolab [solar-panels] https://newspacemarket.com/products/spectrolab-xte-hf/ Cell efficiency: 32.1 @ BOL Mass: 50-84 g ## XTE-LILT Solar Cell — Spectrolab [solar-panels] https://newspacemarket.com/products/spectrolab-xte-lilt/ Cell efficiency: 31.6 @ BOL 1 AU Cell efficiency: 37 @ BOL 5.5 AU Flight heritage: 20+ years of heritage 3J devices ## XTJ Prime Solar Cell — Spectrolab [solar-panels] https://newspacemarket.com/products/spectrolab-xtj-prime/ Cell efficiency: 30.7 @ BOL Cell efficiency: 26.7 @ EOL, 1E15 1MeV electron Form factor: 26–84 cm² Flight heritage: Hundreds of satellites and spacecraft ## 32% Efficiency Triple Junction GaAs Solar Cell — CAVU Aerospace [solar-panels] https://newspacemarket.com/products/sc-3ga-4-solar-cell-assembly/ Supply voltage: 2.666 Output power (BOL): 1.331 W Cell efficiency: 32 Envelope (L×W×H): (80.0±0.1)×(40.0±0.1)×(0.155±0.020) Mass: 2.4 g (nominal) ## Redwire HiPASS – High-Power Rigid Array Solution for SmallSats — Redwire Corporation [solar-panels] https://newspacemarket.com/products/redwire-hipass-solar-array/ Mass: 17000 g Form factor: Deployed wing Deployable: yes Envelope (L×W×H): 76 x 137 x 19 CM @ Stowed Wing Dimensions Envelope (L×W×H): 137 x 365 x 20 CM @ Deployed Wing Dimensions Flight heritage: 10 flight HiPASS wings (for use on multiple U.S. Government missions) are planned for delivery in 2022. Export status: This product is controlled for export from the United States. Contact Redwire for details. ## TJ 3G30-Advanced Space Solar Cell (4×8) — AZUR SPACE [solar-panels] https://newspacemarket.com/products/azurspace-3g30-advanced-4x8/ Envelope (L×W×H): 40.00 (± 0.1) x 80.00 (± 0.1) Mass: 2.6 g Output power (BOL): 1.214 W @ BOL, 1367 W/m2 Cell efficiency: 29.5 @ BOL, 1367 W/m2 Cell efficiency: 29.8 @ BOL, 1353 W/m2 Flight heritage: on-orbit TRL-9 level heritage ## TJ 3G30-Advanced Space Solar Cell (8×8) — AZUR SPACE [solar-panels] https://newspacemarket.com/products/azurspace-3g30-advanced-8x8/ Cell efficiency: 30 @ BOL Mass: 5.2 g @ bare cell (average) Mass: 7.1 g @ assembly (average) Envelope (L×W×H): 80.00 (± 0.1) x 80.00 (± 0.1) @ bare cell Envelope (L×W×H): 80.15 (± 0.05) x 80.15 (± 0.05) @ assembly (SCA / CIC) Cell efficiency: 29.3 @ BOL, Cell, AM0 WRC, 1367 W/m2, T = 28°C Cell efficiency: 29 @ BOL, CIC, AM0 WRC, 1367 W/m2, T = 28°C Cell efficiency: 29.6 @ BOL, Cell, AM0 WRC, 1353 W/m2, T = 28°C Cell efficiency: 29.3 @ BOL, CIC, AM0 WRC, 1353 W/m2, T = 28°C Flight heritage: TRL-9 level heritage ## TJ 3G30-Advanced Space Solar Cell (6×12) — AZUR SPACE [solar-panels] https://newspacemarket.com/products/azurspace-3g30-advanced-6x12/ Cell efficiency: 28.8 @ BOL (1367 W/m2) Envelope (L×W×H): 60.7 (± 0.1) x 124.5 (± 0.1) Mass: 8.8 g Flight heritage: on-orbit TRL-9 level heritage Connector: In-plane, silver coated Kovar, 8.09 x 12.91 x 0.025 mm ## TJ 3G30-Advanced Space Solar Cell (HP) — AZUR SPACE [solar-panels] https://newspacemarket.com/products/azurspace-3g30-advanced-hp/ Cell efficiency: 30 @ beginning-of-life (BOL) Envelope (L×W×H): 145.90 (± 0.1) x 60.69 (± 0.1) @ Bare Cell Outer Dimensions Envelope (L×W×H): 146.10 (± 0.1) x 60.89 (± 0.1) @ Assembly Outer Dimensions Mass: 10.4 g @ Bare Cell Average Weight Mass: 13.1 g @ Assembly Average Weight Cell efficiency: 29 @ BOL Cell, 1367 W/m2 Cell efficiency: 28.7 @ BOL CIC, 1367 W/m2 Cell efficiency: 29.3 @ BOL Cell, 1353 W/m2 Cell efficiency: 29 @ BOL CIC, 1353 W/m2 Flight heritage: in-orbit TRL-9 level heritage ## QJ 4G32-Advanced Space Solar Cell (4×8) — AZUR SPACE [solar-panels] https://newspacemarket.com/products/azurspace-4g32-advanced-4x8/ Mass: 4.2 g @ Assembly Envelope (L×W×H): 40.26 (± 0.1) x 80.26 (± 0.1) @ Assembly Cell efficiency: 30.9 @ BOL, 1367 W/m2, 25°C, CIC Cell efficiency: 31.2 @ BOL, 1353 W/m2, 25°C, CIC Flight heritage: in-orbit TRL-9 level Envelope (L×W×H): total device thickness of 330 µm @ Assembly (variant 2) ## QJ 4G32-Advanced Space Solar Cell (8×8) — AZUR SPACE [solar-panels] https://newspacemarket.com/products/azurspace-4g32-advanced-8x8/ Cell efficiency: 31.1 @ BOL, 1367 W/m2 Mass: 6.5 g (typical) Envelope (L×W×H): 80.00 (± 0.1) x 80.00 (± 0.1) Flight heritage: TRL-9 level heritage ## QJ 4G32-Advanced Space Solar Cell (HP) — AZUR SPACE [solar-panels] https://newspacemarket.com/products/azurspace-4g32-advanced-hp/ Cell efficiency: 32 Envelope (L×W×H): 148.06 (± 0.1) x 60.56 (± 0.1) mm @ Bare Cell Envelope (L×W×H): 148.26 (± 0.1) x 60.76 (± 0.1) mm @ Assembly (SCA / CIC) Mass: 10.4 g @ Bare Cell Mass: 13.6 g @ Assembly (SCA / CIC) Flight heritage: in-orbit TRL-9 level heritage ## Flexible Thermal Straps — Lidax [thermal] https://newspacemarket.com/products/lidax-copper-flexible-thermal-straps/ Mass: 60 g (min) Mass: 880 g (max) Thermal conductance: 0.03 (min) @ ambient conditions Thermal conductance: 0.6 (max) @ ambient conditions Operating temperature: -110 °C (min) Operating temperature: 70 °C (max) ## Polyimide (Kapton®) Thermofoil™ Heaters — Minco Products, Inc [thermal] https://newspacemarket.com/products/polyimide-kapton-thermofoil-heaters/ Mass: 0.04 g @ typically Envelope (L×W×H): 0.25 @ thick over the element Operating temperature: -200-200 °C @ Polyimide/FEP Operating temperature: -200-150 °C @ Polyimide/WA Operating temperature: -200-150 °C @ Polyimide/ULA Operating temperature: -200-260 °C @ All-Polyimide (AP) ## All-Polyimide (KAPTON®) Heaters — Minco Products, Inc [thermal] https://newspacemarket.com/products/all-polyimide-kapton-heaters/ Operating temperature: -200-260 °C Envelope (L×W×H): 560 mm × 1145 mm Mass: 0.04 g (typical) ## Thermal-Clear TM Transparent Heaters — Minco Products, Inc [thermal] https://newspacemarket.com/products/thermal-clear-tm-transparent-heaters/ Flight heritage: Transparent @ Compatible Heater Technologies ## Mica THERMOFOIL TM Heaters — Minco Products, Inc [thermal] https://newspacemarket.com/products/mica-thermofoil-tm-heaters/ Operating temperature: -150 °C (min) Operating temperature: 600 °C (max) Envelope (L×W×H): 560 mm × 1168 mm ## AstraWrap™ HT — Aerospace Fabrication and Materials, LLC [thermal] https://newspacemarket.com/products/astrawrap-ht/ Layers (MLI): 10 @ AW001 & AW002 Mass: 181 g @ AW001 & AW002, 10 Layers Operating temperature: -269 °C (min) @ AW001 & AW002, 10 Layers Operating temperature: 149 °C (max) @ AW001 & AW002, 10 Layers Emissivity: 0.0046 @ AW001 & AW002, 10 Layers Layers (MLI): 15 @ AW001 & AW002 (variant 2) Mass: 272 g @ AW001 & AW002, 15 Layers Operating temperature: -269 °C (min) @ AW001 & AW002, 15 Layers Operating temperature: 149 °C (max) @ AW001 & AW002, 15 Layers Emissivity: 0.0044 @ AW001 & AW002, 15 Layers Layers (MLI): 20 @ AW001 & AW002 (variant 3) Mass: 362 g @ AW001 & AW002, 20 Layers Operating temperature: -269 °C (min) @ AW001 & AW002, 20 Layers Operating temperature: 149 °C (max) @ AW001 & AW002, 20 Layers Emissivity: 0.0042 @ AW001 & AW002, 20 Layers Layers (MLI): 10 @ AW003 & AW004 Mass: 110 g @ AW003 & AW004, 10 Layers Operating temperature: -269 °C (min) @ AW003 & AW004, 10 Layers Operating temperature: 14.9 °C (max) @ AW003 & AW004, 10 Layers Emissivity: 0.0099 @ AW003 & AW004, 10 Layers Layers (MLI): 15 @ AW003 & AW004 (variant 2) Mass: 165 g @ AW003 & AW004, 15 Layers Operating temperature: -269 °C (min) @ AW003 & AW004, 15 Layers Operating temperature: 14.9 °C (max) @ AW003 & AW004, 15 Layers Emissivity: 0.0066 @ AW003 & AW004, 15 Layers Layers (MLI): 20 @ AW003 & AW004 (variant 3) Mass: 220 g @ AW003 & AW004, 20 Layers Operating temperature: -269 °C (min) @ AW003 & AW004, 20 Layers Operating temperature: 14.9 °C (max) @ AW003 & AW004, 20 Layers Emissivity: 0.0055 @ AW003 & AW004, 20 Layers ## Constant Conductance Heat Pipes (CCHPs) — ACT (Advanced Cooling Technologies) [thermal] https://newspacemarket.com/products/act-cchp/ Radiation tolerance (TID): 600 krad @ Total Ionizing Dose (TID) Envelope (L×W×H): Up to 20' (6.1 m) Length Envelope (L×W×H): 0.25" to 1.0" (0.64 cm to 2.5 cm) Diameter @ (variant 2) Flight heritage: Flight-proven in hundreds of missions ## High-Temperature Heat Pipes — ACT (Advanced Cooling Technologies) [thermal] https://newspacemarket.com/products/act-high-temp-heat-pipes/ Export status: ITAR & EAR Compliant Operating temperature: -46.3 °C (min) Operating temperature: 1100 °C (max) Envelope (L×W×H): 0.5 (min) @ Typical diameter Envelope (L×W×H): 4 (max) @ Typical diameter Envelope (L×W×H): 5 (max) @ Heat Transport Length ## Cryocoolers — Northrop Grumman Space Systems [thermal] https://newspacemarket.com/products/ngc-hec-cryocooler/ Flight heritage: NASA’s James Webb Space Telescope Export status: 50 (max) Design lifetime: 10 years Power consumption: 180 W (max) Operating temperature: -40 °C (min) Operating temperature: 70 °C (max) Mass: 4500 g (max) @ single stage Mass: 3800 g (max) @ electronics ## Conductive Glass Fabric High-Temperature Vacuum Insulation — Beyond Gravity (ex-RUAG Space) [thermal] https://newspacemarket.com/products/beyond-gravity-conductive-glass-fabric-insulation/ Envelope (L×W×H): 108 x 108 mm Mass: 429 g Absorptivity: 0.08 Emissivity: 0.93 ## AstraWrap™ Thermal Insulation Space Wrap — Aerospace Fabrication and Materials, LLC [thermal] https://newspacemarket.com/products/astrawrap-thermal-insulation-space-wrap/ Mass: 181 g Layers (MLI): 10 Operating temperature: -269 °C (min) Operating temperature: 149 °C (max) Emissivity: 0.0046 ## Xiomas Wide Area Imager (WAI) — Xiomas Technologies [cameras] https://newspacemarket.com/products/xiomas-wide-area-imager-wai/ Swath width: 24.14 km @ design altitude of 40,000 feet ASL Ground sample distance: 3.5 m @ Thermal, @ 40,000 ASL Ground sample distance: 0.46 m @ VNIR, @ 10,000 AGL Ground sample distance: 0.66 m @ LWIR mosaics Spectral bands: 2 @ Thermal Spectral bands: 3 @ VNIR ## C-RED One SWIR Camera — First Light Imaging [cameras] https://newspacemarket.com/products/first-light-imaging-c-red-one/ Spectral bands: 3 @ J, H and K bands Mass: 19400 g Data interface: Camera Link Data interface: Ethernet @ (variant 2) Operating temperature: 0 °C @ environment Survival temperature: -10 °C Supply voltage: 24 @ camera Supply voltage: 100 @ power supply Power consumption: 700 W @ max Power consumption: 300 W @ cooling (average) Power consumption: 70 W @ keep sensor cold (average) ## SOC-760 VNIR-SWIR Hyperspectral Imager — Surface Optics Corporation [cameras] https://newspacemarket.com/products/surface-optics-soc-760-vnir-swir-hyperspectral-imager/ Sensor resolution: 640 pixels vertical, up to 2048 pixels horizontal @ Spatial Resolution Sensor resolution: 640 @ Camera Resolution Spectral bands: 650 Envelope (L×W×H): 20.5” x 8.5” x 6.5” Power consumption: 50 W @ nominal Supply voltage: 115 VAC @ input Data interface: USB ## 5MP Space Camera — Voyager Technologies [cameras] https://newspacemarket.com/products/4k-space-camera/ Sensor resolution: 2560 (H) x 2160 (V) px Envelope (L×W×H): 10.7 cm L x 8.4 cm W x 23.8 cm H @ with baffle Mass: 1000 g (max) Power consumption: 4 W (max) Supply voltage: 5 (nominal) Data interface: SpaceWire @ at 80 Mbps Design lifetime: 10 years @ LEO/GEO Radiation tolerance (TID): 30 krad @ EEE parts Radiation tolerance (TID): 100 krad @ Optional ## Aurora SWIR Line-Scan Camera — Thoth Technology [cameras] https://newspacemarket.com/products/thoth-aurora-linescan-camera/ Mass: 285 g (max) @ all formats Mass: 280 g @ for Aurora 1000XY-A to 1000XY-F Mass: 281 g @ for Aurora 1000XY-G Envelope (L×W×H): 45 mm x 50 mm x 80 mm @ for Aurora 1000XY-A to 1000XY-E Envelope (L×W×H): 45 mm x 50 mm x 110 mm @ Aurora 1000XY-F Envelope (L×W×H): 45 mm x 50 mm x 110 mm @ Aurora 1000XY-G Operating temperature: -20-40 °C Survival temperature: -35-65 °C Supply voltage: 3.2-4.6 @ nominally Power consumption: 1.2 W @ continuous input feed, derived from 3.2V DC and 375mA (typical) Power consumption: 2.645 W (max) @ continuous input feed, derived from 4.6V DC and 575mA (max) Power consumption: 4.8 W @ in-rush, derived from 3.2V DC and 1500mA Power consumption: 7.5 W @ in-rush, derived from 5.0V DC and 1500mA Data interface: RS-232 @ Prime and redundant serial interfaces Data interface: RS-232 @ asynchronous serial ports Ground sample distance: 750 m @ for Aurora 1000XY-D; objective distance 600km Ground sample distance: 600 m @ for Aurora 1000XY-E; objective distance 600km Ground sample distance: 500 m @ for Aurora 1000XY-F; objective distance 600km Ground sample distance: 400 m @ for Aurora 1000XY-G; objective distance 600km Ground sample distance: 0.67 m @ for Aurora 1000XY-G; altitude 1km Swath width: 512 km @ for Aurora 1000XY-A; objective distance 600km Swath width: 384 km @ for Aurora 1000XY-B; objective distance 600km Swath width: 256 km @ for Aurora 1000XY-C; objective distance 600km Swath width: 192 km @ for Aurora 1000XY-D; objective distance 600km Swath width: 153.6 km @ for Aurora 1000XY-E; objective distance 600km Swath width: 128 km @ for Aurora 1000XY-F; objective distance 600km Swath width: 102.4 km @ for Aurora 1000XY-G; objective distance 600km Focal length: 15 @ for Aurora 1000XY-A Focal length: 20 @ for Aurora 1000XY-B Focal length: 30 @ for Aurora 1000XY-C Focal length: 40 @ for Aurora 1000XY-D Focal length: 50 @ for Aurora 1000XY-E Focal length: 60 @ for Aurora 1000XY-F Focal length: 75 @ for Aurora 1000XY-G Spectral bands: 256 channels Sensor resolution: 256 pixel Connector: Hose DF11 type connector with 6 pins ## KSOI-90 Optical Imager (90 mm) — Kairo Space [cameras] https://newspacemarket.com/products/kairo-space-ksoi-90/ Ground sample distance: 5 m @ PAN @600 km Swath width: 81.9 km @ @600 km Mass: 1400 g Envelope (L×W×H): Ø101 x 243 mm Supply voltage: 5 (nominal) Power consumption: 8 W @ Peak Data interface: RS-422 Data interface: RS-485 @ (variant 2) Data interface: CAN @ (variant 3) Data interface: UART @ default Data interface: CAN @ control Data interface: RS-422 @ control (variant 2) Data interface: RS-232 @ control (variant 3) Radiation tolerance (TID): 25 krad Design lifetime: 3 years Flight heritage: TRL 8 Focal length: 500 Sensor resolution: 4096 × 3072 pixels Spectral bands: 6 @ Up to 6 (RGB, Red Edge, NIR, PAN) ## DragonEye — Dragonfly Aerospace [cameras] https://newspacemarket.com/products/dragonfly-dragoneye/ Ground sample distance: 1.4 m @ PAN at 500 km Ground sample distance: 2.8 m @ MS binned at 500 km Swath width: 22.2 km @ at 500 km Mass: 18000 g Spectral bands: 11 @ 10x MS plus 1x PAN Envelope (L×W×H): 320 mm (D) x 930 mm (L) @ plus electronics Data interface: other @ Multi-gigabit transceiver Data interface: LVDS Data interface: RS422 @ TMTC Interface Power consumption: 45 W (max) @ Imaging mode Power consumption: 25 W (max) @ Readout mode Supply voltage: 28 (nominal) @ DC Operating temperature: 10 °C (min) Operating temperature: 30 °C (max) Survival temperature: -20 °C (min) Survival temperature: 55 °C (max) Flight heritage: 2 DragonEye imagers launched in 2023 ## HRVI-6HD 2nd Gen — Berlin Space Technologies [cameras] https://newspacemarket.com/products/hrvi-6hd-2nd-generation-wide-swath-imager/ Design lifetime: 5 years @ LEO Ground sample distance: 4.6 m @ PAN @ 500km Ground sample distance: 9.2 m @ MS @ 500km Swath width: 70 km @ @ 500km Spectral bands: 5 @ 1 PAN + 4 MS Focal length: 500 Mass: 10450 g @ PLSU + 2x DCP Envelope (L×W×H): 540x320x170mm³ @ DCP (with Baffle) w/o PLSU Operating temperature: 0 °C (min) Operating temperature: 30 °C (max) Survival temperature: -15 °C (min) Survival temperature: 35 °C (max) Data interface: LVDS @ X-Band Data Output Data interface: Ethernet @ X-Band Data Output (variant 2) Data interface: RS-422 @ TMTC Interface Flight heritage: heritage line camera systems Sensor resolution: 2x 7920x6004 px @ Detector Size (per FPU) ## Auricam™ — Sodern [cameras] https://newspacemarket.com/products/sodern-auricam-d35-camera/ Design lifetime: 10 years @ LEO Design lifetime: 15 years @ GEO Sensor resolution: 4 Envelope (L×W×H): 80 x 80 x 140 mm @ D35 Mass: 420 g @ D35 Envelope (L×W×H): 90 x 90 x 135 mm @ D80 Mass: 450 g @ D80 Envelope (L×W×H): 71 x 65 x 155 mm @ D8 Mass: 550 g (max) @ D8 Supply voltage: 5 @ power supply Envelope (L×W×H): 91 x 117 x 25 mm @ Electronic unit Mass: 315 g @ Electronic unit Power consumption: 2.4 W @ BOL Electronic unit Power consumption: 2 W @ BOL Electronic unit (variant 2) Data interface: SpaceWire Focal length: 25 @ D35 Focal length: 10 @ D80 Focal length: 114 @ D8 Ground sample distance: 0.2 m @ @ 1km D35 Ground sample distance: 2 m @ @ 10km D35 Ground sample distance: 0.5 m @ @1km D80 Ground sample distance: 5 m @ @ 10 km D80 Ground sample distance: 0.05 m @ @1km D8 Ground sample distance: 0.48 m @ @10 km D8 Sensor resolution: 2048 x 2048 pixels @ (variant 2) Data interface: SpaceWire @ (variant 2) Supply voltage: 4.6-6 Power consumption: 2 W Operating temperature: -35-55 °C @ baseplate temp. Survival temperature: -45-60 °C @ baseplate temp, non-operating Survival temperature: -45-80 °C @ storage Flight heritage: AurigaTM Star Tracker with 1400+ Units flying and 40+ millions hours of successful operation Flight heritage: Navigation camera of JUICE mission @ (variant 2) Flight heritage: High performance Narrow Angle Camera of the Earth Return Orbiter (ERO) spacecraft @ (variant 3) ## Hawk 1920 — Raptor Photonics [cameras] https://newspacemarket.com/products/raptor-photonics-hawk-1920/ Sensor resolution: 1920 x 1080 Spectral bands: 300-1100nm @ monochrome Mass: 115 g Envelope (L×W×H): 48mm x 43mm x 43mm Supply voltage: 12 (nominal) Power consumption: 5 W (max) @ Total Power Consumption Data interface: Camera Link @ 12 bit base configuration Data interface: Camera link @ 8 bit Connector: Hirose part code HR10A-7R-4PB @ Power Operating temperature: -20-55 °C Survival temperature: -40-70 °C ## OwL 1280 — Raptor Photonics [cameras] https://newspacemarket.com/products/raptor-photonics-owl-1280/ Sensor resolution: 1280 x 1024 Spectral bands: 0.6µm to 1.7µm Mass: 200 g Envelope (L×W×H): 68.8mm x 46.0mm x 49.5mm Supply voltage: 12 (nominal) Supply voltage: 0.5 @ max_delta, DC Power consumption: 8 W (max) @ with TEC ON, NUC ON Data interface: HD-SDI SMPTE-274M Data interface: RS-422 @ (variant 2) Operating temperature: -40 °C (min) Operating temperature: 71 °C (max) Survival temperature: -55 °C (min) Survival temperature: 85 °C (max) Export status: This product is under the export control of UK government and maybe subject to an Single Individual export licence before shipment. ## NanoCam C1U — GomSpace [cameras] https://newspacemarket.com/products/nanocam-c1u/ Ground sample distance: 260 m @ 8 mm lens, from 650 km Ground sample distance: 60 m @ 35 mm lens, from 650 km Ground sample distance: 30 m @ 70 mm lens, from 650 km Spectral bands: 1 @ CMOS sensor Spectral bands: 400 Focal length: 8.2 @ Cinegon 1.4/8-0902 lens Focal length: 34.9 @ XENOPLAN 1.9/35MM COMPACT lens Focal length: 70.5 @ TELE-XENAR 2.2/70MM COMPACT lens Mass: 77 g @ system without optics Mass: 167 g @ with 8 mm lens Mass: 169 g @ with 35 mm lens Mass: 277 g @ with 70 mm lens Envelope (L×W×H): 86.0 x 91.7 x 55.1 mm @ with 8 mm lens Envelope (L×W×H): 86.0 x 91.7 x 57.9 mm @ with 35 mm lens Envelope (L×W×H): 86.0 x 91.7 x 97.2 mm @ with 70 mm lens Supply voltage: 3.2 (min) @ Supply voltage Supply voltage: 3.3 (nominal) @ Supply voltage Supply voltage: 3.6 (max) @ Supply voltage Power consumption: 0.38 W @ Idle Power consumption: 0.8 W @ Image acquisition Power consumption: 0.8 W @ Image processing Power consumption: 1.3 W @ System boot Data interface: CAN @ CSP-enabled Data interface: I2C @ CSP-enabled (variant 2) Data interface: RS-422 @ CSP-enabled (variant 3) Data interface: UART @ TTL level serial interfaces Data interface: USB @ Micro-B connector (production/update only) Connector: Picoblade. Right angle. Molex 53261-0471 @ GOSH Connector (J2) Connector: Picoblade. Right angle. Molex 53261-1571 @ Main Connector (J3) Operating temperature: 0 °C (min) Operating temperature: 60 °C (max) Survival temperature: -40 °C (min) Survival temperature: 85 °C (max) ## Teledyne e2v Space Imaging Detectors — CCDs and HgCdTe Infrared Sensors for Astronomy — Teledyne e2v [cameras] https://newspacemarket.com/products/teledyne-e2v-space-imaging-detectors-ccds-and-hgcdte-infrared-sensors-for-astronomy/ Focal length: 20 Envelope (L×W×H): 98.5 x 93.7 mm @ Package size Connector: Two 51-way micro-D Spectral bands: 300 nm, 350 nm, 400 nm @ Standard Silicon, Multi-25 Spectral bands: 350 nm, 400 nm, 500 nm, 650 nm, 900 nm @ Standard Silicon, Multi-2 Spectral bands: 350 nm, 400 nm, 500 nm, 650 nm, 900 nm @ Deep Depleted Silicon, Multi-2 Supply voltage: 9 (min) @ Image Area Clock Phases Supply voltage: 12 (max) @ Image Area Clock Phases Supply voltage: 25 (min) @ Output Drain Supply voltage: 31 (max) @ Output Drain Supply voltage: 0 (min) @ Substrate Supply voltage: 10 (max) @ Substrate Supply voltage: 9 (min) @ Reset Gate Supply voltage: 13 (max) @ Reset Gate Supply voltage: 9 (min) @ Summing Well Supply voltage: 12 (max) @ Summing Well Supply voltage: 16 (min) @ Reset Drain Supply voltage: 19 (max) @ Reset Drain Supply voltage: 1 (min) @ Output Gate (A) Supply voltage: 2 (typical) @ Output Gate (A) Supply voltage: 9 (min) @ Register Clock Phases Supply voltage: 12 (max) @ Register Clock Phases Supply voltage: 15 (min) @ Dump Drain (A) Supply voltage: 20 (max) @ Dump Drain (A) Power consumption: 0.058 W ## SPECTRE — Arcfield (formerly Orion Space Solutions) [cameras] https://newspacemarket.com/products/spectre-multi-spectral-optical-payload/ Power consumption: 46 W @ OAP Mass: 11000 g Spectral bands: 5 @ Visible (VIS), Near-Infrared (NIR), Short-Wave Infrared (SWIR), Mid-Wave Infrared (MWIR), and Lo Lead time: 11 @ from signed contract to delivery to the launch site ## HRVI-2HD — Berlin Space Technologies [cameras] https://newspacemarket.com/products/hrvi-2hd-high-resolution-video-imager/ Design lifetime: 5 years @ LEO Ground sample distance: 1.92 m @ @500km Swath width: 14.6 km (min) @ @500km Spectral bands: 5 @ 1x PAN & 4x MS Focal length: 1200 Mass: 19000 g Envelope (L×W×H): 520x780x335 mm³ ## RavenEye5 — CAVU Aerospace [cameras] https://newspacemarket.com/products/s-ldu-345-cubesat-camera/ Ground sample distance: 1 m @ Virtual for RGB model Swath width: 2.4 km @ 1/4 for multispectral model Connector: Nano-D 31P Supply voltage: 12 (min) Supply voltage: 18 (max) Power consumption: 14 W @ peak, measured at 12V Data interface: LVDS Data interface: RS422 @ (variant 2) Data interface: CAN @ Command And Telemetry Interface Data interface: UART @ Data Transmission Interface Data interface: RS-485 @ Data Transmission Interface (variant 2) Mass: 2000 g Envelope (L×W×H): 200 ×100× 100 mm3 Radiation tolerance (TID): 30 krad Operating temperature: -10 °C (min) Operating temperature: 50 °C (max) Design lifetime: 2 years (min) @ on Orbit ## Modular Electrical Power System 2 — ISISPACE Group [eps] https://newspacemarket.com/products/isispace-modular-electrical-power-system-2/ Envelope (L×W×H): 11 mm @ Height Mass: 51.6 g @ incl. top mount full CSKB Mass: 57.4 g @ incl. bottom mount full CSKB Power consumption: 0.066 W @ Idle consumption (regulation of VD1 at 5V and VD2 at 3.3V, no external load) Supply voltage: 12.8-16 @ Supply/bus voltage (Rail Voltage) Output rails: VD0: fixed (= rail voltage) Output rails: VD1: user selectable (only below rail voltage) @ (variant 2) Output rails: VD2: user selectable (only below rail voltage) @ (variant 3) Output rails: VDx: x 4 (Option using DaughterBoard mounted regulator) @ (variant 4) Protections: Overcurrent/thermal limit on Unit input Protections: Overvoltage protection on all domains @ (variant 2) Protections: Overcurrent/thermal protection on each output bus channel @ (variant 3) Protections: Voltage ramp slew rate control on each output bus channel @ (variant 4) Protections: Reverse current protection on each output bus channel @ (variant 5) Protections: Safety Mode (when VD0 low) @ (variant 6) Protections: Emergency Low Power Mode (when VD0 low) @ (variant 7) Protections: Hardware Supervisor including Watchdog @ (variant 8) Protections: TT&C Watchdog (stack reset on EPS comms timeout) @ (variant 9) Data interface: I2C Data interface: UART @ (variant 2) Data interface: SPI optional @ (variant 3) Operating temperature: -40-70 °C Survival temperature: -40-85 °C Design lifetime: 12 years Flight heritage: Design based on heritage from ICEPS1 design flown on PEASSS CubeSat (2016). IMEPS1, first generation, flown in 2018. IMEPS2 first flown in 2020. ## Compact Electrical Power System 2 — ISISPACE Group [eps] https://newspacemarket.com/products/isispace-compact-electrical-power-system-2/ Output rails: 3.3V, 5V, VBAT Protections: Battery charge and discharge protection Protections: Low side and high side inhibit switches @ (variant 2) Protections: I2C Watchdog (stack reset on comms failure) @ (variant 3) Protections: Complete output bus protection including short circuit and backflow protection @ (variant 4) Protections: Back-to-back (B2B) protection MOSFETs @ (variant 5) Protections: Optional third low side separation switch @ (variant 6) Protections: Charge load switch for charge current limiting, with under and overvoltage lockout @ (variant 7) Protections: Trickle charge bypass diode to resuscitate batteries that have dropped to voltages below the charge undervoltage lockout threshold @ (variant 8) Protections: Discharge load switch for active discharge current limiting @ (variant 9) Protections: Surge protection using TVS protection diodes @ (variant 10) Mass: 365 g (max) Envelope (L×W×H): 96 x 92 x 16 mm3 @ IU mainboard + DaughterBoard Envelope (L×W×H): 94 x 89 x 21.0 mm3 @ 4 cell BP Power consumption: 0.093 W @ Static (Idle) consumption Operating temperature: -40 °C (min) @ Without battery Operating temperature: 85 °C (max) @ Without battery Survival temperature: -50 °C (min) @ Storage temperature Survival temperature: 65 °C (max) @ Storage temperature Operating temperature: 10 °C (min) @ With battery, charge Operating temperature: 45 °C (max) @ With battery, charge Operating temperature: 0 °C (min) @ With battery, charge up to 800 mA Operating temperature: 45 °C (max) @ With battery, charge up to 800 mA Operating temperature: -20 °C (min) @ With battery, discharge Operating temperature: 60 °C (max) @ With battery, discharge Survival temperature: -20 °C (min) @ With battery, up to 1 month Survival temperature: 50 °C (max) @ With battery, up to 1 month Survival temperature: -20 °C (min) @ With battery, up to 3 months Survival temperature: 40 °C (max) @ With battery, up to 3 months Survival temperature: -20 °C (min) @ With battery, up to 1 year Survival temperature: 20 °C (max) @ With battery, up to 1 year Data interface: I2C Flight heritage: Design based on heritage from ICEPS1 design flown on PEASSS CubeSat (2016). ICEPS2, second generation, flown on the Hiber 1,2 CubeSats (2018) ## CubeSat EPS – STARBUCK-Nano — AAC Clyde Space [eps] https://newspacemarket.com/products/aac-cubesat-eps-starbuck-nano/ Output rails: 3.3V, 5V, and 12V Protections: 10 Latching Current Limiters Design lifetime: 5 years @ in LEO Output rails: 3.3V, 5V, and 12V @ (variant 2) Protections: 10 Configurable Latching Current Limit (LCL) @ (variant 2) Data interface: I2C Supply voltage: 8.2 (max) @ Battery Operating temperature: -40 °C (min) Operating temperature: 85 °C (max) Survival temperature: -50 °C (min) Survival temperature: 100 °C (max) Radiation tolerance (TID): 10 krad Mass: 86 g @ typical Envelope (L×W×H): 95.89 mm x 90.17 mm x 16.2 mm ## Linear EPS Module (LEPSM1) — Pumpkin, Inc. [eps] https://newspacemarket.com/products/pumpkin-linear-eps-module-lepsm1/ Output rails: Unregulated battery power (6 - 8.2Vdc), Regulated +5V, +3.3V Protections: Auto-resetting overcurrent trip fuses on battery, +5V and +3.3V outputs, overcurrent, overvoltage and undervoltage protection circuits (internal to batteries) Mass: 155 g @ With option /00 Mass: 210 g @ With option /01 Envelope (L×W×H): 90 mm x 96 mm x (14 mm or 24 mm + 2 mm) PCB (Length x Width x Height above PCB + Height below PCB) Data interface: I2C ## High-Power Electrical Power System Module (EPSM1) — Pumpkin, Inc. [eps] https://newspacemarket.com/products/pumpkin-epsm1/ Mass: 300 g Mass: 230 g @ Aluminum standoffs, no heat spreader Conversion efficiency: 96 Conversion efficiency: 98.5 @ (variant 2) Conversion efficiency: 97.5 @ minimum efficiency over a wide range of operating currents Output rails: 3.3/5.0/12V @ 3 regulated outputs Output rails: 4-28V @ 1 switchable regulated output Protections: 2 programmable overtemperature (OT) limits Protections: Programmable crowbar current limits @ (variant 2) Protections: Input overvoltage shunt @ (variant 3) Protections: programmable current limit, protected against overcurrent faults @ (variant 4) Envelope (L×W×H): 96 mm x 90 mm x 15.24 mm @ nominal, without any additional heatsinks Supply voltage: 8 (min) @ Solar array input, normal operating conditions Supply voltage: 28 (max) @ Solar array input, normal operating conditions Supply voltage: 16.8 (nominal) @ battery block Supply voltage: 16.8 (nominal) @ Li-Ion batteries Power consumption: 3 W Power consumption: 2 W @ Operating power consumption, Deployment switches not inhibited; no commands or telemetry active Data interface: I2C Connector: discrete connectors @ Solar array inputs Connector: 104-pin connector @ Regulated and unregulated outputs Connector: dedicated, high-current connectorized harnesses @ Battery charger connections Operating temperature: -40 °C (min) Operating temperature: 85 °C (max) ## Modular Electrical Power System (IMEPS2) — Innovative Space Logistics [eps] https://newspacemarket.com/products/modular-electrical-power-system-imeps2-1478/ Envelope (L×W×H): 11 mm @ PDU Height Mass: 51.6 g @ PDU incl. top mount full CSKB Mass: 57.4 g @ PDU incl. bottom mount full CSKB Power consumption: 0.066 W @ PDU Idle consumption (regulation of VD1 at 5V and VD2 at 3.3V, no external load) Supply voltage: 12.8-16 @ PDU input max Output rails: VD0: fixed (= rail voltage); VD1: user selectable (only below rail voltage); VD2: user selectable (only below rail voltage) Output rails: VDx: x 4 (Option using DaughterBoard mounted regulator) @ (variant 2) Protections: - Overcurrent/thermal limit on Unit input; - Overvoltage protection on all domains; - On each output bus channel: Overcurrent/thermal protection; - Voltage ramp slew rate control; - Reverse current protection; - Safety Mode (when VD0 low); - Emergency Low Data interface: I2C Data interface: UART @ (variant 2) Data interface: SPI @ optional Operating temperature: -40-70 °C Survival temperature: -40-85 °C Flight heritage: Design based on heritage from ICEPS1 design flown on PEASSS CubeSat (2016). IMEPS1, first generation, flown in 2018. IMEPS2 first flown in 2020. ## Umbra Space Systems — Umbra Lab Inc. [eps] https://newspacemarket.com/products/umbra-mss-package/ Envelope (L×W×H): 2.02 in x 1.4 in x 0.1 in Mass: 65 g (max) Supply voltage: 5 (nominal) Supply voltage: 5 Power consumption: 0.01 W (max) @ Peak Power Power consumption: 0.01 W (max) @ Average Power Data interface: RS-422 Connector: 15-Pin Micro-D Connector Design lifetime: 5 years Radiation tolerance (TID): 30 krad Flight heritage: Acceptance tested and Flight Heritage ## Integrated Electronics Module (IEM) — Tiger Innovations, Inc. [eps] https://newspacemarket.com/products/tiger-innovations-integrated-electronics-module/ Power consumption: 24 W @ nominal Mass: 5250 g (max) Envelope (L×W×H): 7” x 7.125” x 4.437” Supply voltage: 28 Output rails: +3.3V, ±5V, ±15V Radiation tolerance (TID): 100 krad Flight heritage: STPSat-1 Data interface: RS-422 Power consumption: 24.08 W @ total, nominal ## ISISPACE Compact Electrical Power System — ISISPACE Group [eps] https://newspacemarket.com/products/isispace-compact-electrical-power-system/ Output rails: 3.3V, 5V, unregulated bus Protections: Hardware over-current protection Protections: Hardware supervisor including watchdog @ (variant 2) Protections: I2C Watchdog (stack reset on comms failure) @ (variant 3) Data interface: I2C Flight heritage: Design based on heritage from PEASSS Cubesat (2016). Flight heritage: Second generation improvements flown on the Hiber 1,2 Cubesats (2018). @ (variant 2) Design lifetime: 12 years @ Storage lifetime (at relative humidity < 60 %) Power consumption: 0.093 W @ Static (Idle) consumption Output rails: Battery Voltage @ VD0 Output power (total): 28.8 W @ PBP 2S1P Output power (total): 57.6 W @ PBP 4S1P Mass: 184 g @ Type A Mass: 310 g @ Type B Mass: 360 g @ Type C Envelope (L×W×H): 96 x 92 x 26.5 @ Type A IU mainboard + 2 cell BP Envelope (L×W×H): 96 x 92 x 11.3 @ Type B IU mainboard Envelope (L×W×H): 96 x 92 x 16 @ Type C IU mainboard + daughterboard Envelope (L×W×H): 94 x 89 x 21.0 @ Type B and C 4 cell BP ## Amun — Spacemanic s.r.o. [eps] https://newspacemarket.com/products/spacemanic-amun/ Operating temperature: -40-85 °C Envelope (L×W×H): 90.2 x 95.9 x 19.7 mm Mass: 185 g Output rails: 1x VBAT, 1x 3.3V, 1x 5V, 4x 3.3/5V conf. Conversion efficiency: 73 @ Solar input system Power consumption: 0.0002 W @ Typ. 3.3 V self-consumption Power consumption: 0.0001 W @ Typ. 5 V self-consumption Data interface: UART Data interface: I2C @ (variant 2) Data interface: RS-485 @ (variant 3) Data interface: CAN @ (variant 4) Connector: SAMTEC SSQ-126-03-G-D Connector: Molex PicoBlade 53261-0471 @ Solar input on module Connector: Molex PicoBlade 51021-0400 @ Solar input mates with (cable) Connector: Molex PicoBlade 53261-0271 @ RBF and DS on module Connector: Molex PicoBlade 51021-0200 @ RBF and DS mates with (cable) Connector: Molex PicoBlade 53398-0671 @ EGSE on module Connector: Molex PicoBlade 51021-0600 @ EGSE mates with (cable) Flight heritage: on 10+ missions (e.g. LASARsat, CroCube, GRBBeta and external customers) ## PCU-110 — Berlin Space Technologies [eps] https://newspacemarket.com/products/bst-pcu-110-power-control-unit/ Flight heritage: since 2015 Data interface: RS-422 Data interface: other @ 1-Wire Supply voltage: 20.5 (min) Supply voltage: 23.1 (nominal) Supply voltage: 25.2 (max) Output power (total): 180 W Power consumption: 0.5 W @ idle Envelope (L×W×H): 186.0 x 105.5 x 60.6 mm³ Mass: 1080 g Survival temperature: -30 °C (min) Survival temperature: 50 °C (max) Operating temperature: -20 °C (min) Operating temperature: 40 °C (max) Design lifetime: 5 years Output rails: 2x 12V, 12x 5V, 5x 3.8V @ Regulated (standard) Output rails: Any between 1.8V to 28V @ Regulated (optional) Output rails: 12x 23.1 V (20-25 V) @ Unregulated Protections: Adjustable Switches and Fuses Protections: Latch Protection @ (variant 2) Protections: Schmitt Trigger @ Battery Protection Protections: intelligent Power Management @ Battery Protection (variant 2) Design lifetime: 5 years @ LEO ## PSR 100V MKII — Airbus Defence and Space [eps] https://newspacemarket.com/products/airbus-pureline-pearl-pcdu/ Output power (total): 1500 W (max) @ Distributed Power Conversion efficiency: 98 (min) @ Energy transfer efficiency Output rails: 22V-38V nominal voltage range Protections: Fuse protection lines up to 5Amp Class Protections: latch-up free parts @ (variant 2) Protections: error protection mechanisms @ (variant 3) Mass: 2500 g Envelope (L×W×H): 395 x 125 x 65mm3 Supply voltage: 22-38 @ Bus Voltage (Battery follower) Supply voltage: 22-75 @ Input Solar Array Voltage Power consumption: 760 W @ Solar Array Power (20A charge) Power consumption: 1500 W @ Distributed Power @ 38V (40A) Power consumption: 20 W (max) @ Power dissipation Data interface: CAN @ Redundant CAN serial bus Data interface: CAN @ TM/TC interface (N&R) Operating temperature: -30-60 °C Radiation tolerance (TID): compatible with typical 10 years LEO Design lifetime: 10 years @ typical, in LEO Flight heritage: On orbit since February 2019 ## BRAVO-II Motor Controller — Motiv Space Systems [eps] https://newspacemarket.com/products/motiv-motor-controllers/ Supply voltage: 28 (nominal) @ Input Voltage Range Supply voltage: 22 (min) @ Input Voltage Range Supply voltage: 34 (max) @ Input Voltage Range Power consumption: 5 W @ Quiescent Power Data interface: RS-422 @ Standard Data interface: RS-485 @ Standard (variant 2) Data interface: CAN @ Standard (variant 3) Data interface: MIL-STD-1553 @ Option Data interface: SpaceWire @ Option (variant 2) Data interface: Ethernet @ Option (variant 3) Operating temperature: -55 °C (min) @ Operating Temperature Operating temperature: 70 °C (max) @ Operating Temperature Survival temperature: -55 °C (min) @ Non-Operating Temperature Survival temperature: 125 °C (max) @ Non-Operating Temperature Radiation tolerance (TID): 100 krad @ Radiation Tolerance TID Envelope (L×W×H): 22.8cm x 13.4cm x 6.8cm @ packaged Mass: 2020 g ## XTERRA CubeSat Dispenser (XCD) Hybrid — XTERRA (Arrow Science and Technology) [deployers] https://newspacemarket.com/products/xcd-12u-16u-hybrid-dispenser/ Flight heritage: Over 400 satellites Capacity: 6 @ up to a single payload Capacity: 3 @ config houses up to two payloads Max payload mass: 2170 g @ 1U Max payload mass: 4330 g @ 2U Max payload mass: 6500 g @ 3U Max payload mass: 3250 g @ 2U (variant 2) Max payload mass: 8670 g @ 4U Max payload mass: 13000 g @ 6U Mass: 7250 g @ Empty Dispenser, 3U Configuration Mass: 6500 g @ Empty Dispenser, 6U Configuration Mass: 14700 g @ Empty Dispenser, 3U/3U Quadpack Configuration Mass: 13900 g @ Empty Dispenser, 3U/6U Quadpack Configuration Mass: 13200 g @ Empty Dispenser, 6U/6U Quadpack Configuration Actuation: spring Separation velocity: 0.8 m/s @ 3U, 2.00kg Separation velocity: 1.1 m/s @ 3U, 4.00kg Separation velocity: 0.9 m/s @ 3U, 6.00kg Separation velocity: 1.1 m/s @ 6U, 6.00kg Separation velocity: 1 m/s @ 6U, 8.00kg Separation velocity: 0.9 m/s @ 6U, 10.00kg Separation velocity: 0.8 m/s @ 6U, 12.00kg Flight heritage: Over 400 deployments @ (variant 2) ## Hyperion PocketQube Deployer — Quub (Mini-Cubes) [deployers] https://newspacemarket.com/products/quub-hyperion-pocketqube-deployer/ Max payload mass: 1000 g @ total Actuation: spring Mass: 600 g @ Total Deployer Mass Envelope (L×W×H): 192 (w) × 108 (d) × 279 (h) mm Supply voltage: 12 (nominal) @ command input ## GPOD CubeSat Deployer — GAUSS Srl [deployers] https://newspacemarket.com/products/gauss-gpod-deployer/ Mass: 1900 g Max payload mass: 4000 g @ Nominal Max payload mass: 5200 g Envelope (L×W×H): 430 x 132 x 129 @ Outside envelope 3U Separation velocity: 1.11-1.25 m/s @ With nominal Payload Mass Actuation: non-pyro Flight heritage: The GPOD flew successfully on UniSat-5 and UniSat-6 in two different Dnepr LV missions. ## EBAD TiNi Microlatch ML50-1 Separation System — Ensign-Bickford Aerospace & Defense (EBAD) [deployers] https://newspacemarket.com/products/ebad-tini-microlatch-ml50-1-separation-system/ Actuation: non-pyro Supply voltage: 3-5.5 ## ESPA Separation System (PSR 1575 mm / 62 in) — Beyond Gravity (ex-RUAG Space) [deployers] https://newspacemarket.com/products/beyond-gravity-espa-psr-1575-separation-system/ Flight heritage: 40 years of flight heritage ## PAS 381S (15 in) Separation System — Beyond Gravity (ex-RUAG Space) [deployers] https://newspacemarket.com/products/beyond-gravity-pas-381s-separation-system/ Mass: 3700 g @ Total Mass: 980 g @ Separated mass Envelope (L×W×H): Height 79 mm Actuation: other Flight heritage: flight proven systems at Beyond Gravity. Developed for over 30 years, the Beyond Gravity Space product family to date includes a broad range of Separation Systems, spanning diameters from 360mm to 2624mm (14” to 103”). Our Separation Systems have an outst ## PAS 432S (17 in) Separation System — Beyond Gravity (ex-RUAG Space) [deployers] https://newspacemarket.com/products/beyond-gravity-pas-432s-separation-system/ Max payload mass: 200000 g @ @ 0.45 mm Mass: 7200 g @ Total 1) Mass: 1900 g @ Separated mass Envelope (L×W×H): 123 mm Actuation: non-pyro Flight heritage: 30 years of flight heritage ## PAS 610S (24 in) Separation System — Beyond Gravity (ex-RUAG Space) [deployers] https://newspacemarket.com/products/beyond-gravity-pas-610s-separation-system/ Mass: 5800 g @ Total Mass: 1000 g @ Separated mass Envelope (L×W×H): Height 73 mm Flight heritage: The PAS 610S Separation System is based on the already flight proven systems at Beyond Gravity. Developed for over 30 years, the Beyond Gravity Space product family to date includes a broad range of Separation Systems, spanning diameters from 360 mm to 26 ## Deployers 3U — KOSMOLAB Launch Services [deployers] https://newspacemarket.com/products/deployers-3u/ Capacity: 3 Envelope (L×W×H): 557 × 158 × 187 mm Mass: 4700 g Max payload mass: 6000 g Separation velocity: 0.5-2 m/s Operating temperature: -60-60 °C Lead time: 4-6 ## XCD-3U/6U Hybrid — XTERRA (Arrow Science and Technology) [deployers] https://newspacemarket.com/products/xterra-xcd-3u-6u-hybrid/ Flight heritage: XTERRA has designed and/or manufactured hardware that has successfully deployed over 400 satellites Flight heritage: Over 95% of our 400+ satellite deployments use these preload fundamentals @ (variant 2) Capacity: 12 @ can be converted from Capacity: 16 @ can be converted to Max payload mass: 32000 g Actuation: motor Mass: 17910 g @ Empty Dispenser Connector: standard ## XCD-12U/16U Hybrid — XTERRA (Arrow Science and Technology) [deployers] https://newspacemarket.com/products/xterra-xcd-12u-16u-hybrid/ Capacity: 12 (min) Capacity: 16 (max) Max payload mass: 28000 g @ 12U Max payload mass: 32000 g @ 16U Actuation: actuator Mass: 17910 g @ Empty Dispenser Flight heritage: successfully deployed over 400 satellites Flight heritage: Over 95% of our 400+ satellite deployments use these preload fundamentals @ (variant 2) ## ASTROFEIN PicoSatellite Launcher PSL1U / PSL2U / PSL3U — EXA (Astro-und Feinwerktechnik) [deployers] https://newspacemarket.com/products/psl1u-psl2u-psl3u-picosatellite-launcher/ Max payload mass: 1330 g Max payload mass: 2660 g @ (variant 2) Max payload mass: 4000 g @ (variant 3) ## Reliable and Advanced Mission Injector (RAMI) — UARX Space [deployers] https://newspacemarket.com/products/rami-cubesat-deployer/ Capacity: 12 (max) @ 1x 12U Capacity: 6 (max) @ 2x 6U Capacity: 6 (max) @ 1x 6U + 2x 3U Capacity: 3 (max) @ 4x 3U Max payload mass: 30000 g Envelope (L×W×H): 330.6 mm x 383.9 mm x 448.8 mm Mass: 9000 g (min) @ configuration dependant Actuation: non-pyro ## TOTEM — Software Defined Radio — Alén Space [sdr-modems] https://newspacemarket.com/products/alen-totem-sdr/ Frequency: 70-6000 MHz Mass: 130 g @ with shieldings Envelope (L×W×H): 89.3 mm x 93.3 mm Supply voltage: 5 Operating temperature: -40-85 °C Data interface: Ethernet Data interface: UART @ (variant 2) Data interface: JTAG @ (variant 3) Data interface: I2C @ (variant 4) Data interface: CAN @ (variant 5) Frequency: 70-6000 MHz @ (variant 2) Data interface: LVDS @ (variant 6) Supply voltage: 4.7-5.2 Power consumption: 1.4 W @ typical Power consumption: 2.62 W @ max Supply voltage: 3.7-6 @ Absolute maximum Operating temperature: -40-85 °C @ Absolute maximum Envelope (L×W×H): 93.3 x 89.3 x 5 mm @ (variant 2) Mass: 59 g @ shielding not included Mass: 130 g @ shieldings included ## SWIFT Software-Defined Radio Family — Tethers Unlimited, Inc. (AMERGINT) [sdr-modems] https://newspacemarket.com/products/tethers-unlimited-swift-sdr-family/ Data rate: 25000 kbps @ Tx Data rate: 5000000 kbps @ Rx Frequency: 1700-2300 MHz TX power: 1.995 W @ Finely Adjustable Modulation: BPSK, AMFSK, SGLS, USB @ Rx Modulation: BPSK, QPSK, OQPSK, 8PSK, 16APSK, SGLS, USB @ Tx Envelope (L×W×H): (L) 98 x (W) 94 x (H) 42 mm Mass: 400 g (max) Supply voltage: 9-34.6 Power consumption: 16 W @ Operating Power Power consumption: 4 W @ Standby Power Operating temperature: -30C to +60C Radiation tolerance (TID): 40 krad Data interface: RS-422 @ for TT&C (Prime and Redundant ports) Data interface: LVDS @ for Data Transfer Connector: SMA @ 1 Tx port Connector: SMA @ 1 Rx port Protocols / waveforms: CCSDS TM/TC/AOS/Security Packet Flight heritage: Proven communications on several missions Flight heritage: Units currently on-orbit supporting LEO & GEO missions @ (variant 2) ## SWIFT® Radios and RAVEN – SDR — Tethers Unlimited, Inc. (AMERGINT) [sdr-modems] https://newspacemarket.com/products/tethers-unlimited-raven-sdr/ Data rate: 25000 kbps @ Tx Data rate: 5000 kbps @ Rx Frequency: 1700-2300 TX power: 1.995 W Modulation: BPSK, AMFSK, SGLS, USB (Rx) Modulation: BPSK, QPSK, OQPSK, 8PSK, 16APSK, SGLS, USB (Tx) @ (variant 2) Envelope (L×W×H): (L) 98 x (W) 94 x (H) 42 mm Mass: 400 g (max) Supply voltage: 9-34.6 Power consumption: 16 W (max) @ Operating Power Power consumption: 4 W (max) @ Standby Power Operating temperature: -30C to +60C Radiation tolerance (TID): 40 krad Data interface: RS-422 @ for TT&C (Prime and Redundant ports) Data interface: LVDS @ for Data Transfer Connector: SMA @ 1 Tx port Connector: SMA @ 1 Rx port Protocols / waveforms: Convolutional Coding, Reed Solomon, LDPC, BCH (Forward Error Correction) Protocols / waveforms: CCSDS TM/TC/AOS/Security Packet, Gryphon Framing, NTIA/SFCG Mask Compliant, PN Ranging (one-way, two-way) @ (variant 2) Flight heritage: Flight Heritage, Proven communications on several missions, Units currently on-orbit supporting LEO & GEO missions ## U7720 – High-Performance Networking Satellite Modem/Router — SpaceBridge Inc. [sdr-modems] https://newspacemarket.com/products/u7720-odu/ Protocols / waveforms: DVB-S2/S2X ACM @ Forward Link Protocols / waveforms: DVB-RCS2 @ Return Link Frequency: 950-2150 MHz @ Receive Modulation: QPSK to 256APSK @ Forward Link Protocols / waveforms: 3D-TDMA and WaveSwitch @ Forward Link TDMA (Tx) Modulation: SS-BPSK, BPSK, QPSK, 8PSK, 16QAM, 32QAM, 64QAM @ Forward Link TDMA (Tx) TX power: 0-0.001 W Frequency: 950-2400 MHz @ Terminal IFL TX Interface Data rate: 100000 kbps @ Download speed Data rate: 25000 kbps @ Upload speed Data rate: 20000 kbps @ Return Link dSCPC (Tx) Upload Speed Data interface: Ethernet @ U7720-60/SA/ODU Data interface: Ethernet @ U7720-120 Envelope (L×W×H): 19 x 6 x 1.75 inches (482.6 x 153.4 x 44.4 mm) @ U7720-60 Envelope (L×W×H): 19 x 12 x 1.75 inches (482.6 x 306.8 x 44.4 mm) @ U7720-120 Envelope (L×W×H): 5 x 9 x 7 inches (127 x 229 x 178 mm) @ Outdoor IP-67 enclosure Mass: 3400 g (max) Power consumption: 60 W @ U7720-60 and ODU (AC PS) Power consumption: 40 W (max) @ U7720-60 and ODU (RF/BUC power) Power consumption: 120 W @ U7720-120 (AC PS) Power consumption: 100 W @ U7720-120 (RF/BUC power) Supply voltage: 90-260 @ U7720-60 and ODU (AC PS) Supply voltage: 90-260 @ U7720-120 (AC PS) Supply voltage: 24 @ U7720-ODU (external) Power consumption: 20 W (max) @ U7720-ODU (external) Supply voltage: 24 @ U7720-SA (external) Power consumption: 60 W @ U7720-SA (external) Power consumption: 40 W (max) @ U7720-SA (RF/BUC power) Operating temperature: 0-50 °C @ Indoor rack mount Operating temperature: -30-60 °C @ Outdoor enclosure Survival temperature: -40-85 °C ## U7780 – ESTELLA System Professional MF-TDMA Satellite Modem — SpaceBridge Inc. [sdr-modems] https://newspacemarket.com/products/u7780/ Data rate: 120000 kbps @ Download speed Data rate: 25000 kbps @ Upload Speed Data rate: 25000 kbps @ Upload Speed (WaveSwitch) Frequency: 950-2150 MHz @ Terminal IF RX Frequency: 950-2400 MHz @ Terminal IFL TX TX power: 0 W (min) TX power: 0.001 W (max) Mass: 3400 g Supply voltage: 24 @ input Supply voltage: 100-240 @ Option: DIN Rail mounted Supply voltage: 48 @ Option: DIN Rail mounted Power consumption: 30 W @ to U7780 modem and LNB Power consumption: 100 W @ to the BUC Power consumption: 120 W @ Option: DIN Rail mounted 100-240VAC to 24VDC Power consumption: 240 W @ Option: DIN Rail mounted 100-240VAC to 24VDC (variant 2) Power consumption: 120 W @ Option: DIN Rail mounted 48VDC to 24VDC Power consumption: 240 W @ Option: DIN Rail mounted 48VDC to 24VDC (variant 2) Operating temperature: 0-60 °C ## U7900 – High-Performance Networking Satellite Modem/Router — SpaceBridge Inc. [sdr-modems] https://newspacemarket.com/products/u7900/ Frequency: 950-2150 MHz @ RX Data rate: 700000 kbps @ downstream Data rate: 50000 kbps @ upstream Data rate: 100000 kbps @ download speed Data rate: 25000 kbps @ upload speed TX power: 0-0.001 W Modulation: QPSK to 256 APSK @ Forward Link Modulation: QPSK, 8PSK, 16QAM @ Return Link Protocols / waveforms: DVB-S2X, DVB-RCS2 Mass: 3400 g Envelope (L×W×H): 435 x 45 x 272 mm Supply voltage: 24 Supply voltage: 100-240 @ Option Power consumption: 30 W @ to U7780 modem and LNB Power consumption: 100 W @ to the BUC Data interface: Ethernet @ User ports Data interface: Ethernet @ MGMT ports Connector: F-type 75 Ohm @ Terminal IF RX Interface Connector: F-type 75 Ohm @ Terminal IFL TX Interface Operating temperature: 0-60 °C ## U7920 – High-Performance Networking Satellite Modem/Router — SpaceBridge Inc. [sdr-modems] https://newspacemarket.com/products/u7920/ Protocols / waveforms: DVB-RCS2 Protocols / waveforms: OpenAMIP @ (variant 2) Data rate: 300000 kbps @ forward link Data rate: 20000 kbps @ return link Protocols / waveforms: DVB-S2X @ (variant 3) Modulation: QPSK to 16QAM Frequency: 950-2150 MHz @ Forward Link Modulation: DVB-S2/S2X: QPSK to 256 APSK @ Forward Link Data interface: Ethernet @ User Data interface: Ethernet @ MGMT Data rate: 300000 kbps @ Download speed Data rate: 20000 kbps @ Upload speed Protocols / waveforms: IPv4/IPv6, IGMP, 802.1q @ (variant 4) Envelope (L×W×H): 435 x 306.8 x 44.4 mm Mass: 3400 g (max) Power consumption: 40 W @ modem Power consumption: 100 W @ to BUC/LNB Operating temperature: 0-50 °C Survival temperature: -40-85 °C Modulation: QPSK, 8PSK, 16QAM @ Return Link TX power: 0-0.001 W ## U7400-M Satellite Mesh Modem (ASAT™ System Mesh Satellite Modem) — SpaceBridge Inc. [sdr-modems] https://newspacemarket.com/products/u7400-m/ Frequency: 950 MHz (min) @ Terminal IFL Input/Output Frequency: 2150 MHz (max) @ Terminal IFL Input/Output Data rate: 100000 kbps (max) @ Download Speed Data rate: 100000 kbps (max) @ Upload Speed Modulation: QPSK up to 256APSK LDPC/BCH Modulation: BPSK, QPSK, 8PSK, 16QAM @ (variant 2) Protocols / waveforms: DVB-S2/S2X ACM, GSE encapsulation Mass: 3800 g Envelope (L×W×H): 435 x 45 (1RU) x 315mm (W x H x D) Supply voltage: 100 (min) @ universal AC Supply voltage: 240 (max) @ universal AC Supply voltage: -48 @ DC power supply option Supply voltage: 24 @ DC to BUC Power consumption: 50 W @ not including RF equipment / BUC power Power consumption: 65 W @ available for installation and RF equipment Data interface: Ethernet @ 1x 10/100/1000 Mbps Eth RJ-45 Connector: RJ-45 Connector: F-type 75 ohm @ (variant 2) Operating temperature: 0 °C (min) Operating temperature: 50 °C (max) ## SBM-90X Wideband GEO SCPC Professional Modem — SpaceBridge Inc. [sdr-modems] https://newspacemarket.com/products/sbm-90x-wideband-geo-leo-meo-scpc-mcpc-modem/ Data rate: 738000 kbps @ TX Data rate: 738000 kbps @ RX Modulation: QPSK up to 256APSK LDPC/ BCH @ TX Modulation: QPSK up to 256APSK LDPC/ BCH @ RX Protocols / waveforms: DVB-S2X (EN 302 307-2) @ TX Protocols / waveforms: DVB-S2X (EN 302 307-2) @ RX Envelope (L×W×H): 435 x 45 (1RU) x 292 mm (W x H x D) Power consumption: 150 W @ AC Data interface: Ethernet @ user data Data interface: Ethernet @ modem management Connector: N type @ TX IFL Output Frequency: 950-2150 MHz @ TX L-band Connector: N type @ RX IFL Input Frequency: 950-2150 MHz @ RX L-band ## QubeFlex CubeSat/SmallSat Transceiver/Modem — Teledyne Defence & Space [sdr-modems] https://newspacemarket.com/products/qubeflex-cubesat-smallsat-transceiver-modem/ Data rate: 5000 kbps @ Options Data rate: 10000 kbps @ Options (variant 2) Data rate: 25000 kbps @ Options (variant 3) Data rate: 50000 kbps @ Options (variant 4) Modulation: BPSK, QPSK & OQPSK 1/2, 2/3, 3/4,5/6, 7/8 @ Modulator Protocols / waveforms: CCSDS (CCSDS 131.0-B-1) Protocols / waveforms: Intelsat (IESS-308) @ (variant 2) Mass: 3000 g Envelope (L×W×H): 1U chassis, 285mm deep excluding front panel handles and rear panel connectors and fans Supply voltage: 24 @ DC options Supply voltage: 48 @ DC options (variant 2) Data interface: Ethernet Data interface: Ethernet @ (variant 2) Data interface: RS-422 @ (variant 3) Data interface: other @ X.21 Data interface: other @ V.35 Data interface: RS-232 @ (variant 4) Data interface: LVDS @ (variant 5) Data interface: LVDS @ (variant 6) Connector: N-type connectors @ Tx & Rx Connector: 25-pin D-type female connector @ Serial EIA-530 Interface Connector: 25-pin D-type female connector @ High-speed Serial LVDS Interface ## Software Defined Radio (SDR) — Plan-S (Connecta) [sdr-modems] https://newspacemarket.com/products/software-defined-radio-sdr-4217/ Frequency: 70 MHz (min) Frequency: 6000 MHz (max) Supply voltage: 6 (min) @ SDR_PWR Supply voltage: 15 (max) @ SDR_PWR Power consumption: 7 W (max) @ without RF_FE Data interface: LVDS Data interface: JTAG @ (variant 2) Data interface: I2C @ (variant 3) Data interface: UART @ (variant 4) Data interface: SPI @ (variant 5) Data interface: USB @ (variant 6) Data interface: CAN @ (variant 7) Data interface: Ethernet @ (variant 8) Connector: 0.8mm Pitch Edge Type Connector (compatible with Samtech HSEC8-DV) Mass: 280 g (max) Operating temperature: -40 °C (min) @ Thermal Cycling Test Operating temperature: 85 °C (max) @ Thermal Cycling Test Flight heritage: Flight heritage demonstrated on 16 satellites with 32 units ## NanoCom SDR MK3 with 1xTR600 — GomSpace [sdr-modems] https://newspacemarket.com/products/nanocom-sdr-mk3-with-1xtr600/ Mass: 272 g @ typical Envelope (L×W×H): 95 x 95 x 23,85 mm Frequency: 70-6000 MHz Operating temperature: -40-50 °C Survival temperature: -40-85 °C Supply voltage: 12-32 Power consumption: 2.22 W @ Vin = 12V, 25°C, Linux running in idle, default after startup, no PL services running, no extern Power consumption: 2.25 W @ Vin = 18V, 25°C, Linux running in idle, default after startup, no PL services running, no extern Power consumption: 2.4 W @ Vin = 24V, 25°C, Linux running in idle, default after startup, no PL services running, no extern Power consumption: 2.56 W @ Vin = 32V, 25°C, Linux running in idle, default after startup, no PL services running, no extern Power consumption: 5.46 W @ Vin = 12V, 25°C, enable one TR600 on Slot A, TR600(s) are powered-on (PL activated) without any Power consumption: 5.58 W @ Vin = 18V, 25°C, enable one TR600 on Slot A, TR600(s) are powered-on (PL activated) without any Power consumption: 5.688 W @ Vin = 24V, 25°C, enable one TR600 on Slot A, TR600(s) are powered-on (PL activated) without any Power consumption: 5.888 W @ Vin = 32V, 25°C, enable one TR600 on Slot A, TR600(s) are powered-on (PL activated) without any Data interface: SpaceWire Data interface: USB @ (variant 2) Data interface: I2C @ (variant 3) Data interface: CAN @ (variant 4) Flight heritage: Flight heritage Connector: SMPM RF connectors Connector: Harwin Gecko G125-MH10605L1R @ (variant 2) Connector: Harwin Gecko G125-MH12005L1R @ (variant 3) Connector: Gecko G125-MH11005L1R @ (variant 4) ## NanoDock SDR (MK2) — GomSpace [sdr-modems] https://newspacemarket.com/products/nanodock-sdr-mk2/ Operating temperature: -20 °C (min) Operating temperature: 85 °C (max) Survival temperature: -20 °C (min) Survival temperature: 85 °C (max) Mass: 74.2 g Supply voltage: 4 (min) Supply voltage: 6.5 (max) Operating temperature: -20 °C (min) @ (variant 2) Operating temperature: 85 °C (max) @ (variant 2) Survival temperature: -20 °C (min) @ (variant 2) Survival temperature: 85 °C (max) @ (variant 2) Supply voltage: 4.5 (min) @ (variant 2) Supply voltage: 5.5 (max) @ (variant 2) Power consumption: 2.25 W (min) @ max power consumption Power consumption: 3.3 W (max) @ max power consumption Data rate: 3000 kbps (max) @ RS422 Data rate: 1000 kbps (max) @ CAN Mass: 76.4 g @ (variant 2) ## Software Defined Radio (MK2) — GomSpace [sdr-modems] https://newspacemarket.com/products/software-defined-radio-mk2/ Mass: 271 g @ Collective mass (NanoDock, Z7000, 1 TR-600 and 2 slot shields) Operating temperature: -40 °C (min) Operating temperature: 85 °C (max) Survival temperature: -40 °C (min) Survival temperature: 85 °C (max) Frequency: 70 MHz (min) @ NanoCom TR-600 Frequency: 6000 MHz (max) @ NanoCom TR-600 Data interface: USB Data interface: RS-422 @ (variant 2) Data interface: I2C @ (variant 3) Data interface: CAN @ (variant 4) Data interface: LVDS @ (variant 5) Data interface: UART @ (variant 6) Supply voltage: 5 (nominal) @ J16-EPS ## AX-60-S02190 CCSDS TM/TC Modem — WORK Microwave [sdr-modems] https://newspacemarket.com/products/ax-60-s02190-ccsds-tm-tc-modem/ Frequency: 950-2150 MHz @ TX Signal output L-band TX power: 0-0.001 W @ Output power Modulation: BPSK @ CCSDS 231.0 Modulation Modulation: QPSK @ CCSDS 231.0 Modulation (variant 2) Modulation: QPSK @ DVB-S2X Modulation (normal FEC frame) Modulation: 8PSK @ DVB-S2X Modulation (normal FEC frame) (variant 2) Modulation: 16APSK @ DVB-S2X Modulation (normal FEC frame) (variant 3) Modulation: 32APSK @ DVB-S2X Modulation (normal FEC frame) (variant 4) Modulation: 64APSK @ DVB-S2X Modulation (normal FEC frame) (variant 5) Modulation: 128PSK @ DVB-S2X Modulation (normal FEC frame) (variant 6) Modulation: 256PSK @ DVB-S2X Modulation (normal FEC frame) (variant 7) Modulation: QPSK @ DVB-S2X Modulation (short FEC frame) Modulation: 8PSK @ DVB-S2X Modulation (short FEC frame) (variant 2) Modulation: 16APSK @ DVB-S2X Modulation (short FEC frame) (variant 3) Modulation: 32APSK @ DVB-S2X Modulation (short FEC frame) (variant 4) Modulation: 16APSK @ DVB-S2X Modulation linear (normal FEC frame) Modulation: 32APSK @ DVB-S2X Modulation linear (normal FEC frame) (variant 2) Modulation: 64APSK @ DVB-S2X Modulation linear (normal FEC frame) (variant 3) Modulation: 256PSK @ DVB-S2X Modulation linear (normal FEC frame) (variant 4) Modulation: QPSK @ DVB-S2 Modulation (normal and short FEC frame) Modulation: 8PSK @ DVB-S2 Modulation (normal and short FEC frame) (variant 2) Modulation: 16APSK @ DVB-S2 Modulation (normal and short FEC frame) (variant 3) Modulation: 32APSK @ DVB-S2 Modulation (normal and short FEC frame) (variant 4) Protocols / waveforms: CCSDS 231.0-B-3 TC Protocols / waveforms: CCSDS 131.0-B-3 TM @ (variant 2) Protocols / waveforms: DVB-S2X - ETSI EN 302 307-2 @ (variant 3) Protocols / waveforms: DVB-S2 - ETSI EN 302 307-1 @ (variant 4) Protocols / waveforms: CCSDS 131.3-B-1 CADU frames over DVB-S2 @ (variant 5) Frequency: 950-2150 MHz @ RX Signal input L-band Frequency: 680-2300 MHz @ RX Signal input L-band w/ licenses RXL680 and RXL2300 RX sensitivity: -70--10 @ Input power Modulation: BPSK @ CCSDS 131.0 Modulation Modulation: QPSK @ CCSDS 131.0 Modulation (variant 2) Modulation: OQPSK @ CCSDS 131.0 Modulation (variant 3) Modulation: QPSK @ DVB-S2X Modulation (normal FEC frame) (variant 8) Modulation: 8PSK @ DVB-S2X Modulation (normal FEC frame) (variant 9) Modulation: 16APSK @ DVB-S2X Modulation (normal FEC frame) (variant 10) Modulation: 32APSK @ DVB-S2X Modulation (normal FEC frame) (variant 11) Modulation: 64APSK @ DVB-S2X Modulation (normal FEC frame) (variant 12) Modulation: 128PSK @ DVB-S2X Modulation (normal FEC frame) (variant 13) Modulation: 256PSK @ DVB-S2X Modulation (normal FEC frame) (variant 14) Modulation: QPSK @ DVB-S2X Modulation (short FEC frame) (variant 5) Modulation: 8PSK @ DVB-S2X Modulation (short FEC frame) (variant 6) Modulation: 16APSK @ DVB-S2X Modulation (short FEC frame) (variant 7) Modulation: 32APSK @ DVB-S2X Modulation (short FEC frame) (variant 8) Modulation: 16APSK @ DVB-S2X Modulation linear (normal FEC frame) (variant 5) Modulation: 32APSK @ DVB-S2X Modulation linear (normal FEC frame) (variant 6) Modulation: 64APSK @ DVB-S2X Modulation linear (normal FEC frame) (variant 7) Modulation: 256PSK @ DVB-S2X Modulation linear (normal FEC frame) (variant 8) Modulation: QPSK @ DVB-S2 Modulation (normal and short FEC frame) (variant 5) Modulation: 8PSK @ DVB-S2 Modulation (normal and short FEC frame) (variant 6) Modulation: 16APSK @ DVB-S2 Modulation (normal and short FEC frame) (variant 7) Modulation: 32APSK @ DVB-S2 Modulation (normal and short FEC frame) (variant 8) Data interface: Ethernet @ Data network Data interface: Ethernet @ M&C network Connector: N female @ TX Signal output L-band Connector: 1x F female @ RX Signal input L-band Connector: Ethernet RJ-45 @ Data network Connector: Ethernet RJ-45 @ M&C network Connector: BNC female @ 10 MHz reference input w/ option RI Connector: DSUB-9 female @ Alarm w/ option RI Operating temperature: 0-50 °C @ Operating Operating temperature: -30-60 °C @ Operating w/ option EXT Survival temperature: -30-80 °C @ Storage Supply voltage: 100-240 (nominal) @ Mains power Input Supply voltage: 90-264 (max) @ Mains power Input Power consumption: 45 W @ typical Envelope (L×W×H): 483 x 44 x 505 mm³ (WxHxD) Mass: 10000 g @ approx, up to, depending on device type ## QUASAR-STRX — AAC Clyde Space [sdr-modems] https://newspacemarket.com/products/aac-quasar-strx/ Design lifetime: 3 years (min) Design lifetime: 5 years (max) Mass: 250 g (max) Data interface: I2C @ currently supported Data interface: CAN @ under development Data interface: SPI @ under development (variant 2) Power consumption: 3.4 W @ receive mode (always on) Connector: SMP Design lifetime: 3 years TX power: 0.501 W TX power: 1 W @ (variant 2) TX power: 1.995 W @ (variant 3) Power consumption: 9 W @ TX Modulation: Filtered (O)QPSK @ TX Data rate: 1024 kbps (max) @ TX Protocols / waveforms: TM Synchronization and Channel Coding (CCSDS 131.0-B-3) @ TX Protocols / waveforms: TM Space Data Link Protocol (CCSDS 132.0 B 3) @ TX (variant 2) Envelope (L×W×H): 93 x 88 x 24 mm Data rate: 32 kbps @ RX BPSK Data rate: 64 kbps @ RX QPSK RX sensitivity: -150 + 10*log(symbol rate) dBm Power consumption: 3.4 W @ RX Modulation: Filtered BPSK @ RX Protocols / waveforms: TC Synchronization and Channel Coding (CCSDS 231.0-B-4) @ RX Protocols / waveforms: TC Space Data Link Protocol (CCSDS 232.0 B 4) @ RX (variant 2) Protocols / waveforms: TM Synchronization and Channel Coding (CCSDS 131.0-B-3) @ RX (variant 3) Protocols / waveforms: TM Space Data Link Protocol (CCSDS 132.0 B 3) @ RX (variant 4) ## C7700 Desktop HTS Broadband VSAT Router — SpaceBridge Inc. [sdr-modems] https://newspacemarket.com/products/c7700/ Protocols / waveforms: DVB-S2/S2X ACM @ Forward Link Protocols / waveforms: MF-TDMA @ Return Link ASAT-II Protocols / waveforms: BM-FDMA or MF-TDMA @ Return Link Estella Modulation: QPSK to 256APSK @ Forward Link Modulation: QPSK, 8PSK, 16QAM @ Return Link ASAT-II Modulation: BPSK, QPSK, 8PSK, 16QAM, 32QAM, 64QAM @ Return Link Estella TX power: 0 W (min) TX power: 0.001 W (max) Data rate: 120000 kbps @ Download speed Data rate: 20000 kbps @ Upload Speed Envelope (L×W×H): 2” x 7.25” x 5” (51 x 182 x 127 mm) Mass: 340 g Power consumption: 12 W @ not including RF equipment / BUC power Supply voltage: 95 (min) @ External universal power supply Supply voltage: 240 (max) @ External universal power supply Power consumption: 65 W @ External universal power supply Operating temperature: 0 °C (min) Operating temperature: 50 °C (max) Frequency: 950 MHz (min) @ Terminal IF RX Interface Frequency: 2150 MHz (max) @ Terminal IF RX Interface Frequency: 950 MHz (min) @ Terminal IFL TX Interface Frequency: 2400 MHz (max) @ Terminal IFL TX Interface Data interface: Ethernet @ User ports Data interface: Ethernet @ MGMT ports ## MOD1250 DVB-S2X Wideband Modulator — SpaceBridge Inc. [sdr-modems] https://newspacemarket.com/products/mod1250-dvb-s2x-wideband-modulator/ Modulation: DVB-S2X ACM, QPSK up to 256APSK Protocols / waveforms: DVB-S2X Data rate: 3000000 kbps @ Data throughput TX power: 0.003 W (max) Frequency: 950 MHz (min) Frequency: 2150 MHz (max) Data interface: Ethernet @ Data Input Ports (2x 10 GbE) Data interface: Ethernet @ Management Interface (2x 1 GbE) Connector: BNC @ Timing and Frequency Connector: N-type(F) @ Output Connector: SMA (F) @ L-band Monitor Mass: 4000 g Envelope (L×W×H): 435 x 44 (1RU) x 458 mm (W x H x D) Power consumption: 60 W Operating temperature: 0 °C (min) Operating temperature: 55 °C (max) ## XRF-33F/XRF-34F High-Value Ka-Band VSAT Transceiver — SpaceBridge Inc. [sdr-modems] https://newspacemarket.com/products/xrf-33f-xrf-34f-high-value-ka-band-vsat-transceiver/ TX power: 3 W @ XRF33F TX power: 4 W @ XRF34F Supply voltage: 18 (min) @ TX Subsystem Supply voltage: 50 (max) @ TX Subsystem Supply voltage: 18 (min) @ Rx Subsystem Supply voltage: 22 (max) @ Rx Subsystem Power consumption: 25 W @ XRF33F Power consumption: 40 W @ XRF34F Power consumption: 4 W @ Rx Subsystem Frequency: 1400 MHz (min) @ TX IF Input Frequency: 2400 MHz (max) @ TX IF Input Frequency: 29000 MHz (min) @ TX RF Output Frequency: 30000 MHz (max) @ TX RF Output Frequency: 17800 MHz (min) @ RX RF Input Frequency: 20200 MHz (max) @ RX RF Input Frequency: 950 MHz (min) @ RX IF Output Frequency: 2150 MHz (max) @ RX IF Output Operating temperature: -40 °C (min) Operating temperature: 55 °C (max) Mass: 1100 g @ Including feed Envelope (L×W×H): 208LLx100Hx49W ## NanoCom TR-600 — GomSpace [sdr-modems] https://newspacemarket.com/products/nanocom-tr-600/ Frequency: 70 MHz (min) Frequency: 6000 MHz (max) TX power: 0.004 W @ approximate, 1 GHz to 5 GHz, 0 dB attenuation TX power: 0.001 W @ approximate, 6 GHz, 0 dB attenuation Protocols / waveforms: TDD Protocols / waveforms: FDD @ (variant 2) Mass: 16.8 g @ PCB Mass: 65.3 g @ PCB + shield Envelope (L×W×H): 65.0 x 40.0 x 14.8 mm Supply voltage: 4.5 (min) Supply voltage: 5.5 (max) Data interface: SPI Data interface: LVDS @ (variant 2) Data interface: I2C @ (variant 3) Connector: Molex SSMCX EDGE 73415-4670 Connector: Samtec LSHM-150-04.0-L-DV-A-S-K-TR @ (variant 2) Operating temperature: -40 °C (min) @ TRX IC Operating temperature: 85 °C (max) @ TRX IC Flight heritage: Flight proven ## Expedite — Remos Space Systems AB [sdr-modems] https://newspacemarket.com/products/expedite/ Modulation: BPSK Modulation: QPSK @ (variant 2) Modulation: oQPSK @ (variant 3) Modulation: FSK @ (variant 4) Modulation: GMSK @ (variant 5) Modulation: AFSK @ (variant 6) Modulation: ASK @ (variant 7) Modulation: GFSK @ (variant 8) Modulation: PCM/PM @ (variant 9) Modulation: PCM/PSK/PM @ (variant 10) Protocols / waveforms: CCSDS CADU Protocols / waveforms: CLTU @ (variant 2) Protocols / waveforms: AX.25 @ (variant 3) Protocols / waveforms: HDLC @ (variant 4) Protocols / waveforms: AirMac @ (variant 5) Protocols / waveforms: RAW @ (variant 6) Protocols / waveforms: CSP @ (variant 7) Protocols / waveforms: Satlab @ (variant 8) Protocols / waveforms: CCSDS Space Link Extension (SLE) @ (variant 9) Protocols / waveforms: PLOP-1 @ (variant 10) Protocols / waveforms: PLOP-2 @ (variant 11) Mass: 16000 g Envelope (L×W×H): 177 × 482 × 555 mm Supply voltage: 230 @ AC supply Power consumption: 500 W @ maximum consumption Data interface: TCP/IP Data interface: REST @ (variant 2) Data interface: WebSocket @ (variant 3) Data interface: ZeroMQ @ (variant 4) Data interface: other @ serial drive Connector: SMA female, 50 Ω ## AX-60/AX-61 IP Modem — WORK Microwave [sdr-modems] https://newspacemarket.com/products/ax-60-ax-61-ip-modem/ Frequency: 950-2150 MHz @ Signal output L-band Frequency: 50-180 MHz @ Signal output 70/140 MHz w/ options IF50 or IF75 Frequency: 950-2150 MHz @ Signal input L-band Frequency: 680-2300 MHz @ Signal input L-band w/ licenses RXL680 and RXL2300 Frequency: 50-180 MHz @ Signal input 70/140 MHz w/ options IF50 or IF75 Data rate: 360000 kbps @ up to, integrated TX power: 0 W (min) @ Signal output L-band TX power: 0.001 W (max) @ Signal output L-band TX power: 0 W (min) @ Signal output 70/140 MHz w/ options IF50 or IF75 TX power: 0.003 W (max) @ Signal output 70/140 MHz w/ options IF50 or IF75 RX sensitivity: -70 (min) @ Signal input L-band RX sensitivity: -10 (max) @ Signal input L-band RX sensitivity: -60 (min) @ Signal input 70/140 MHz w/ options IF50 or IF75 RX sensitivity: 15 (max) @ Signal input 70/140 MHz w/ options IF50 or IF75 Modulation: QPSK to 256APSK normal, short, linear @ DVB-S2X Modulation: QPSK to 32APSK; normal, short @ DVB-S2 Protocols / waveforms: DVB-S2X/S2/S Mass: 10000 g (max) @ depending on device type Envelope (L×W×H): 483 x 44 x 505 mm³ (WxHxD) Supply voltage: 90-264 @ AC max Power consumption: 45 W @ typical Data interface: Ethernet @ Data network Data interface: Ethernet @ M&C network Connector: N female @ Signal output L-band Connector: BNC female @ Signal output 70/140 MHz w/ options IF50 or IF75 Connector: 1x F female @ Signal input L-band Connector: 1x BNC female @ Signal input 70/140 MHz w/ options IF50 or IF75 Connector: RJ-45 @ Data network, M&C network Connector: BNC female @ 10 MHz reference input w/ option RI Connector: DSUB-9 female @ Alarm w/ option RI Connector: IEC C14 @ Mains power Operating temperature: 0-50 °C @ Operating Operating temperature: -30-60 °C @ Operating w/ option EXT Survival temperature: -30-80 °C @ Storage ## AX-80 Wideband Modem — WORK Microwave [sdr-modems] https://newspacemarket.com/products/ax-80-wideband-modem/ Frequency: 950 MHz (min) @ TX Signal output L-band Frequency: 2150 MHz (max) @ TX Signal output L-band Frequency: 950 MHz (min) @ RX Signal input L-band Frequency: 2150 MHz (max) @ RX Signal input L-band Data rate: 3000000 kbps (max) @ per direction TX power: 0 W (min) @ TX Signal output L-band TX power: 0.001 W (max) @ TX Signal output L-band RX sensitivity: -55 (min) @ RX Signal input L-band, total aggregate power RX sensitivity: -10 (max) @ RX Signal input L-band, total aggregate power Modulation: QPSK to 256APSK normal, short, linear @ DVB-S2X Modulation: QPSK to 32APSK; normal, short @ DVB-S2 Modulation: QPSK, 8PSK, 16APSK, 32APSK, 64APSK, 128APSK, 256APSK @ DVB-S2X, normal FEC frame Modulation: QPSK, 8PSK, 16APSK, 32APSK @ DVB-S2X, short FEC frame Modulation: 8PSK, 16APSK, 32APSK, 64APSK, 256APSK @ DVB-S2X, linear normal FEC frame Modulation: QPSK, 8PSK, 16APSK, 32APSK @ DVB-S2, normal and short FEC frame (9/10 normal FEC frame only) Protocols / waveforms: DVB-S2X - ETSI EN 302 307-2 Protocols / waveforms: DVB-S2 - ETSI EN 302 307-1 @ (variant 2) Protocols / waveforms: GSE and MPE encapsulation @ (variant 3) Protocols / waveforms: DVB-CID according to ETSI TS 103129 @ (variant 4) Protocols / waveforms: Generic Stream Encapsulation (GSE) according to ETSI TS 102606 @ (variant 5) Protocols / waveforms: Multiprotocol Encapsulation (MPE) according to ETSI EN 301192 @ (variant 6) Protocols / waveforms: RTP/UDP/IP over Ethernet according to IETF RFC 2250 @ Stream inputs Protocols / waveforms: RTP/UDP/IP over Ethernet according to IETF RFC 2250 @ Stream outputs Protocols / waveforms: CCSDS CADU frames @ (variant 7) Protocols / waveforms: SNMP @ Remote monitoring and control Protocols / waveforms: HTTP web browser interface @ Remote monitoring and control (variant 2) Mass: 14000 g (max) @ depending on device type Envelope (L×W×H): 483 x 89 x 505 mm³ (WxHxD) Supply voltage: 90 (min) @ Mains power input Supply voltage: 264 (max) @ Mains power input Power consumption: 150 W (nominal) @ typical Data interface: Ethernet @ Data network Data interface: Ethernet @ M&C network Connector: N female @ TX Signal output L-band Connector: N female / SMA female adapter @ RX Signal input L-band Connector: RJ-45 @ Data network Connector: SFP+ adapter slot @ Data network (variant 2) Connector: RJ-45 @ M&C network Connector: BNC female @ Reference input Connector: BNC female @ 1 PPS input Connector: DSUB-9 female @ Alarm Connector: BNC female @ Reference Input w/ option RI Connector: IEC C14 @ Mains power Operating temperature: 0 °C (min) Operating temperature: 50 °C (max) Survival temperature: -30 °C (min) Survival temperature: 80 °C (max) ## Q8RFG3 Gen 3 RFSoC Processor — Xiphos Technologies [sdr-modems] https://newspacemarket.com/products/xiphos-q8rfg3/ Frequency: 6000 MHz (max) @ RF Input Mass: 200 g Envelope (L×W×H): 100 mm x 100 mm x 20 mm Supply voltage: 5-15 Power consumption: 25-35 W @ typ. Data interface: LVDS Data interface: GPIO @ (variant 2) Data interface: PCIe Gen 3 @ (variant 3) Data interface: 100G Ethernet @ (variant 4) Data interface: PCIe Gen 2 @ (variant 5) Data interface: SATA @ (variant 6) Operating temperature: -40-60 °C @ Derated Radiation tolerance (TID): 30 krad ## DIGITAL 1000 – RF over IP Digitiser — ETL Systems [sdr-modems] https://newspacemarket.com/products/digital-1000-rf-over-ip-digitiser/ Frequency: 850 MHz (min) Frequency: 2450 MHz (max) Protocols / waveforms: IEEE-ISTO Std 4900-2021 (DIFI) Information Class 0x0000, 0x0002, 0x0003, 0x0004 Data interface: Ethernet Connector: RF: 50Ω SMA 1PPS: 50Ω SMA 10MHz: 50Ω SMA Connector: Sample Data: SFP+ @ (variant 2) Connector: Control: RJ45 @ (variant 3) TX power: 0 W @ 1dB GCP Supply voltage: 12 (min) Supply voltage: 24 (max) Power consumption: 50 W @ Full load, max. consumption at steady rate Operating temperature: 0 °C (min) Operating temperature: 40 °C (max) Survival temperature: -20 °C (min) Survival temperature: 60 °C (max) Mass: 490 g Envelope (L×W×H): 215mm x 85mm x 40mm (excluding cooling fans) ## Satellite Modulator OEM Module — WORK Microwave [sdr-modems] https://newspacemarket.com/products/satellite-modulator-oem-module/ Data rate: 213000 kbps @ max per ASI Interface Data rate: 170000 kbps @ max, BISS-1/E active Modulation: QPSK / 8PSK / 16APSK / 32APSK / 64APSK / 128APSK / 256APSK (normal, short and linear) @ DVB-S2X Modulation: QPSK / 8PSK / 16APSK / 32APSK (normal, short) @ DVB-S2 Modulation: QPSK / 8PSK / 16QAM @ DVB-S and DVB-DSNG Protocols / waveforms: DVB-S2X - ETSI EN 302 307-2, DVB-S2 - ETSI EN 302 307-1, DVB-DSNG - ETSI EN 301 210, DVB-S - ETSI EN 300 421 Protocols / waveforms: DVB Carrier ID - ETSI TS 103 129 @ (variant 2) Protocols / waveforms: BISS-E encryption @ (variant 3) Envelope (L×W×H): 185 x 17 x 100 mm³ (WxHxD) @ standard module Envelope (L×W×H): 185 x 25 x 100 mm³ (WxHxD) @ with cables and/or option EXT Mass: 450000 g @ approx Power consumption: 14 W @ Standard, typ. Power consumption: 17 W @ Option EXT, typ. Data interface: ASI Data interface: RS232 @ (variant 2) Connector: SMA female Connector: MCX female @ Transport Stream Inputs Connector: 2.54 mm pin header @ Monitoring and Control Interface Connector: 2.54mm pin header @ Mains Power Input ## AR-60/AR-61 IP Demodulator — WORK Microwave [sdr-modems] https://newspacemarket.com/products/ar-60-ar-61-ip-demodulator/ Warranty: 3 Protocols / waveforms: DVB-S2X Protocols / waveforms: DVB-S2 @ (variant 2) Protocols / waveforms: DVB-S @ (variant 3) Modulation: QPSK to 256APSK @ DVB-S2X normal, short, linear Modulation: QPSK to 32APSK @ DVB-S2 normal, short Data rate: 360000 kbps Frequency: 950-2150 MHz @ Signal input L-band Frequency: 680-2300 MHz @ Signal input L-band w/ licenses RXL680 and RXL2300 Connector: 1x F female @ Signal input L-band RX sensitivity: -70 (min) @ Input power, Signal input L-band RX sensitivity: -10 (max) @ Input power, Signal input L-band Frequency: 50-180 MHz @ Signal input 70/140 MHz w/ option IF Connector: 1x BNC female @ Signal input 70/140 MHz w/ option IF RX sensitivity: -60 (min) @ Input power, Signal input 70/140 MHz w/ option IF RX sensitivity: 15 (max) @ Input power, Signal input 70/140 MHz w/ option IF Protocols / waveforms: DVB-S2X @ ModCods Protocols / waveforms: DVB-S2 @ ModCods (variant 2) Protocols / waveforms: DVB-S @ ModCods (variant 3) Data interface: Ethernet @ Data network Connector: 1x Ethernet RJ-45 @ Data network Data interface: Ethernet @ M&C network Connector: 1x Ethernet RJ-45 @ M&C network Connector: BNC female @ 10 MHz reference input w/ option RT Connector: SMC male, 26 pin @ RX time stamp synchronization w/ option RT Data rate: 360000 kbps (max) @ IP data rate limits Data interface: Ethernet @ RTP/UDP/IP over Ethernet Protocols / waveforms: CCSDS @ CCSDS CADU frames Operating temperature: 0-50 °C Operating temperature: -30-60 °C @ w/ option EXT Survival temperature: -30-80 °C Supply voltage: 100-240 @ AC nominal Supply voltage: 90-264 @ AC max Power consumption: 45 W @ typical Connector: IEC C14 @ Mains power Envelope (L×W×H): 483 x 44 x 505 mm³ (WxHxD) Mass: 10000 g (max) @ depending on device type ## Propulsion Tanks — Northrop Grumman Space Systems [tanks-valves] https://newspacemarket.com/products/northrop-grumman-propulsion-tanks/ Flight heritage: 60+ years of proven performance, visited every planet in the Solar System, even the Sun, and zero on-orbit failures. 7,000+ tanks produced. ## Check Valves and Relief Valves — VACCO Industries [tanks-valves] https://newspacemarket.com/products/vacco-check-relief-valves-spacecraft/ Operating temperature: -170-45 °C Operating pressure (MEOP): 37.9212 bar Mass: 20 g Design lifetime: 10 years Flight heritage: Successful Flight Heritage ## Tanques soldados por Friction Stir Welding (FSW) — VENG S.A. [tanks-valves] https://newspacemarket.com/products/veng-fsw-structural-tanks/ Material: Aleaciones de aluminio Material: aluminio 2219 de uso espacial @ (variant 2) Envelope (L×W×H): 3,5 metros de longitud, 2,5 metros de diámetro y 3,2 milímetros de espesor ## Bradford Standard Accuracy Pressure Transducer — Bradford Space [tanks-valves] https://newspacemarket.com/products/bradford-standard-pressure-transducer/ Media / propellant: Hydrazine, MON, MMH, Green Propellant, IPA, GHe, GN2, GXe, Deionized H2O Operating pressure (MEOP): 320 bar (max) Material: Ti6Al4V and/or AISI 316L/304L Mass: 230 g (max) @ excluding cable Envelope (L×W×H): 126 (for 30mm stub tube) x 77 x 43.5mm Supply voltage: 15 to 28 V Power consumption: 0.3 W (max) Operating temperature: -20˚ to +70˚C Survival temperature: -40˚ to +75˚C Radiation tolerance (TID): 100 krad Design lifetime: 18 years Flight heritage: Galileo IOV, GB2, GOCE, Planck, Rosetta, ATV, PRISMA, AMOS3, Cygnus CRS, O3b, SWARM, Sentinel, Galileo FOC, IVX, ExoMars 2016 TGO, Microscope, SmallGEO, Venµs, BepiColombo, GOSAT-2, STPSat-5, SkySat ## Bradford Miniaturised Pressure Transducer — Bradford Space [tanks-valves] https://newspacemarket.com/products/bradford-mini-pressure-transducer/ Media / propellant: Hydrazine, MON, MMH, LMP-103S, Ammonia, IPA, GHe, GN2, GXe, Deionized H2O Operating pressure (MEOP): 320 bar (max) Material: Ti6Al4V and/or AISI 316L/304L Mass: 125 g (max) @ excluding cable Envelope (L×W×H): 84.6 (for 30mm stub tube) x 72 x 43.5 mm Supply voltage: 28 Power consumption: 0.3 W (max) @ nominal Operating temperature: -40-75 °C Survival temperature: -50-75 °C Radiation tolerance (TID): 100 krad Design lifetime: 18 years Flight heritage: 200+ units in space ## Coarse Sun Sensor (Cosine Type) — Adcole Space (Redwire) [sun-sensors] https://newspacemarket.com/products/adcole-coarse-sun-sensor-cosine-type/ Mass: 10 g @ NOMINAL Envelope (L×W×H): 2.8 CM X 1.9 CM X 1.2 CM Radiation tolerance (TID): 100 krad @ > Flight heritage: GRAIL, Mars Phoenix, GPM, GPIM, LRO/LCROSS, WISE, Kepler, SDO, EMM (Hope), Worldview, Fermi (GLAST), MRO, Deep Impact, Swift, Classified Programs ## Fine Sun Sensor — Adcole Space (Redwire) [sun-sensors] https://newspacemarket.com/products/adcole-fine-sun-sensor/ Field of view: 100 @ x 100° (each sensor) Accuracy: 0.01 ° (min) Accuracy: 0.05 ° (max) Flight heritage: Adcole Fine Sun Sensors have flown on more than 100 spacecraft ## Fine Spinning Sun Sensor (±64°) — Adcole Space (Redwire) [sun-sensors] https://newspacemarket.com/products/adcole-fine-spinning-sun-sensor/ Field of view: 64 @ half-angle, Fan-shaped (each sensor) Accuracy: 0.1 ° @ Sun Pulse at 0° Accuracy: 0.3 ° @ Sun Pulse at 40° Accuracy: 0.6 ° @ Sun Pulse at 64° Accuracy: 0.1 ° @ Aspect Angle 0° to 40° Accuracy: 0.25 ° @ Aspect Angle 40° to 64° Envelope (L×W×H): 66×33×25 mm @ Sensor Envelope (L×W×H): 51×82×89 mm @ Electronics Mass: 109 g (nominal) @ Sensor Mass: 475 g (min) @ Electronics Mass: 725 g (max) @ Electronics Supply voltage: 28 (nominal) Supply voltage: 21 (min) Supply voltage: 35 (max) Power consumption: 0.4 W @ Typical power dissipation Output type: analog @ Sun Pulse (one per revolution) Output type: digital @ Parallel Coarse Data Output type: analog @ Fine Data (Vsine, Vcosine, Vbias) Flight heritage: ERG, BSAT-2, IMAGE, INDOSTAR, KOREASAT, INMARSAT, GPS IIR, GGS, AURORA, GEOTAIL, DBS, MST5, VIKING, SAN MARCOS, SCATHA, ISEE-C, TELSAT, BSE, SATCOM. all Mars Rovers, New Horizons, Juno, and the Parker Solar Probe. ## SpaceTech CESS (Coarse Earth Sun Sensor) — SpaceTech GmbH [sun-sensors] https://newspacemarket.com/products/spacetech-cess/ Envelope (L×W×H): 108 x 42 x 58 mm³ Mass: 80 g Connector: 26 Pin HD D-Sub Connector Survival temperature: 5 °C Flight heritage: GRACE, CHAMP, CryoSat-2 Flight heritage: CHAMP, GRACE, Terra-SAR-X, TanDEM-X, Paz, CryoSat-2, SWARM @ (variant 2) Accuracy: 7.3 ° @ Earth 68% Accuracy: 19 ° @ Earth 99% Accuracy: 25 ° @ Earth 99.9% Accuracy: 4.4 ° @ Sun 68% Accuracy: 10.6 ° @ Sun 99% Accuracy: 13 ° @ Sun 99.9% Design lifetime: 15 years ## FDSS Fine Digital Sun Sensor — Solar MEMS Technologies [sun-sensors] https://newspacemarket.com/products/solar-mems-fdss/ Field of view: 140 @ x Field of view: 140 @ y Accuracy: 0.1 ° @ Better than Output type: digital Data interface: RS-232 Connector: nanoD connector Supply voltage: 5 @ nominal Power consumption: 2 W @ consumption Envelope (L×W×H): 70 x 60 x 40 mm Mass: 170 g Operating temperature: -30 °C (min) Operating temperature: 70 °C (max) Radiation tolerance (TID): 20 krad Flight heritage: COTS camera with space heritage and space grade parts ## Cubesat Sun Sensor — SSBV Aerospace & Technology [sun-sensors] https://newspacemarket.com/products/ssbv-cubesat-sun-sensor/ Field of view: 114 Update rate: 10 Hz @ > Accuracy: 0.5 ° @ < Mass: 5 g @ < Envelope (L×W×H): 33mm x 11mm x 6mm Operating temperature: -25-50 °C Radiation tolerance (TID): 10 krad Supply voltage: 5 Output type: analog Data interface: other @ analogue channels Connector: 9-way Nano-D Flight heritage: The Cubesat Sun-sensor will fly on the TDS-1 satellite in 2012 and two other cubesats in 2013. ## Bradford Fine Sun Sensor (FSS) — Bradford Space [sun-sensors] https://newspacemarket.com/products/bradford-fine-sun-sensor-fss/ Mass: 375 g @ per sensor unit Envelope (L×W×H): <108 x 108 x 52.5 mm, including all protrusions by mounting feet, connectors, alignment cube and bondpin, exclusive dowel pins. Floor space: 104 x 94 mm Field of view: 128 @ Nominal FOV, COTS sensor version Field of view: 138 @ Unobstructed FOV Accuracy: 0.3 ° @ EOL Bias error, whole 128° x 128° FOV Accuracy: 0.03 ° @ Resolution Accuracy: 0.05 ° @ Noise equivalent angle Output type: analog @ quadrant outputs, sun presence output Power consumption: 0.25 W (max) @ from ±15 V secondary power Radiation tolerance (TID): 10 krad @ active element accumulated dose, with shielding (>3 mm of cover glass thickness) Radiation tolerance (TID): 100 krad @ EEE parts rad tolerance, with shielding (>7.5 mm aluminium) Design lifetime: 5 years @ Reliability for 5 years in orbit for a single unit ## Bradford Mini Fine Sun Sensor (Mini FSS) — Bradford Space [sun-sensors] https://newspacemarket.com/products/bradford-mini-fine-sun-sensor/ Mass: 50 g Envelope (L×W×H): 50 x 46 x 17 mm Field of view: 128 @ Nominal FOV Field of view: 172 @ Unobstructed FOV Accuracy: 1.5 ° @ Without on-board implementation of look-up table Accuracy: 0.2 ° @ With on-board implementation of look-up table Output type: analog Operating temperature: -50-80 °C ## Advanced Coarse Sun Sensor (ACSS) — Solar MEMS Technologies [sun-sensors] https://newspacemarket.com/products/solar-mems-acss-coarse-sun-sensor/ Flight heritage: since 2019 with hundreds of flight units delivered Operating temperature: -55 to 105º Celsius Radiation tolerance (TID): 200 krad @ (gamma) Flight heritage: more than 2500 units in orbit since 2019 @ (variant 2) Field of view: 60 @ half-angle Output type: analog Connector: 15-pin micro connector Supply voltage: 15 (min) Supply voltage: 30 (max) Operating temperature: -45º to 85º Celsius @ (variant 2) Envelope (L×W×H): 65 x 47 x 13 mm Mass: 40 g ## VANTAGESun — Voyager Technologies [sun-sensors] https://newspacemarket.com/products/voyager-vantagesun/ Accuracy: 5 ° (max) @ over full FoV Field of view: 120 (max) @ Full Angle Circular Mass: 10 g (max) @ including flying leads Envelope (L×W×H): Housing Diameter: 12.70mm; Flange Diameter: 22.86mm; Sensor Height: 8.99mm Connector: Two flying leads, 1.27m (50”) length M22759/33-26 26 AWG wire Operating temperature: -40-100 °C Survival temperature: -55-125 °C Flight heritage: more than 20 years of spaceflight heritage ## nanoSSOC A60 — Solar MEMS Technologies [sun-sensors] https://newspacemarket.com/products/solar-mems-nanossoc-a60/ Operating temperature: -30-85 °C Radiation tolerance (TID): 100 krad @ gamma Radiation tolerance (TID): 3000 krad @ protons (6 MeV) Flight heritage: since 2016 with hundreds of units in orbit. Field of view: 60 @ pm Output type: analog Connector: 10-pin micro-connector Supply voltage: 3.3-5 Envelope (L×W×H): 27.4 x 14 x 5.9 mm Mass: 4 g ## nanoSSOC-D60 — Solar MEMS Technologies [sun-sensors] https://newspacemarket.com/products/solar-mems-nanossoc-d60/ Field of view: 60 @ half-angle Data interface: UART Data interface: I2C @ (variant 2) Data interface: SPI @ (variant 3) Connector: 10-pin micro-connector Supply voltage: 3.3 (nominal) Supply voltage: 5 (nominal) @ (variant 2) Mass: 6.5 g (typical) Envelope (L×W×H): 43 x 14 x 5.9 mm Operating temperature: -30 °C (min) Operating temperature: 85 °C (max) Radiation tolerance (TID): 30 krad (typical) Flight heritage: since 2016 with hundreds of units in orbit. ## SSOC A60 — Solar MEMS Technologies [sun-sensors] https://newspacemarket.com/products/solar-mems-ssoc-a60/ Field of view: 60 @ pm Mass: 25 g Supply voltage: 5 (nominal) Envelope (L×W×H): 40 x 30 x 12 mm Operating temperature: -45-85 °C Radiation tolerance (TID): 100 krad (min) Flight heritage: since 2009 with hundreds of units in orbit Output type: analog ## NanoSense FSS — GomSpace [sun-sensors] https://newspacemarket.com/products/gomspace-nanosense-fss-fine-sun-sensor/ Mass: 2.2 g Envelope (L×W×H): 22 x 11 x 5 mm @ FSS casing Envelope (L×W×H): 22 x 11 x 1.3 mm @ Elevator Data interface: I2C Output type: digital Accuracy: 0.5 ° @ 3-sigma, FOV < 45°, No albedo Accuracy: 2 ° @ 3-sigma, FOV < 60°, No albedo Update rate: 100 Hz @ Max, converted from 10 ms sample period Field of view: 60 @ Half Angle ## Earth Horizon Sensor — Pyxis Space [sun-sensors] https://newspacemarket.com/products/pyxis-earth-horizon-sensor/ Accuracy: 1 ° @ rms Update rate: 1 Hz Field of view: 80 @ HxV IR Field of view: 120 @ HxV IR (variant 2) Field of view: 92 @ HxV VIS Field of view: 114 @ HxV VIS (variant 2) Data interface: CAN @ 2.0B Supply voltage: 4.5 (min) Supply voltage: 12 (max) Power consumption: 0.2 W Mass: 42 g Envelope (L×W×H): 28 x 28 x 53 mm3 Operating temperature: -20 °C (min) Operating temperature: 50 °C (max) Radiation tolerance (TID): 10 krad Data interface: I2C @ option Data interface: UART @ option (variant 2) ## Earth Horizon Sensor — Plan-S (Connecta) [sun-sensors] https://newspacemarket.com/products/earth-horizon-sensor-4217/ Accuracy: 1 ° Mass: 24 g Envelope (L×W×H): 40 x 25 x 20 mm Supply voltage: 5 (nominal) Data interface: CAN Data interface: RS-485 @ (variant 2) Connector: Molex Micro-Lock Plus ## Multiband GNSS OEM Receiver Board M-GNSSB-RX — Arralis [gnss-receivers] https://newspacemarket.com/products/arralis-m-gnssb-rx-multiband-gnss-oem-receiver-board/ Constellations: GNSS bands L1 and B1 Supply voltage: 3.3 Supply voltage: 5 @ RS485 option Envelope (L×W×H): 58mm x 58mm Supply voltage: 3.3 @ (variant 2) Supply voltage: 5 @ RS485 output Data interface: RS-485 Data interface: UART @ (variant 2) Connector: J4 Connector: J1 @ (variant 2) ## Space GNSS Receivers and GNSS Reflectometry Instruments — SSTL (Surrey Satellite Technology) [gnss-receivers] https://newspacemarket.com/products/sstl-sgr-ligo/ Envelope (L×W×H): 92 x 87 x 12 Power consumption: 0.5 W (max) @ at 5V Mass: 90 g Radiation tolerance (TID): 5 krad @ core components Operating temperature: -20-50 °C Survival temperature: -30-85 °C @ non-operating Channels: 24 Constellations: GPS L1 C/A Code, GLONASS G1 (option), Galileo E1 (option) Position accuracy: 5 m @ Under defined 680km polar orbit, Earth pointing conditions Velocity accuracy: 0.1 m/s @ Under defined 680km polar orbit, Earth pointing conditions Time to first fix (cold): 90 s @ NVRAM, Under defined 680km polar orbit, Earth pointing conditions Data interface: UART Data interface: CAN @ (variant 2) Data interface: I2C @ (variant 3) Power consumption: 0.4 W (max) @ lower power mode, 12 channel operation, at 3V3 Supply voltage: 3.3-5 Flight heritage: Due for launch on two CubeSats in 2019; Derived from SGR-Axio and SGR-ReSI with extensive flight heritage ## SGR-Axio Space GNSS Receiver — SSTL (Surrey Satellite Technology) [gnss-receivers] https://newspacemarket.com/products/sstl-sgr-axio/ Envelope (L×W×H): 160 x 180 x 50 Power consumption: 4 W @ baseline mode Supply voltage: 28 (nominal) Mass: 1000 g Radiation tolerance (TID): 5 krad @ core components tested to 10krads Operating temperature: -20-50 °C Survival temperature: -30-80 °C Channels: 24 Constellations: GPS L1 C/A Code, GLONASS G1 (option), Galileo E1 (option), GPS L2C (Option) Position accuracy: 5 m Velocity accuracy: 0.1 m/s Time to first fix (cold): 120 s @ NVRAM Data interface: RS-485 Data interface: LVDS @ (variant 2) Data interface: other @ (variant 3) Data interface: CAN @ (variant 4) Data interface: RS-422 @ (variant 5) Data interface: SpaceWire @ (variant 6) Flight heritage: In orbit on 4 satellites, first launch 2018 Flight heritage: Derived from SGR-ReSI, in orbit since 2014 @ (variant 2) ## GNSS Receiver Module (GPSRM 1) Kit — Pumpkin, Inc. [gnss-receivers] https://newspacemarket.com/products/pumpkin-gnss-receiver-module-gpsrm-1-kit/ Channels: 555 Constellations: GPS: L1 C/A, L1C, L2C, L2P, L5 Constellations: GLONASS: L1 C/A, L2 C/A, L2P, L3, L5 @ (variant 2) Constellations: Galileo: E1, E5 AltBOC, E5a, E5b, E6 @ (variant 3) Constellations: BeiDou: B1, B2, B3 @ (variant 4) Constellations: QZSS: L1 C/A, L1C, L2C, L5, L6 @ (variant 5) Constellations: NavIC: L5 @ (variant 6) Constellations: SBAS: L1, L5 @ (variant 7) Time to first fix (cold): 40 s @ Cold start (typical) Time to first fix (cold): 19 s @ Warm start (typical) Position accuracy: 1.5 m @ Position L1 (RMS) Position accuracy: 1.2 m @ Position L1/L2 (RMS) Position accuracy: 0.01 m @ Limit (w/RTK etc.) Velocity accuracy: 0.03 m/s (max) @ Velocity Update rate: 20 Hz (min) @ Measurements Update rate: 100 Hz (max) @ Measurements Update rate: 20 Hz (min) @ Position Update rate: 100 Hz (max) @ Position Data interface: UART Data interface: USB @ (variant 2) Data interface: I2C @ (variant 3) Supply voltage: 3.3 @ OEM719 nominal Power consumption: 1.2 W @ OEM719 nominal Power consumption: 1.8 W (max) @ OEM719 Supply voltage: 5 @ Active antenna available Power consumption: 1 W (max) @ Active antenna available Supply voltage: 5 @ SupMCU nominal Power consumption: 0.05 W (max) @ SupMCU nominal Flight heritage: 4x CubeSat-class LEO missions Mass: 109 g Envelope (L×W×H): 96mm W x 90mm L x 11mm H Operating temperature: -40-85 °C Supply voltage: -0.3-6 @ +5V_USB bus, +5V_SYS bus Supply voltage: -0.3-5.5 @ VCC_SYS bus, VCC_MCU bus Power consumption: 1.3 W @ Operating, Supervisor MCU & GPS active, no antenna connected Power consumption: 0.025 W @ Operating, Supervisor MCU active, GPS unpowered Data interface: USB @ (variant 4) Data interface: I2C @ (variant 5) Connector: 104-pin CSK bus connector Connector: MCX antenna input @ (variant 2) Connector: MCX PPS output @ (variant 3) Connector: MMCX VARF output @ (variant 4) ## NewSpace GNSS Receiver — Rakon Limited [gnss-receivers] https://newspacemarket.com/products/rakon-ns-gnss-receiver/ Design lifetime: 5 years (max) @ LEO Design lifetime: 7 years (max) @ LEO (variant 2) Envelope (L×W×H): 55 x 41 x 16 mm Channels: 448 @ Up to Position accuracy: 1.2 m @ 800 km altitude (RMS) Time to first fix (cold): 20 s @ Warm start Time to first fix (cold): 45 s @ Cold start Power consumption: 0.6 W (min) Power consumption: 1.1 W (max) Supply voltage: 3.3 Constellations: GPS L1C/A, L1PY, L2C, L2P, L5 Constellations: GALILEO E1, E5a, E5b, E5 AltBoc, E6* @ (variant 2) Constellations: BEIDOU B1I, B1C, B2a, B2I, B3 @ (variant 3) Constellations: QZSS L1C/A, L2C, L5 @ (variant 4) Constellations: GLONASS L1CA, L2CA, L2P, L3 CDMA @ (variant 5) Constellations: NAVIC L5 @ (variant 6) Constellations: SBAS Egnos, WAAS, GAGAN, MSAS, SDCM (L1, L5) @ (variant 7) Velocity accuracy: 0.03 m/s @ RMS Update rate: 20 Hz Data interface: UART Data interface: USB @ (variant 2) Data interface: other @ PPS outputs Data interface: other @ GPIO Data interface: other @ Ready status Data interface: other @ 3DFix status Data interface: other @ Event/TimeSync input Data interface: other @ On/Off input Data interface: other @ External reset input Connector: SEMS 60-pin dual row female socket (0.8 mm pitch) Connector: MMCX female connector, 50 Ω @ (variant 2) Operating temperature: -30 to 70 Survival temperature: -40 to 85 Design lifetime: 5 years (min) @ LEO Mass: 56 g Envelope (L×W×H): 55 x 41 x 16 mm @ (variant 2) ## ASTROFEIN GPS receiver unit- ARGO — EXA (Astro-und Feinwerktechnik) [gnss-receivers] https://newspacemarket.com/products/argo-l1-gnss-receiver-unit/ Constellations: GPS L1 Band, C/A code Channels: 12 Time to first fix (cold): 180 s @ warm start (90%) Time to first fix (cold): 900 s @ cold start (90%) Position accuracy: 10 m @ 3D rms Velocity accuracy: 0.1 m/s @ 3D rms Update rate: 1 Hz Envelope (L×W×H): 130.0 x 216.6 x 34.4 mm³ @ Configuration 1 Envelope (L×W×H): 51.0 x 216.6 x 109.4 mm³ @ Configuration 2 Mass: 1200 g (max) @ 2x antennas and 2x LNAs, Configuration 1&2 Supply voltage: 18 (min) Supply voltage: 36 (max) Power consumption: 2.2 W @ stand alone single receiver Power consumption: 2.4 W @ single receiver with 2x LNAs Data interface: CAN Data interface: RS422 @ (variant 2) Operating temperature: -20 °C (min) @ Receiver and LNA Operating temperature: 60 °C (max) @ Receiver and LNA Operating temperature: -55 °C (min) @ Antenna Operating temperature: 85 °C (max) @ Antenna Survival temperature: -30 °C (min) @ Receiver and LNA Survival temperature: 70 °C (max) @ Receiver and LNA Design lifetime: 7 years @ in LEO Radiation tolerance (TID): 20 krad (min) @ in LEO missions utilizing aluminum shield thickness of 2 mm ## PODRIX GNSS Receiver — Beyond Gravity (ex-RUAG Space) [gnss-receivers] https://newspacemarket.com/products/beyond-gravity-podrix-gnss-receiver/ Position accuracy: 0.2 m @ real-time PPP with optional SW upgrade Position accuracy: 0.2 m @ With PPP software upgrade (Galileo-only mode) Position accuracy: 1 m @ Standard performance Velocity accuracy: 1 m/s @ With PPP software upgrade (Galileo-only mode) Velocity accuracy: 2 m/s @ Standard performance Time to first fix (cold): 90 s @ Warm start Time to first fix (cold): 900 s @ Cold start GPS Time to first fix (cold): 2400 s @ Cold start GALILEO Constellations: GPS L1 C/A, GPS L2C-M and L2C-L, GPS L5 I/Q, Galileo E1 B/C, Galileo E5a I/Q, Galileo E6 B/C (optionally) Mass: 3000 g @ Electronic box Mass: 735 g @ Antenna Envelope (L×W×H): 280x240x81 mm3 @ Electronic box (incl feet) Envelope (L×W×H): Ø 200 mm, h: 87 mm @ Antenna (incl feet) Supply voltage: 28 @ Primary power input Power consumption: 15 W @ avg Data interface: MIL-STD-1553B @ TC/TM Data interface: UART @ TC/TM (variant 2) Data interface: RS-422 @ TC/TM (variant 3) Data interface: SpaceWire @ TC/TM (variant 4) Data interface: RS-422 @ PPS output Operating temperature: -30 °C (min) @ qualification level Operating temperature: 60 °C (max) @ qualification level Survival temperature: -40 °C (min) @ Minimum switch-on temperature (qualification level) Radiation tolerance (TID): suitable for orbits between 300 and 1500km, any inclination Design lifetime: 7.5 years @ gt Flight heritage: More than 90 flight models of GNSS receivers delivered. Example missions: Swarm, Sentinel-1, Sentinel-2, Sentinel-3 A/B, Sentinel-6/Michael Freilich A/B, Earthcare, ICESat-2, PACE, OSAM-1, Biomass, FLEX, KOMPSAT-6, -7, CAS-500, WSF-M ## GEORIX GNSS Receiver — Beyond Gravity (ex-RUAG Space) [gnss-receivers] https://newspacemarket.com/products/beyond-gravity-georix-gnss-receiver/ Position accuracy: 20 m @ 3D rms in GEO Velocity accuracy: 0.01 m/s @ 3D rms Time to first fix (cold): 900 s @ Warm start in GEO Constellations: GPS C/A on L1, Galileo E1 B/C Mass: 600 g @ LNA Mass: 9000 g @ Electronic box Mass: 548 g @ Antenna (recommended for GEO) Envelope (L×W×H): 168x54x80 mm @ LNA Envelope (L×W×H): 286x201x226 mm @ Electronic box Envelope (L×W×H): 212 mm, h: 179 mm @ Antenna (recommended for GEO) Supply voltage: 100 @ regulated primary power input Power consumption: 15 W @ avg Data interface: MIL-STD-1553B Data interface: UART @ RS-422 Data interface: SpaceWire @ (variant 2) Data interface: RS-422 @ PPS output Operating temperature: -30-60 °C @ qualification level Operating temperature: -40 °C @ Minimum switch-on temperature (qualification level) Design lifetime: 15 years @ GEO Design lifetime: 0.54 years @ GTO (200 days) Flight heritage: SWARM (ESA), Sentinel-1, Sentinel-2 and Sentinel-3 A/B satellites (Copernicus), Sentinel-1, Sentinel-2 and Sentinel-3 C/D, Sentinel-6/Michael Freilich A/B (NASA/ESA), Earthcare (ESA/JAXA), ICESat-2 (NASA), PACE (NASA), OSAM-1 (NASA), Biomass (ESA), FLEX ( ## FoX NavRIX GNSS Receiver — Beyond Gravity (ex-RUAG Space) [gnss-receivers] https://newspacemarket.com/products/beyond-gravity-fox-navrix-gnss-receiver/ Position accuracy: 0.2 m (max) @ 3D rms, PPP Velocity accuracy: 0.001 m/s (max) @ 3D rms, PPP Time to first fix (cold): 60 s (max) @ Warm start Time to first fix (cold): 60 s (max) @ Cold start Constellations: GPS L1 C/A, GPS L5 I/Q, GPS L2C, Galileo E1 B/C, Galileo E5a I/Q, Galileo E6 @ Supported Signals Mass: 3600 g @ Standard Mass: 4100 g @ GEO version Envelope (L×W×H): 210x155x112 mm3 @ incl. feet Operating temperature: -20 °C (min) Operating temperature: 60 °C (max) Power consumption: 10 W @ avg Design lifetime: 10 years (min) @ in LEO Data interface: UART @ TC/TM Data interface: RS-422 @ TC/TM (variant 2) Supply voltage: 28 (nominal) @ unregulated Flight heritage: SWARM (ESA), Sentinel-1, Sentinel-2 and Sentinel-3 A/B (Copernicus), Sentinel-1, Sentinel-2 and Sentinel-3 C/D, Sentinel-6/Michael Freilich A/B (NASA/ESA), EarthCare (ESA/JAXA), ICESat-2 (NASA), PACE (NASA), OSAM-1 (NASA), Biomass (ESA), FLEX (ESA), KOMPS ## NanoSense GPS Kit — GomSpace [gnss-receivers] https://newspacemarket.com/products/nanosense-gps-kit/ Position accuracy: 1.5 m Velocity accuracy: 0.03 m/s Supply voltage: 3.3 @ GPS module Mass: 31 g @ GPS module Envelope (L×W×H): 46 x 72 x 11 mm @ GPS module Mass: 54 g (min) @ collective, including GPS module Mass: 57 g (max) @ collective, including GPS module ## Control Moment Gyroscopes — Blue Canyon Technologies [imus-gyros] https://newspacemarket.com/products/bct-cmg-12/ Mass: 13000 g (max) Supply voltage: 22 (min) Supply voltage: 36 (max) Power consumption: 25 W @ FULL MOMENTUM Power consumption: 30 W @ MANEUVER Data interface: RS-422 ## LN-200S Inertial Measurement Unit — Northrop Grumman Space Systems [imus-gyros] https://newspacemarket.com/products/ngc-ln-200s-imu/ Gyro range: 1000 Bias instability: 1 °/h @ 1s Angle random walk: 0.07 (max) Power consumption: 12 W @ nominal Envelope (L×W×H): Diameter: 3.5 in. (8.89 cm) Height: 3.35 in. (8.51 cm) Mass: 748 g Data interface: RS-422/485 serial data Design lifetime: 15 years Flight heritage: The LN-200S IMU has been utilized and is still performing on the NASA Mars rovers after more than 10 years. The first prototype LN-200S was qualified for space flight onboard the Clementine spacecraft. Many spacecraft now depend on the IMU to provide reli ## G-200 / G-510 Gyroscopes — ElmSpace [imus-gyros] https://newspacemarket.com/products/elmspace-g200-g510-gyroscopes/ Mass: 12 g Envelope (L×W×H): 34 x 29 x 9 mm Supply voltage: 3.3 (nominal) Power consumption: 0.11 W Angle random walk: 0.2 Bias instability: 1.5 °/h Gyro range: 125 (max) Data interface: UART Radiation tolerance (TID): 20 krad ## ASTROFEIN Gyro System AGS-1 — EXA (Astro-und Feinwerktechnik) [imus-gyros] https://newspacemarket.com/products/astrofein-gyro-system-ags-1/ Gyro range: 40 (max) Bias instability: 1 °/h (max) Angle random walk: 0.1 (max) Update rate: 200 Hz Mass: 1000 g (max) Envelope (L×W×H): 134 mm x 85 mm x 60 mm Supply voltage: 18-34 Power consumption: 8 W @ Steady state Power consumption: 10 W @ Maximum Data interface: RS-422 Operating temperature: -15-40 °C Survival temperature: -30-60 °C Design lifetime: 5 years @ in low earth orbit Design lifetime: 5 years @ low earth orbit ## G-200 Gyroscope — ElmSpace [imus-gyros] https://newspacemarket.com/products/elmspace-g-200-gyroscope/ Mass: 12 g Envelope (L×W×H): 34 x 29 x 9 mm Supply voltage: 3.3 Power consumption: 0.11 W Operating temperature: -40-85 °C Angle random walk: 0.2 Bias instability: 1.5 °/h Gyro range: 125 Data interface: UART Radiation tolerance (TID): 20 krad ## G-510 Gyroscope — ElmSpace [imus-gyros] https://newspacemarket.com/products/elmspace-g-510-gyroscope/ Mass: 40 g Envelope (L×W×H): 54 x 54 x 16 mm Supply voltage: 3.3 (nominal) Power consumption: 0.25 W Operating temperature: -40 °C (min) Operating temperature: 85 °C (max) Angle random walk: 0.09 Bias instability: 0.5 °/h Gyro range: 125 Data interface: RS-422 Data interface: CAN @ (variant 2) Data interface: UART @ (variant 3) Radiation tolerance (TID): 20 krad ## AOCS/GNC Sensors — Airbus Defence and Space [imus-gyros] https://newspacemarket.com/products/airbus-bass-bi-axis-sun-sensor/ Bias instability: 0.02 °/h @ over 1 h (steady temperature) Bias instability: 0.2 °/h @ end of life (all effects included) Gyro range: 60 (min) @ qualified (higher speed on demand) Angle random walk: 0.005 @ standard performance design Angle random walk: 0.0025 @ high performance design Operating temperature: -20 °C (min) Operating temperature: 65 °C (max) Radiation tolerance (TID): 25 krad @ at component level Design lifetime: 15 years (max) Mass: 1400 g Envelope (L×W×H): 100 x 100 x 100 mm Supply voltage: 20 (min) Supply voltage: 52 (max) Data interface: RS-422 Data interface: RS-485 @ (variant 2) Power consumption: 7 W ## AOCS & GNC Sensors — Airbus Defence and Space [imus-gyros] https://newspacemarket.com/products/airbus-astrix-gyroscope-series/ Bias instability: 0.02 °/h (max) @ steady temperature, over 1 h Bias instability: 0.2 °/h @ end of life, all effects included Gyro range: 60 (min) @ full performance, qualified Angle random walk: 0.005 (max) @ standard performance design Angle random walk: 0.0025 @ high performance design Operating temperature: -20 °C (min) Operating temperature: 65 °C (max) Radiation tolerance (TID): 25 krad (min) @ at component level Design lifetime: 15 years (max) Mass: 1400 g Envelope (L×W×H): 100 x 100 x 100 mm Supply voltage: 20 (min) Supply voltage: 52 (max) Data interface: RS-422 Data interface: RS-485 @ (variant 2) Power consumption: 7 W ## C14 Bi-Axis Gimbal — Sierra Space [pointing-mechanisms] https://newspacemarket.com/products/sierra-c14-bi-axis-gimbal/ Mass: 1230 g @ excluding cables Mass: 1500 g @ including 85 cm of cabling Angular resolution: 0.0625 deg Max torque: 14 mN·m @ Output @ 4 degrees/s Max torque: 0.9 mN·m @ Unpowered Holding Power consumption: 10 W @ Heater (nominal, each) Operating temperature: -70 °C (min) Operating temperature: 70 °C (max) Survival temperature: -95 °C (min) Survival temperature: 85 °C (max) Flight heritage: Eagle (ESPA Augmented Geostationary Laboratory Experiment) Flight heritage: OrbView 3 and 4 Satellites @ (variant 2) Flight heritage: Geosynchronous Space Situational Awareness Program (GSSAP) 1, 2, 3, and 4 @ (variant 3) Flight heritage: Samaritan Satellite @ (variant 4) ## LDC20 Low-Disturbance Gimbal — Sierra Space [pointing-mechanisms] https://newspacemarket.com/products/sierra-ldc20-low-disturbance-gimbal/ Travel range: 99 (max) @ about the X- and Y-axis Angular resolution: 0.007 deg @ at 64 Microstep Resolution Max torque: 13.6 mN·m @ Powered Holding Torque Max torque: 0.34 mN·m @ Unpowered Holding Torque Mass: 8200 g Power consumption: 15 W @ total power capacity for Y actuator transition Operating temperature: -25 °C (min) Operating temperature: 70 °C (max) Survival temperature: -60 °C (min) @ Nonoperating Temperatures Survival temperature: 75 °C (max) @ Nonoperating Temperatures Flight heritage: GeoEye ## Cobalt — Blue Cubed [pointing-mechanisms] https://newspacemarket.com/products/blue-cubed-bluefin/ Mass: 5300 g Envelope (L×W×H): 295 mm tall, 255 mm diameter (dynamic) Supply voltage: 40 (max) Power consumption: 20 W (min) @ mode dependent Power consumption: 30 W (max) @ mode dependent Data interface: 1000BASE-T Operating temperature: -20 °C (min) Operating temperature: 55 °C (max) Survival temperature: -40 °C (min) Survival temperature: 85 °C (max) ## Umbra Battery Module (8S1P/8S2P) — Umbra Lab Inc. [batteries] https://newspacemarket.com/products/umbra-battery-module/ Supply voltage: 22 (min) @ Battery Voltage Range Supply voltage: 31 (max) @ Battery Voltage Range Supply voltage: 28 (nominal) @ Battery Voltage Nominal Flight heritage: Flown on Umbra 1 - 12 Design lifetime: 5 years (min) Cell chemistry: Lithium Ion Connector: Combination D-Sub (2 power and 5 signal contacts) Envelope (L×W×H): L: 7.13 in W: 4.04 in H: 2.50 in Mass: 1600 g Capacity: 250 Wh Capacity (charge): 8 Ah Radiation tolerance (TID): 30 krad Operating temperature: 10 °C (min) @ Charge Operating temperature: 45 °C (max) @ Charge Operating temperature: -20 °C (min) @ Discharge Operating temperature: 60 °C (max) @ Discharge Survival temperature: -20 °C (min) Survival temperature: 50 °C (max) ## High Capacity Batteries — Blue Canyon Technologies [batteries] https://newspacemarket.com/products/bct-2p8s-battery/ Capacity (charge): 6.8 Ah Capacity: 198 Wh Mass: 1210 g (max) Supply voltage: 28 (nominal) Supply voltage: 24 (min) Supply voltage: 33.6 (max) ## 28-300 Battery Module — Dragonfly Aerospace [batteries] https://newspacemarket.com/products/300-battery-module/ Capacity: 297 Wh Cell chemistry: LFP Mass: 4800 g Envelope (L×W×H): 350 (L) x 108 (W) x 115 mm (H) Supply voltage: 29.7 (nominal) Power consumption: 600 W @ Discharge - Continuous Power consumption: 1200 W @ Discharge - Peak (for 60sec) Data interface: other @ SMBus Data interface: other @ Direct Control Lines Operating temperature: -10 °C (min) Operating temperature: 40 °C (max) Radiation tolerance (TID): 20 krad (min) Design lifetime: 5 years @ in LEO ## ABSL CM1040 8s18p Li-ion Space Battery (28 V, 36 Ah) — EnerSys / ABSL Space Products [batteries] https://newspacemarket.com/products/absl-cm1040-8s18p-space-battery/ Cell chemistry: Li-ion Supply voltage: 24 (min) Supply voltage: 33.6 (max) Capacity (charge): 36 Ah Capacity: 1066 Wh Envelope (L×W×H): 209 x 362 mm @ Footprint Envelope (L×W×H): 131 mm @ Height Mass: 8800 g Flight heritage: over 5.5 billion cell hours of in-orbit heritage using ABSL™ Li-ion cell technology Operating temperature: 0 °C (min) @ Thermal chamber only Operating temperature: 40 °C (max) @ Thermal chamber only Survival temperature: -20 °C (min) @ Cell Level Qual only Survival temperature: 60 °C (max) @ Cell Level Qual only ## ABSL CM2300 8s40p Li-ion Space Battery (28 V, 80 Ah) — EnerSys / ABSL Space Products [batteries] https://newspacemarket.com/products/absl-cm2300-8s40p-space-battery/ Cell chemistry: Li-ion Supply voltage: 24 (min) Supply voltage: 33.6 (max) Capacity (charge): 80 Ah Capacity: 2300 Wh Envelope (L×W×H): 260 x 359 mm (footprint) Envelope (L×W×H): 177 mm (height) @ (variant 2) Mass: 20000 g Flight heritage: over 5.5 billion cell hours of in-orbit heritage using ABSL™ Li-ion cell technology Survival temperature: -20 °C (min) Survival temperature: 50 °C (max) Operating temperature: 0 °C (min) Operating temperature: 40 °C (max) ## ABSL CM170 4s6p Li-ion Space Battery (14 V, 12 Ah) — EnerSys / ABSL Space Products [batteries] https://newspacemarket.com/products/absl-cm170-4s6p-space-battery/ Capacity (charge): 12 Ah Capacity: 178 Wh Supply voltage: 16.8 (max) Supply voltage: 12 (min) Envelope (L×W×H): 95 @ Height Mass: 1600 g Survival temperature: -10 °C (min) @ Non-Operating Survival temperature: 50 °C (max) @ Non-Operating Operating temperature: 0 °C (min) @ Thermal chamber only Operating temperature: 40 °C (max) @ Thermal chamber only ## ABSL CM230 8s4p Li-ion Space Battery (28 V, 8 Ah) — EnerSys / ABSL Space Products [batteries] https://newspacemarket.com/products/absl-cm230-8s4p-space-battery/ Cell chemistry: Li-ion P20 Supply voltage: 33.6 (max) Supply voltage: 24 (min) Capacity (charge): 8 Ah Capacity: 236.8 Wh Envelope (L×W×H): 114 x 168 mm @ Footprint Envelope (L×W×H): 117 mm @ Height Mass: 2050 g Flight heritage: 5.5 billion cell hours of in-orbit heritage using ABSL™ Li-ion cell technology Survival temperature: -20 °C (min) @ Cell Level Qual only Survival temperature: 60 °C (max) @ Cell Level Qual only Operating temperature: 0 °C (min) @ Thermal chamber only Operating temperature: 40 °C (max) @ Thermal chamber only ## NanoPower BPX 100 Wh — GomSpace [batteries] https://newspacemarket.com/products/nanopower-bpx-100-wh/ Capacity: 100 Wh @ nominal Capacity: 86 Wh @ in recommended operating range Capacity: 87 Wh @ VBAT= 23.6V to 32.0V Capacity: 89 Wh @ VBAT= 23.6V to 33.6V Capacity (charge): 7 Ah @ 4S-2P configuration Capacity (charge): 3.5 Ah @ 8S-1P configuration Cell chemistry: Lithium-ion battery pack for space applications Cell chemistry: 18650 Lithium-ion cells @ (variant 2) Mass: 500 g Envelope (L×W×H): 93 x 86 x 41 (L x W x H) mm Supply voltage: 14.4 (nominal) @ 4S-2P Supply voltage: 28.8 (nominal) @ 8S-1P Power consumption: 6 W @ Heater power usage 16 V 4S-2P Power consumption: 6 W @ Heater power usage 32 V 8S-1P Data interface: CAN Data interface: I2C @ (variant 2) Data interface: UART @ (variant 3) Connector: Picoblade Molex 0532610971 (Heater Connector P1) Connector: Picoblade Molex 0532610871 (Debug P2) @ (variant 2) Connector: Harwin M80-5421442 (Battery Connector PBAT1) @ (variant 3) Connector: Harwin M80-5421442 (Battery Connector PBAT2) @ (variant 4) Connector: Harwin M80-5430805 (Ground Breaker PGND1) @ (variant 5) ## NanoPower BP8 100 Wh — GomSpace [batteries] https://newspacemarket.com/products/nanopower-bp8-100-wh/ Capacity: 100 Wh Capacity: 86 Wh @ in recommended operating range Capacity: 86 Wh @ VBAT= 23.6V to 32.0V Capacity: 89 Wh @ VBAT= 23.6V to 33.6V Capacity (charge): 3.5 Ah @ nominal capacity Capacity (charge): 3 Ah @ in recommended operating range Cell chemistry: lithium-ion Mass: 486 g Envelope (L×W×H): 94.8 x 95 x 42 (L x W x H) mm Supply voltage: 28.8 (nominal) Supply voltage: 23.6 (min) Supply voltage: 32 (max) Power consumption: 6 W @ Heater power usage Data interface: CAN Data interface: I2C @ (variant 2) Data interface: UART @ (variant 3) Connector: G125-FS13405L0R @ Main battery connector (J1) Connector: G125-FS13405L0R @ Secondary battery connector (J2) Connector: G125-FS11005L0R @ Ground breaker connector (J3) Connector: Picoblade 53398-0871 @ GOSH connector for configuration (J5) Operating temperature: -10 °C (min) @ Charge Operating temperature: 45 °C (max) @ Charge Operating temperature: -20 °C (min) @ Discharge Operating temperature: 60 °C (max) @ Discharge ## Cubesat Magnetorquer Rod — SSBV Aerospace & Technology [magnetorquers] https://newspacemarket.com/products/ssbv-cubesat-magnetorquer-rod/ Magnetic dipole moment: 0.2 A·m² (min) Residual moment: 0.001 A·m² (max) Power consumption: 0.2 W @ typically Supply voltage: 5 @ supply Operating temperature: -35 °C (min) Operating temperature: 75 °C (max) Design lifetime: 10 years (min) Envelope (L×W×H): 70 mm (length) x 9 mm (diameter) Mass: 30 g (max) Data interface: other ## Magnetic Torque Rod family (PS-MTQ-0.8 and PS-MTQ-4) — Plan-S (Connecta) [magnetorquers] https://newspacemarket.com/products/magnetic-torque-rod-family-ps-mtq-0-8-and-ps-mtq-4-4217/ Magnetic dipole moment: 4 A·m² Supply voltage: 5 Data interface: CAN Data interface: RS-485 @ (variant 2) Connector: Harwin Gecko Mass: 200 g Envelope (L×W×H): 160 x 35 x 20 mm ## Reaction Wheels — Sinclair Interplanetary (Rocket Lab) [reaction-wheels] https://newspacemarket.com/products/sinclair-10-mnms-picosatellite-reaction-wheel/ Angular momentum storage: 0.01 N·m·s @ Nominal Angular momentum storage: 0.018 N·m·s @ peak, at 5 V supply Max torque: 1 mN·m @ at 0.01 Nms (at 5 V supply) Data interface: UART Data interface: I2C @ (variant 2) Data interface: other @ SMBus Envelope (L×W×H): 50 mm x 50 mm x 30 mm Mass: 120 g Supply voltage: 3.4 (min) @ Nominal Supply voltage: 6 (max) @ Nominal Supply voltage: 8 (max) @ Maximum Power consumption: 1.05 W @ @ 0.01 Nms, + 1 mNm Power consumption: 0.25 W @ @ 0.018 Nms, steady state Power consumption: 0.11 W @ @ 0.005 Nms, steady state Operating temperature: -40 °C (min) Operating temperature: 70 °C (max) Radiation tolerance (TID): 20 krad Bearing type: ball @ Diamond coated hybrid ball bearings Design lifetime: 10 years @ on-orbit Flight heritage: 10 Units total on-orbit on 4 satellites, first launched June 2014 ## Trillian-1 — AAC Clyde Space [reaction-wheels] https://newspacemarket.com/products/aac-trillian-1/ Angular momentum storage: 1.2 N·m·s (nominal) @ Total Momentum Storage Angular momentum storage: 1.2 N·m·s (nominal) @ Total Momentum Storage (variant 2) Max torque: 47.1 mN·m (max) @ Maximum Torque Max torque: 47.1 mN·m (max) @ Maximum Torque (variant 2) Wheel speed: 6500 (max) @ Maximum Rotation Rate Wheel speed: 6500 (max) @ Maximum Rotation Rate (variant 2) Mass: 1500 g (nominal) Mass: 1500 g (nominal) @ (variant 2) Envelope (L×W×H): 135x135x82 @ Compact Envelope (L×W×H): 135x135x82 Supply voltage: 20 (min) @ Supply Voltage Supply voltage: 34 (max) @ Supply Voltage Power consumption: 24 W @ peak Power consumption: 1.5 W @ Idle Power consumption: 12 W @ Nominal Power consumption: 24 W @ Peak (variant 2) Operating temperature: -10 °C (min) Operating temperature: 50 °C (max) Survival temperature: -40 °C (min) @ Storage Temperature Survival temperature: 85 °C (max) @ Storage Temperature Flight heritage: since 2019 @ in-orbit heritage ## RWA-05 — Berlin Space Technologies [reaction-wheels] https://newspacemarket.com/products/rwa05-24-reaction-wheel-assembly/ Angular momentum storage: 0.5 N·m·s Wheel speed: 500-5000 @ Min +/- Wheel speed: 500-5000 @ Max +/- Max torque: 16 mN·m @ @ 500 rpm Max torque: 14.2 mN·m @ @ 5000 rpm Supply voltage: 5 @ Electronics Supply voltage: 17-32 @ Motor Power consumption: 0.5 W @ @ 5V Data interface: UART @ Command Interface Data interface: RS-422 @ Command Interface (variant 2) Envelope (L×W×H): 105.0 x 106.6 x 109.5 mm³ Survival temperature: -30-50 °C @ Storage Operating temperature: -20-40 °C @ Operation Design lifetime: 5 years @ LEO Flight heritage: Yes Radiation tolerance (TID): 30 krad @ Co60 Mass: 1700 g @ (RW + WDE + Gyro) Mass: 1550 g @ (RW + WDE) ## RW-1Nms — Dragonfly Aerospace [reaction-wheels] https://newspacemarket.com/products/rw-1nms/ Angular momentum storage: 1 N·m·s @ @28.5 V Max torque: 39 mN·m (nominal) Max torque: 74 mN·m (max) Wheel speed: -10000-10000 Supply voltage: 12-36 Power consumption: 1.2 W @ @ 0.1 Nms Power consumption: 108 W @ Peak Operating temperature: -20-60 °C Envelope (L×W×H): 102.8 x 100 x 50 mm Mass: 1000 g Static imbalance: 2 Dynamic imbalance: 50 Radiation tolerance (TID): 20 krad @ at component level Data interface: CAN Data interface: RS-485 @ (variant 2) Bearing type: ball @ ABEC 7 ## MicroCMG — EXA (Astro-und Feinwerktechnik) [reaction-wheels] https://newspacemarket.com/products/microcmg-control-moment-gyroscope/ Angular momentum storage: 8 N·m·s @ @3820rpm Wheel speed: 3820 @ Nominal Rotation Speed Max torque: 14000 mN·m @ Nominal Torque Mass: 8000 g (max) Envelope (L×W×H): 188mm*188mm*240mm Operating temperature: -20 °C (min) Operating temperature: 50 °C (max) Design lifetime: 11 years ## Magnetometer — SSBV Aerospace & Technology [magnetometers] https://newspacemarket.com/products/ssbv-magnetometer/ Measurement range: 50 µT (max) Resolution: 13 nT Update rate: 10 Hz (max) Mass: 20 g @ sensor Mass: 180 g @ electronics Envelope (L×W×H): 20x12x5mm @ Sensor only Envelope (L×W×H): 85x36x17mm @ Electronics (including sensor) Supply voltage: 5 Power consumption: 0.4 W Data interface: RS-422 Data interface: RS-485 @ (variant 2) Data interface: I2C @ (variant 3) Connector: 9-pin micro-D @ stand alone version Operating temperature: -35-75 °C Radiation tolerance (TID): 10 krad @ component level ## NSS Magnetometer — NewSpace Systems (NSS) [magnetometers] https://newspacemarket.com/products/nss-tri-axial-amr-magnetometers/ Measurement range: 60 µT @ PEGASUS-1 Measurement range: 60 µT @ PEGASUS-30K Measurement range: 100 µT @ PEGASUS-30K (variant 2) Resolution: 8 nT (max) @ PEGASUS-1 Resolution: 8 nT (max) @ PEGASUS-30K Update rate: 25 Hz (max) @ PEGASUS-1 Update rate: 20 Hz (max) @ PEGASUS-30K Noise density: 16 nT (max) @ PEGASUS-1 Noise density: 16 nT (max) @ PEGASUS-30K Mass: 82 g @ PEGASUS-1 Mass: 107 g @ PEGASUS-30K Envelope (L×W×H): 99 mm × 43 mm × 17 mm @ PEGASUS-1 Envelope (L×W×H): 92 mm × 43 mm × 17.5 mm @ PEGASUS-30K Power consumption: 0.735 W (max) @ PEGASUS-1 Power consumption: 0.5 W (max) @ PEGASUS-30K Supply voltage: 5 @ PEGASUS-1 Supply voltage: 5 @ PEGASUS-30K Operating temperature: -30 °C (min) @ PEGASUS-1 Operating temperature: 75 °C (max) @ PEGASUS-1 Operating temperature: -30 °C (min) @ PEGASUS-30K Operating temperature: 75 °C (max) @ PEGASUS-30K Radiation tolerance (TID): 10 krad @ PEGASUS-1 Radiation tolerance (TID): 30 krad @ PEGASUS-30K Data interface: RS-485 @ PEGASUS-1 Data interface: RS-422 @ PEGASUS-1 (variant 2) Data interface: RS-485 @ PEGASUS-30K Data interface: RS-422 @ PEGASUS-30K (variant 2) Connector: 9-pin Female Micro-D @ PEGASUS-1 Connector: 15-pin Female Micro-D @ PEGASUS-30K Flight heritage: TRL 9 with significant in-orbit heritage. Developed in collaboration with the Space and Atmospheric Physics Group of Imperial College London, the sensor head first flew on the CINEMA mission and then as an integrated unit in July 2014. Since then, > 400 u ## Lodestone — Spacemanic s.r.o. [magnetometers] https://newspacemarket.com/products/spacemanic-lodestone/ Operating temperature: -40 °C (min) Operating temperature: 85 °C (max) Envelope (L×W×H): 22 x 20 x 6 mm Mass: 10 g (max) Supply voltage: 3.3 (nominal) Power consumption: 0.01 W (max) @ average Power consumption: 0.01 W (max) @ peak Measurement range: 800 µT (max) Data interface: I2C Connector: Molex PicoBlade 53261-0671 Flight heritage: on multiple missions (e.g. CroCube, Veronika and external customers) ## piMAGGYRO — SkyFox Labs s.r.o. [magnetometers] https://newspacemarket.com/products/skyfox-labs-pimaggyro/ Export status: controlled @ regulated goods, needs special Export License approved by the Ministry of Industry and Trade of Measurement range: 300 µT @ per axis Resolution: 6 nT @ Per each axis. Noise density: 5 nT Update rate: 10 Hz Update rate: 10 Hz @ (variant 2) Mass: 33 g Envelope (L×W×H): 53×32×(+14, -2) mm Supply voltage: 2.8-3.6 Supply voltage: 2.8-3.6 @ (variant 2) Power consumption: 0.05 W @ typical, 3.3 V @ 25°C Power consumption: 0.05 W @ Active Operating Power Data interface: UART Connector: 2 mm pitch, 2×5 pin header Operating temperature: -40-85 °C Operating temperature: -40-85 °C @ (variant 2) Survival temperature: -45-90 °C ## MAG15 — Lusospace [magnetometers] https://newspacemarket.com/products/lusospace-mag15-analogue-magnetometer/ Measurement range: 64 µT (max) Noise density: 3 nT (max) Update rate: 50 Hz (max) Mass: 260 g (max) Envelope (L×W×H): 83x90x45 mm (excl. connectors) Supply voltage: 15 (nominal) Power consumption: 1 W (max) @ nominal Connector: Test connector Operating temperature: -40-70 °C Survival temperature: -50-80 °C Radiation tolerance (TID): 50 krad (max) Flight heritage: Sentinel (all), Sentinel 3 (all), Sentinel 5p, SEOSAT, CHEOPS, BIOMASS and more. ## NanoSense M315 — GomSpace [magnetometers] https://newspacemarket.com/products/gomspace-nanosense-m315/ Measurement range: 800 µT (max) Noise density: 15 nT @ No external magnetic disturbances Update rate: 140 Hz (max) Mass: 8 g Mass: 8 g @ (variant 2) Envelope (L×W×H): 23 x 20 x 8 mm Envelope (L×W×H): 23 x 20 x 8 mm @ (variant 2) Supply voltage: 3.2 (min) Supply voltage: 5 (max) Connector: Pico-blade 1.25 mm Pitch. Molex 53261-0471. Operating temperature: -40 °C (min) Operating temperature: 85 °C (max) Survival temperature: -40 °C (min) Survival temperature: 85 °C (max) Flight heritage: Flight proven ## Mag610/611 — Bartington Instruments [magnetometers] https://newspacemarket.com/products/mag610-611/ Operating temperature: 0 °C (min) Operating temperature: -98.2 °C (max) @ Mag610 Operating temperature: -58.2 °C (max) @ Mag611 Survival temperature: 0 °C (min) Survival temperature: -98.2 °C (max) @ Mag610 Survival temperature: -58.2 °C (max) @ Mag611 Envelope (L×W×H): 23 x 23 x 21.4mm Mass: 25 g @ with 1m wires Connector: RM15-TPD-10P (when supplied with Mag610/611 RTPDE) ## CryoMag® — Bartington Instruments [magnetometers] https://newspacemarket.com/products/cryomag/ Measurement range: 70 µT @ abs Measurement range: 100 µT @ abs (variant 2) Measurement range: 250 µT @ abs (variant 3) Measurement range: 500 µT @ abs (variant 4) Operating temperature: -271 °C (min) @ Probe + probe harness Operating temperature: 70 °C (max) @ Probe + probe harness Operating temperature: 0 °C (min) @ Electronics + interconnection block (dynamic cable) Operating temperature: 70 °C (max) @ Electronics + interconnection block (dynamic cable) Operating temperature: -40 °C (min) @ Electronics + interconnection block (static cable) Operating temperature: 70 °C (max) @ Electronics + interconnection block (static cable) Survival temperature: -40 °C (min) Survival temperature: 60 °C (max) Envelope (L×W×H): 21mm Diameter x 50mm Long @ Probe Dimensions Standard Envelope (L×W×H): 7 x 5 x 38mm typical @ Probe Dimensions IE Envelope (L×W×H): 25.4mm Diameter x 220mm Long @ Electronics Enclosure Mass: 320 g (typical) Connector: Fischer AL-1731-DEU-1031-A010-SR-11-11-G-12 Supply voltage: 12 (min) Supply voltage: 17 (max) ## Mag-03RCU — Bartington Instruments [magnetometers] https://newspacemarket.com/products/mag-03rcu/ Measurement range: 100 µT Measurement range: 200 µT @ (variant 2) Measurement range: 300 µT @ (variant 3) Operating temperature: -10 °C (min) Operating temperature: 50 °C (max) Envelope (L×W×H): 582.5 x ø50mm Mass: 1100 g @ sensor only Mass: 1650 g @ with bowspring assembly Connector: Hydrobond HRS106-10P/SS/L, or Hydrobond HRS106-10P/Ti/L @ magnetometer connector Supply voltage: 15 (min) @ Supply voltage Supply voltage: 30 (max) @ Supply voltage Supply voltage: 12 (min) @ Supply voltage (absolute min. and max.) Supply voltage: 30 (max) @ Supply voltage (absolute min. and max.) ## Mag639 — Bartington Instruments [magnetometers] https://newspacemarket.com/products/mag639/ Measurement range: 100 µT (max) Update rate: 12000 Hz (max) Mass: 300 g Envelope (L×W×H): 28.1 (Ø) x 218mm (L) Supply voltage: 15-17 @ ± Connector: Hirose RM15TRD10S Operating temperature: -20-70 °C ## Mag612 Miniature — Bartington Instruments [magnetometers] https://newspacemarket.com/products/mag612-miniature/ Envelope (L×W×H): 20 x 20 x 20mm @ Probe head only Mass: 72 g @ Probe head only Connector: Molex Picoblade 51021-1000 Measurement range: 1000 µT (max) Envelope (L×W×H): 20 x 20 x 20mm @ Probe head only (variant 2) Mass: 72 g @ Probe head only (variant 2) Connector: Molex Picoblade 51021-1000 @ (variant 2) ## Mag614-FL — Bartington Instruments [magnetometers] https://newspacemarket.com/products/mag614-fl/ Operating temperature: -20 °C (min) Operating temperature: -98.2 °C (max) Survival temperature: -40 °C (min) Survival temperature: -98.2 °C (max) Envelope (L×W×H): 24.7 x 19.7 x 11mm Mass: 27 g ## UAS-Mag® — Bartington Instruments [magnetometers] https://newspacemarket.com/products/uas-mag/ Export status: Dual-use 6a006a3 @ Standard Noise Export status: EAR99 @ Basic Noise Export status: ITAR-free Measurement range: 105 µT Mass: 25 g Envelope (L×W×H): 110 x 29 x 24mm Supply voltage: 4.5 (min) Supply voltage: 15 (max) Power consumption: 0.3 W @ typical @5V Data interface: DroneCAN Connector: JST-GH-4P Operating temperature: -40 °C (min) Operating temperature: 85 °C (max) Survival temperature: -40 °C (min) Survival temperature: 85 °C (max) ## Mag-01H® — Bartington Instruments [magnetometers] https://newspacemarket.com/products/mag-01h/ Resolution: 0.1 nT Measurement range: 2000 µT Measurement range: 200 µT @ depending on probe Measurement range: 2000 µT @ depending on probe (variant 2) Resolution: 0.1 nT @ Maximum Operating temperature: 0 °C (min) Operating temperature: 50 °C (max) Envelope (L×W×H): 155 x 68 x 175mm Mass: 950 g Supply voltage: 12 (nominal) @ Battery charger inlet Measurement range: 20 µT (max) @ Low field probes (B, C and F) Measurement range: 290 µT (max) @ Low field probes (B, C and F) (variant 2) Measurement range: 290 µT (max) @ High field probes (D, E and G) Measurement range: 1000 µT (max) @ High field probes (D, E and G) (variant 2) Resolution: 1 nT @ Low field probes (B, C and F), Range 0-20μT Resolution: 10 nT @ Low field probes (B, C and F), Range 20-290μT Resolution: 10 nT @ High field probes (D, E and G), Range 0-290μT Resolution: 100 nT @ High field probes (D, E and G), Range 290-1000μT Measurement range: 2 µT (max) @ Mag-01H (x10 sensitivity), Low field probes Measurement range: 100 µT (max) @ Mag-01H (x10 sensitivity), Low field probes (variant 2) Measurement range: 290 µT (max) @ Mag-01H (x10 sensitivity), Low field probes (variant 3) Measurement range: 20 µT (max) @ Mag-01H (x10 sensitivity), High field probes Measurement range: 1000 µT (max) @ Mag-01H (x10 sensitivity), High field probes (variant 2) Measurement range: 2000 µT (max) @ Mag-01H (x10 sensitivity), High field probes (variant 3) Resolution: 0.1 nT @ Mag-01H (x10 sensitivity), Low field probes, Range 0-2μT Resolution: 1 nT @ Mag-01H (x10 sensitivity), Low field probes, Range 2-100μT Resolution: 10 nT @ Mag-01H (x10 sensitivity), Low field probes, Range 100-290μT Resolution: 1 nT @ Mag-01H (x10 sensitivity), High field probes, Range 0-20μT Resolution: 10 nT @ Mag-01H (x10 sensitivity), High field probes, Range 20-1000μT Resolution: 100 nT @ Mag-01H (x10 sensitivity), High field probes, Range 1000-2000μT Power consumption: 0.026 W @ Excitation power, low field probes Power consumption: 0.016 W @ Excitation power, high field probes Operating temperature: -30 °C (min) @ axial and transverse probes Operating temperature: 75 °C (max) @ axial and transverse probes Operating temperature: Liquid helium to +30ºC @ cryogenic probes ## DAS3 — Bartington Instruments [magnetometers] https://newspacemarket.com/products/das3/ Envelope (L×W×H): 740mm D x 575mm W x 424mm H @ With covers fitted Envelope (L×W×H): 630mm D x 575mm W x 424mm H @ Without covers fitted Mass: 80000 g (min) Operating temperature: 0 °C (min) Operating temperature: 40 °C (max) Survival temperature: -40 °C (min) Survival temperature: 71 °C (max) ## Mag-13® — Bartington Instruments [magnetometers] https://newspacemarket.com/products/mag-13/ Measurement range: 70 µT (nominal) Measurement range: 100 µT (nominal) @ (variant 2) Measurement range: 250 µT (nominal) @ (variant 3) Measurement range: 500 µT (nominal) @ (variant 4) Measurement range: 1000 µT (nominal) @ (variant 5) Supply voltage: 12 (min) Supply voltage: 17 (max) Operating temperature: -40 °C (min) Operating temperature: 70 °C (max) Survival temperature: -40 °C (min) Survival temperature: 70 °C (max) Mass: 82.5 g (typical) @ Mag-13MC Mass: 222.6 g (typical) @ Mag-13MS Mass: 300 g (typical) @ Mag-13MSS Mass: 950 g (typical) @ Mag-13MCD Mass: 950 g (typical) @ Mag-13MCDFL Mass: 950 g (typical) @ Mag-13MCDT Mass: 23.5 g (typical) @ Mag-13U Mass: 157 g (max) @ Mag-13U-TPU (max cable length) Envelope (L×W×H): Ø 25.4 x 203mm (typical) @ Mag-13MC Envelope (L×W×H): 32 x 32 x 203mm (typical) @ Mag-13MS Envelope (L×W×H): 30 x 30 x 251mm (typical) @ Mag-13MSS Envelope (L×W×H): Ø 60 x 301mm (typical) @ Mag-13MCD Envelope (L×W×H): Ø60 x 264mm (typical) @ Mag-13MCDFL Envelope (L×W×H): Ø60 x 264mm (typical) @ Mag-13MCDT Envelope (L×W×H): Ø 23.2 x 150mm (typical) @ Mag-13U Envelope (L×W×H): Probe: Ø23.2 x 43mm, Electronics: 19.5 x 129mm (typical) @ Mag-13U-TPU Connector: Fischer AL-1731-DEU-1031-A010-SR-11-11-G-12 (typical) @ Mag-13MC Connector: Fischer AL-1731-DEU-1031-A010-SR-11-11-G-12 (typical) @ Mag-13MS Connector: SubConn MCBH10F-NM (underwater mateable) (typical) @ Mag-13MSS Connector: SubConn MCBH10F (underwater mateable) (typical) @ Mag-13MCD Connector: MacArtney Type 4622C Cable (typical) @ Mag-13MCDFL Connector: MacArtney Type MCOM10F (typical) @ Mag-13MCDT Connector: Molex 53047-0810 (typical) @ Mag-13U Connector: Molex 53047-0810 (typical) @ Mag-13U-TPU ## Mag646/710 — Bartington Instruments [magnetometers] https://newspacemarket.com/products/mag646-710/ Measurement range: 100 µT (max) Measurement range: 200 µT (max) @ (variant 2) Measurement range: 500 µT (max) @ (variant 3) Measurement range: 1000 µT (max) @ (variant 4) Update rate: 1000 Hz (min) @ Mag646, at -3dB Mass: 10 g Envelope (L×W×H): 7 x 25 x 76mm Supply voltage: 11 (min) Supply voltage: 17 (max) Connector: Molex 70553-0004 Operating temperature: -20 °C (min) Operating temperature: 70 °C (max) Survival temperature: -20 °C (min) Survival temperature: 70 °C (max) ## Mag658 — Bartington Instruments [magnetometers] https://newspacemarket.com/products/mag658/ Measurement range: 524.287 µT Resolution: 0.0625 nT Noise density: 10 nT Mass: 35 g Envelope (L×W×H): 50mm x 20mm x 128mm Supply voltage: 10-20 Power consumption: 1 W @ nominal Power consumption: 1.3 W @ (max) transmitting Data interface: RS-422 Connector: Molex Picoblade 14W 53047-1410 or solder pads Operating temperature: -30-40 °C Survival temperature: -40-70 °C ## Mag900/901 — Bartington Instruments [magnetometers] https://newspacemarket.com/products/mag900-901/ Measurement range: 60 µT Measurement range: 100 µT @ (variant 2) Envelope (L×W×H): 29 x 25 x 100mm Mass: 25 g Connector: Hirose DF11-10DP-2DSA(01) Supply voltage: 4.5-15 Operating temperature: -40-70 °C Survival temperature: -40-50 °C ## Mag619 — Bartington Instruments [magnetometers] https://newspacemarket.com/products/mag619/ Measurement range: 60 µT @ Mag619U Measurement range: 100 µT @ Mag619U (variant 2) Measurement range: 500 µT @ Mag619U (variant 3) Measurement range: 1000 µT @ Mag619U (variant 4) Resolution: 150 nT @ Zero Field Offset, Mag619U Resolution: 150 nT @ Zero Field Offset, Mag619 Probe Update rate: 3000 Hz @ frequency range, minimum within -3dB level, Mag619U Mass: 10 g @ Probe/Sensor, Mag619U Mass: 115 g @ Probe/Sensor (Including harness), Mag619U Mass: 12.5 g @ Electronics, Mag619U Mass: 10 g @ Not including harness, Mag619 Probe Mass: 115 g @ Including harness, Mag619 Probe Envelope (L×W×H): 29 x 20 x 11 @ Probe/Sensor, Mag619U Envelope (L×W×H): 90 x 85 x 30 @ Electronics, Mag619U Envelope (L×W×H): 29 x 20 x 11 @ Not including harness, Mag619 Probe Supply voltage: 11 (min) @ Positive supply voltage, Mag619U Supply voltage: 15.5 (max) @ Positive supply voltage, Mag619U Supply voltage: -11 (min) @ Negative supply voltage, Mag619U Supply voltage: -15.5 (max) @ Negative supply voltage, Mag619U Operating temperature: -40 °C (min) @ Probe & Electronics, Mag619U Operating temperature: 70 °C (max) @ Probe & Electronics, Mag619U Operating temperature: -40 °C (min) @ Mag619 Probe Operating temperature: 65 °C (max) @ Mag619 Probe Survival temperature: -40 °C (min) @ Probe & Electronics, Mag619U Survival temperature: 70 °C (max) @ Probe & Electronics, Mag619U Survival temperature: -40 °C (min) @ Mag619 Probe Survival temperature: 70 °C (max) @ Mag619 Probe ## Mag566 — Bartington Instruments [magnetometers] https://newspacemarket.com/products/mag566/ Measurement range: 100 µT (max) Noise density: 1.5 nT (max) @ at 1Hz Mass: 27 g Envelope (L×W×H): 42 x 20 x 52 (±0.5)mm Supply voltage: 4.8-5.2 @ supply Power consumption: 0.02 W @ nominal Connector: 14 way, Samtec MTSW-107-08-S-D-340 Operating temperature: -32-50 °C Survival temperature: -40-70 °C ## Gradiometer (MFG-2S) — Magson GmbH [magnetometers] https://newspacemarket.com/products/magson-gradiometer-mfg-2s/ Mass: 395 g Envelope (L×W×H): 170 x 105 x 33 Power consumption: 1.5 W Measurement range: 65 µT Resolution: 0 nT Data interface: RS422 Update rate: 1 Hz Update rate: 10 Hz @ (variant 2) Update rate: 50 Hz @ (variant 3) Update rate: 100 Hz @ (variant 4) ## Grad-13® — Bartington Instruments [magnetometers] https://newspacemarket.com/products/grad-13/ Measurement range: 70 µT (nominal) Measurement range: 100 µT (nominal) @ (variant 2) Mass: 1400 g (nominal) @ Grad-13-500L & S Mass: 1700 g (nominal) @ Grad-13-750L & S Mass: 2000 g (nominal) @ Grad-13-1000L & S Envelope (L×W×H): ø35 x 677mm + cable @ Grad-13-500L Envelope (L×W×H): ø35 x 927mm + cable @ Grad-13-750L Envelope (L×W×H): ø35 x 1177mm + cable @ Grad-13-1000L Envelope (L×W×H): ø38 x 677mm + cable @ Grad-13-500S Envelope (L×W×H): ø38 x 927mm + cable @ Grad-13-750S Envelope (L×W×H): ø38 x 1177mm + cable @ Grad-13-1000S Supply voltage: 9 (min) Supply voltage: 32 (max) Power consumption: 5 W (max) @ typical Data interface: RS422 Connector: Amphenol 62GB-16J12-08PN @ L Connector: SUBCONN MCOM8M @ S Operating temperature: -30 °C (min) Operating temperature: 85 °C (max) Survival temperature: -40 °C (min) Survival temperature: 85 °C (max) Noise density: 12 nT (max) ## Grad-01-1000L — Bartington Instruments [magnetometers] https://newspacemarket.com/products/grad-01-1000l/ Measurement range: 0.1 µT (max) @ full scale Measurement range: 1 µT (max) @ full scale (variant 2) Update rate: 10 Hz (max) @ Bandwidth Update rate: 10 Hz (min) @ Bandwidth Mass: 820 g Envelope (L×W×H): 38mm diameter x 1052mm in length Supply voltage: 12 (nominal) Supply voltage: 9.5 (min) Supply voltage: 18.5 (max) Connector: 12 pole Tajimi R04-R12M Operating temperature: -20 °C (min) Operating temperature: 70 °C (max) Noise density: 100 nT ## Mag693U — Bartington Instruments [magnetometers] https://newspacemarket.com/products/mag693u/ Measurement range: 100 µT Noise density: 0.01 nT (min) @ at 1Hz Noise density: 0.15 nT (max) @ at 1Hz Envelope (L×W×H): 88 x 18 x 15 Mass: 10 g (max) Connector: AMP / TE Connectivity 640456-7 Supply voltage: 12 (min) Supply voltage: 15 (max) Operating temperature: -20 °C (min) Operating temperature: 80 °C (max) Survival temperature: -20 °C (min) Survival temperature: 80 °C (max) ## Mag652 — Bartington Instruments [magnetometers] https://newspacemarket.com/products/mag652/ Measurement range: 60 µT Resolution: 1 nT Envelope (L×W×H): 111 x 83 x 46 Mass: 600 g (max) @ 1.5m variant Mass: 800 g (max) @ 15m variant Connector: TE Connectivity T4113002081-000 M12 Right-Angled Male 8-Way Connector Field Installable Operating temperature: -30 °C (min) Operating temperature: 50 °C (max) Supply voltage: 3.5 (min) Supply voltage: 15 (max) ## Mag648 / Mag649® — Bartington Instruments [magnetometers] https://newspacemarket.com/products/mag648-mag649/ Measurement range: 60 µT @ Mag648 Measurement range: 100 µT @ Mag648 (variant 2) Measurement range: 60 µT Resolution: 100 nT @ Offset (in zero field) Update rate: 30 Hz @ Bandwidth (-3dB): Mag648 Update rate: 1000 Hz Mass: 120 g Mass: 330 g @ Mag648S/Mag649S (approximate) Mass: 200 g @ Mag648U/Mag649U (approximate) Envelope (L×W×H): 30 x 32 x 70mm Envelope (L×W×H): 40 x 40 x 141mm @ Mag648S/Mag649S (W x H x L) Envelope (L×W×H): 29 x 23 x 66mm @ Mag648U/Mag649U (W x H x L) Supply voltage: 3.5-15 @ DC Power consumption: 0.0112 W @ Mag648 (basic noise) in zero field Power consumption: 0.0098 W Power consumption: 0.0189 W @ Mag649® (low noise & ±200μT) in zero field Connector: Binder 99 9125 00 08 Connector: Flying leads 8x0.22mm @ Mag648FL/Mag649FL Connector: SubConn MCBH10FNM @ Mag648S/Mag649S Connector: Molex 53047-1010 @ Mag648U/Mag649U Operating temperature: -40-70 °C Survival temperature: -40-60 °C ## GNSS Active Patch Antenna — ISISPACE Group [antennas] https://newspacemarket.com/products/isispace-gnss-active-patch-antenna/ Mass: 20 g (max) Envelope (L×W×H): 58 x 58 x 9.7 mm Operating temperature: -20 °C Gain: 34.5 Antenna type: MMCX (RF and power line combined, female) Supply voltage: 3-5 ## S-Band TMTC Antenna — ISISPACE Group [antennas] https://newspacemarket.com/products/isispace-s-band-tmtc-antenna/ Mass: 60 g (max) Envelope (L×W×H): Diameter: 78 mm; Height with connector: 16.0 mm Operating temperature: -20-60 °C Gain: 6 (min) Beamwidth: 100 Power consumption: 2 W ## S-Band Patch Antenna — ISISPACE Group [antennas] https://newspacemarket.com/products/isispace-s-band-patch-antenna/ Mass: 60 g (max) Envelope (L×W×H): Diameter: 80 mm; Height (without connector): 5.0 mm; Connector height (straight): 9 mm Operating temperature: -20-50 °C Gain: 6.5 Beamwidth: 100 Power consumption: 2 W Flight heritage: Since 2021 ## 3-channel X-band Multiplexer — Glavkosmos [antennas] https://newspacemarket.com/products/3-channel-x-band-multiplexer/ Design lifetime: 15 years Lead time: 4 Power consumption: 150 W Power consumption: 450 W @ (variant 2) ## 4-channel C-band Multiplexer — Glavkosmos [antennas] https://newspacemarket.com/products/4-channel-c-band-multiplexer/ Design lifetime: 15 years Lead time: 4 Power consumption: 125 W Power consumption: 500 W @ (variant 2) ## Antenna Array — Glavkosmos [antennas] https://newspacemarket.com/products/antenna-array/ Antenna type: Helical, turnstile, log-periodic, whip, horn, etc. ## Antenna ASNB-1 — Glavkosmos [antennas] https://newspacemarket.com/products/antenna-asnb-1/ Design lifetime: 3 years Lead time: 3 Gain: 25 Envelope (L×W×H): 90 × 90 × 30 Mass: 1000 g ## Antenna ASNB-2 — Glavkosmos [antennas] https://newspacemarket.com/products/antenna-asnb-2/ Design lifetime: 3 years Lead time: 3 Envelope (L×W×H): Ø165 × 40 Mass: 1000 g ## Antenna-feeder Device 475-2 — Glavkosmos [antennas] https://newspacemarket.com/products/antenna-feeder-device-475-2/ Design lifetime: 7 years Lead time: 12 Mass: 25000 g ## Antenna-feeder Device 77531 — Glavkosmos [antennas] https://newspacemarket.com/products/antenna-feeder-device-77531/ Design lifetime: 8 years Lead time: 6 Mass: 1000 g ## Antenna-feeder Device (AFD) Ionosphere — Glavkosmos [antennas] https://newspacemarket.com/products/antenna-feeder-device-afd-ionosphere/ Design lifetime: 8 years Lead time: 6 Mass: 4000 g ## Antenna-feeder Device (AFD) MBITS-01 — Glavkosmos [antennas] https://newspacemarket.com/products/antenna-feeder-device-afd-mbits-01/ Design lifetime: 8 years Lead time: 6 Mass: 2500 g ## Antenna-feeder Device BASN — Glavkosmos [antennas] https://newspacemarket.com/products/antenna-feeder-device-basn/ Design lifetime: 7 years Lead time: 5 Mass: 300 g ## Antenna-feeder Device BIS-MV — Glavkosmos [antennas] https://newspacemarket.com/products/antenna-feeder-device-bis-mv/ Design lifetime: 8 years Lead time: 6 Mass: 2000 g ## Antenna-feeder Device of Wideband Communication System — Glavkosmos [antennas] https://newspacemarket.com/products/antenna-feeder-device-of-wideband-communication-system/ Design lifetime: 10 years Design lifetime: 15 years @ (variant 2) Lead time: 20 Power consumption: 75 W Gain: 41 Mass: 55000 g TRL: 9 ## Antenna-feeder Device TKS — Glavkosmos [antennas] https://newspacemarket.com/products/antenna-feeder-device-tks/ Design lifetime: 8 years Lead time: 6 Mass: 1000 g ## C-band Antenna which Forms Planimetric Directional Diagram — Glavkosmos [antennas] https://newspacemarket.com/products/c-band-antenna-which-forms-planimetric-directional-diagram/ Design lifetime: 15 years Lead time: 15 Mass: 4700 g Mass: 8400 g @ (variant 2) ## C-band Global-beam Antenna — Glavkosmos [antennas] https://newspacemarket.com/products/c-band-global-beam-antenna/ Envelope (L×W×H): 1105×455 mm ## Cassegrainian Antenna — Glavkosmos [antennas] https://newspacemarket.com/products/cassegrainian-antenna/ Antenna type: Cassegrain Envelope (L×W×H): reflector max Ø – 2200 mm, reflector min Ø – 600 mm ## Deployable Reflector of Antenna with 4.2 m Aperture Diameter — Glavkosmos [antennas] https://newspacemarket.com/products/deployable-reflector-of-antenna-with-4-2-m-aperture-diameter/ Mass: 33500 g (max) Flight heritage: Flight-qualified ## Double-mirror Ka-band Parabolic Antenna — Glavkosmos [antennas] https://newspacemarket.com/products/double-mirror-ka-band-parabolic-antenna/ Mass: 10500 g ## Feed as a Component of the Ku-band Multiple-beam Antenna — Glavkosmos [antennas] https://newspacemarket.com/products/feed-as-a-component-of-the-ku-band-multiple-beam-antenna/ Antenna type: polarization selector, diplexer, hard and lightweight load-bearing structure with a temperature decoupling Mass: 13000 g Lead time: 12 ## Feed of the C-band Antenna which Forms Planimetric Directional Diagram — Glavkosmos [antennas] https://newspacemarket.com/products/feed-of-the-c-band-antenna-which-forms-planimetric-directional-diagram/ Lead time: 12 Mass: 16000 g ## Feed of the Large Ku-band Antenna System which Forms Planimetric Directional Diagram — Glavkosmos [antennas] https://newspacemarket.com/products/feed-of-the-large-ku-band-antenna-system-which-forms-planimetric-directional-diagram/ Mass: 6000 g ## Horn Antenna — Glavkosmos [antennas] https://newspacemarket.com/products/horn-antenna/ Antenna type: Smooth conical, crimped, modified Envelope (L×W×H): Ø in the deployed position – 410 mm, length – 1100 mm ## Ka-band Antenna for the Locator Beacon Signal Transmission — Glavkosmos [antennas] https://newspacemarket.com/products/ka-band-antenna-for-the-locator-beacon-signal-transmission/ Mass: 1300 g ## Ka-band High-precision Antenna — Glavkosmos [antennas] https://newspacemarket.com/products/ka-band-high-precision-antenna/ Mass: 6300 g ## Ku-band Multiple-beam Antenna — Glavkosmos [antennas] https://newspacemarket.com/products/ku-band-multiple-beam-antenna/ Design lifetime: 15 years Lead time: 15 ## Large Ku-band Antenna System which Forms Planimetric Directional Diagram — Glavkosmos [antennas] https://newspacemarket.com/products/large-ku-band-antenna-system-which-forms-planimetric-directional-diagram/ Design lifetime: 15 years Lead time: 15 Envelope (L×W×H): 3.5×2 m ## Mirror Antenna Reflector — Glavkosmos [antennas] https://newspacemarket.com/products/mirror-antenna-reflector/ Envelope (L×W×H): reflector max Ø – 2200 mm, reflector min Ø – 180 mm ## Mirror Antenna — Glavkosmos [antennas] https://newspacemarket.com/products/mirror-antenna/ Envelope (L×W×H): reflector max Ø – 1200 mm, reflector min Ø – 600 mm ## Offset Mirror Antenna — Glavkosmos [antennas] https://newspacemarket.com/products/offset-mirror-antenna/ Design lifetime: 15 years Lead time: 15 Envelope (L×W×H): reflector max Ø – 1800 mm, reflector min Ø – 180 mm ## P-band Global-beam Antenna — Glavkosmos [antennas] https://newspacemarket.com/products/p-band-global-beam-antenna/ Envelope (L×W×H): 1440×202 mm Mass: 10000 g ## Reflector as a Component of the Ku-band Multiple-beam Antenna — Glavkosmos [antennas] https://newspacemarket.com/products/reflector-as-a-component-of-the-ku-band-multiple-beam-antenna/ Design lifetime: 15 years Lead time: 12 Envelope (L×W×H): 2900×2030 mm Mass: 35000 g ## Reflector of the C-band Antenna which Forms Planimetric Directional Diagram — Glavkosmos [antennas] https://newspacemarket.com/products/reflector-of-the-c-band-antenna-which-forms-planimetric-directional-diagram/ Design lifetime: 15 years Lead time: 12 Envelope (L×W×H): 1830×790 mm Mass: 9000 g ## Reflector of the Large Ku-band Antenna System which Forms Planimetric Directional Diagram — Glavkosmos [antennas] https://newspacemarket.com/products/reflector-of-the-large-ku-band-antenna-system-which-forms-planimetric-directional-diagram/ Design lifetime: 15 years Lead time: 12 Envelope (L×W×H): 3500×2000 mm Envelope (L×W×H): 3850×1650 mm @ (variant 2) Mass: 2500 g ## UHF Antenna System with Service Panel — Glavkosmos [antennas] https://newspacemarket.com/products/uhf-antenna-system-with-service-panel/ Design lifetime: 1 years Lead time: 3 Mass: 60 g Connector: USB 3.0 micro Connector: Hirose GT8E @ (variant 2) ## X-band Transmit/Receive Antenna — Glavkosmos [antennas] https://newspacemarket.com/products/x-band-transmit-receive-antenna/ Gain: 31.4 (min) Envelope (L×W×H): 900×770 mm Mass: 6900 g Flight heritage: Not yet flight-qualified ## Antenna ANT-406VA — Glavkosmos [antennas] https://newspacemarket.com/products/antenna-ant-406va/ Design lifetime: 3 years Lead time: 3 Envelope (L×W×H): 240x238.34x60 Mass: 700 g ## Antenna AA2-KKS — Glavkosmos [antennas] https://newspacemarket.com/products/antenna-%d0%b0%d0%b02-%d0%ba%d0%ba%d1%81/ Gain: 33 Envelope (L×W×H): 80 × Ø120 mm Supply voltage: 5 Operating temperature: -50 °C Mass: 700 g Design lifetime: 3 years Flight heritage: Not yet flight-qualified ## Antenna AFU-NMSS M — Glavkosmos [antennas] https://newspacemarket.com/products/antenna-afu-nmss-m/ Design lifetime: 3 years Lead time: 3 Gain: 30 Envelope (L×W×H): 130x74x26.7 Mass: 350 g ## Antenna ASNG-2 — Glavkosmos [antennas] https://newspacemarket.com/products/antenna-asng-2/ Design lifetime: 3 years Lead time: 3 Gain: 35 Envelope (L×W×H): 91.5khØ178 Mass: 1500 g ## Antenna ASNG-3 — Glavkosmos [antennas] https://newspacemarket.com/products/antenna-asng-3/ Design lifetime: 3 years Lead time: 3 Envelope (L×W×H): 92.0khØ178 Mass: 2300 g ## Antenna ASNK-1 — Glavkosmos [antennas] https://newspacemarket.com/products/antenna-asnk-1/ Design lifetime: 3 years Lead time: 3 Gain: 30 Envelope (L×W×H): 47.5x44x19 Mass: 150 g ## Antenna ASNK-2 — Glavkosmos [antennas] https://newspacemarket.com/products/antenna-asnk-2/ Design lifetime: 3 years Lead time: 3 Gain: 30 Envelope (L×W×H): 47.5x44x19 Mass: 150 g ## Antenna ASNM-6 — Glavkosmos [antennas] https://newspacemarket.com/products/antenna-asnm-6/ Design lifetime: 3 years Lead time: 3 Gain: 25 Envelope (L×W×H): 60.3x60.3x18.5 Mass: 150 g ## Antenna ASNP-2 — Glavkosmos [antennas] https://newspacemarket.com/products/antenna-asnp-2/ Design lifetime: 3 years Lead time: 3 Gain: 25 Envelope (L×W×H): 36x36x10 Mass: 20 g ## Antenna ASNP-2M — Glavkosmos [antennas] https://newspacemarket.com/products/antenna-asnp-2m/ Design lifetime: 3 years Lead time: 3 Gain: 25 Envelope (L×W×H): 27x25x10.5 Mass: 50 g ## Antenna ASNP-4 — Glavkosmos [antennas] https://newspacemarket.com/products/antenna-asnp-4/ Design lifetime: 3 years Lead time: 3 Gain: 20 Envelope (L×W×H): 50 × 50 × 12 Mass: 50 g ## Antenna MAZ-M2 — Glavkosmos [antennas] https://newspacemarket.com/products/antenna-maz-m2/ Design lifetime: 3 years Lead time: 3 Gain: 30 Envelope (L×W×H): 101x101x62 Mass: 600 g ## Antenna SA2-M — Glavkosmos [antennas] https://newspacemarket.com/products/antenna-sa2-m/ Design lifetime: 3 years Lead time: 3 Envelope (L×W×H): 105xØ462 Mass: 5000 g ## VHF/UHF Antenna System 1 — ISISPACE Group [antennas] https://newspacemarket.com/products/isispace-vhf-uhf-antenna-system-1/ Mass: 90 g (max) Envelope (L×W×H): 98 x 98 x 7 mm (including aluminium cover plate) Power consumption: 0.04 W (max) Power consumption: 0.06 W (max) @ (variant 2) Operating temperature: -20 °C Operating temperature: -5 °C @ (variant 2) Power consumption: 2 W ## VHF/UHF Antenna System 2 — ISISPACE Group [antennas] https://newspacemarket.com/products/isispace-vhf-uhf-antenna-system-2/ Envelope (L×W×H): 98 x 98 mm (height depends on configuration) Power consumption: 0.08 W Power consumption: 2.3 W (max) Operating temperature: -20 °C Operating temperature: -5 °C @ (variant 2) Power consumption: 2 W @ (variant 2) Flight heritage: Since 2020 ## GNSS-701 — AAC Clyde Space [antennas] https://newspacemarket.com/products/aac-gnss-701/ Supply voltage: 3.3 Power consumption: 1 W (max) Operating temperature: -40 °C Survival temperature: -55 °C Envelope (L×W×H): ~90 x 90 x 15 mm Radiation tolerance (TID): 10 krad TRL: 9 Flight heritage: >20 missions ## CubeCAT — AAC Clyde Space [antennas] https://newspacemarket.com/products/aac-cubecat/ Supply voltage: 5 Operating temperature: -20 °C Envelope (L×W×H): ~100 x 100 x 20 mm Radiation tolerance (TID): 10 krad TRL: 8 ## Standard Gain Horn Antennas (SGH) — Anteral [antennas] https://newspacemarket.com/products/anteral-sgh/ Antenna type: Standard gain horn antenna ## Scalar Feed Horn Antennas (SFHA) — Anteral [antennas] https://newspacemarket.com/products/anteral-sfha/ Antenna type: Scalar feed horn antenna ## Lens Horn Antennas (LHA) — Anteral [antennas] https://newspacemarket.com/products/anteral-lha/ Antenna type: Dielectric lens horn antenna ## ANT-100 VHF/UHF Whip Antenna — AAC SpaceQuest (AAC Clyde Space subsidiary) [antennas] https://newspacemarket.com/products/aac-spacequest-ant-100/ Antenna type: Static whip antenna, tunable ## ANT-GPS L-Band GPS Patch Antenna — AAC SpaceQuest (AAC Clyde Space subsidiary) [antennas] https://newspacemarket.com/products/aac-spacequest-ant-gps/ Antenna type: Patch antenna ## MEGA Multi-Beam Electronic Antenna (MEOLUT Phased Array) — TTI Norte [antennas] https://newspacemarket.com/products/tti-norte-mega-phased-array-antenna/ Antenna type: Planar phased array, no moving parts ## Aurora Ka-Band Satcom Terminal — Thorium Space Technology [antennas] https://newspacemarket.com/products/thorium-aurora-satcom-terminal/ Operating temperature: -40 °C ## Commercial IFC Antennas — ThinKom Solutions, Inc. [antennas] https://newspacemarket.com/products/thinkom-thinair-ka2517/ Antenna type: High-torque brushless DC motors, no contacting parts, enables rapid satellite switching ## S-Band IoT Antenna Array — TALOS GmbH [antennas] https://newspacemarket.com/products/talos-sband-antenna-array/ Flight heritage: RAVEN microsatellite (launched 2026 on SpaceX Falcon 9) ## Taoglas GVLB208 Series (GVLB208 / AGVLB208.A) — Taoglas [antennas] https://newspacemarket.com/products/taoglas-gvlb208-dual-band-gnss-antenna/ Envelope (L×W×H): 20 x 20 x 8 mm Connector: I-PEX MHF I connector ## Storm MA410 4in1 Permanent Mount GPS/GLONASS/BeiDou & 2G/3G/4G & 2xMIMO & L-Band 1621MHz Antenna — Taoglas [antennas] https://newspacemarket.com/products/taoglas-storm-ma410-gnss-iridium-antenna/ Antenna type: SMA Antenna type: TGC-200 @ (variant 2) Connector: Straight Connector: Normal @ (variant 2) Mass: 440 g Gain: 5.9 ## Vireo Ka 288 — CesiumAstro [antennas] https://newspacemarket.com/products/cesiumastro-vireo-ka-288/ Power consumption: 361 W Flight heritage: Flight-qualified hardware shipping to Rocket Lab for SDA Tranche 2 Transport Layer; selected by Raytheon Technologies for SDA Tranche 1 Tracking Layer ## APEX Electronically Steered Antenna — Hanwha Phasor [antennas] https://newspacemarket.com/products/hanwha-phasor-apex-electronically-steered-antenna/ Antenna type: Flat-panel electronically steered antenna (ESA), phased array ## piPATCH-ADSB — SkyFox Labs s.r.o. [antennas] https://newspacemarket.com/products/skyfox-labs-pipatch-adsb/ Export status: controlled and needs special Export License approved by the Ministry of Industry and Trade of the Czech Republic (the local control entity), if exported outside EU-member states territory. The request for the Export License has to be submitted by the manu Antenna type: High Gain Non-Deployable ADS-B Antenna Envelope (L×W×H): 98x82.6x(+8/-4) mm, low profile, MCX-F connector ## Antenna-feeder system of the UHF band — SPUTNIX [antennas] https://newspacemarket.com/products/antenna-feeder-system-of-the-uhf-band/ Antenna type: monopole Antenna type: linear @ (variant 2) Envelope (L×W×H): 12.4 x 25 x 205 mm Mass: 21 g ## S band antenna-feeder system — SPUTNIX [antennas] https://newspacemarket.com/products/s-band-antenna-feeder-system/ Antenna type: Two-way spiral Antenna type: Circular, RHCP @ (variant 2) Envelope (L×W×H): 80 x 80 x 235 mm Mass: 190 g ## X band antenna-feeder system — SPUTNIX [antennas] https://newspacemarket.com/products/x-band-antenna-feeder-system/ Antenna type: Mirror Antenna type: Circular, RHCP @ (variant 2) Envelope (L×W×H): 138 x 317 x 317 mm Mass: 570 g ## Antenna-feeder system of global navigation satellite systems — SPUTNIX [antennas] https://newspacemarket.com/products/antenna-feeder-system-of-global-navigation-satellite-systems/ Antenna type: Printed Antenna type: Circular, RHCP @ (variant 2) Envelope (L×W×H): 68 x 68 x 15 mm Mass: 61 g ## Onyx Aero Terminal — MDA Space [antennas] https://newspacemarket.com/products/onyx-aero-terminal/ Antenna type: electronically steered, no moving parts ## Deployable Booms & Antennas — Astronika [antennas] https://newspacemarket.com/products/astronika-deployable-booms/ Antenna type: Tubular booms, antenna deployers, dual-wishbone Flight heritage: ESA JUICE, RadCube, multiple CubeSats ## S-Band Patch Antenna RHCP for HISPICO — IQ Spacecom [antennas] https://newspacemarket.com/products/s-band-patch-antenna-rhcp-for-hispico/ Lead time: 4 ## Helios deployable antenna — Helical Communication Technologies (HCT) [antennas] https://newspacemarket.com/products/helios-deployable-antenna/ Lead time: 90 ## CubeSat & SmallSat UHF Antenna System — NanoAvionics [antennas] https://newspacemarket.com/products/nanoavionics-uhf-antenna-system/ Antenna type: Turnstile / Quad-Monopole Connector: MCX (50 Ohm) Power consumption: 10 W ## CHORUS Deployable Antenna — 2NDSpace Srl [antennas] https://newspacemarket.com/products/chorus-01-deployable-antenna/ Gain: 0 (min) Supply voltage: 3.3 ## QHA Deployable Antenna — Helical Communication Technologies (HCT) [antennas] https://newspacemarket.com/products/hct-qha-deployable-antenna/ Antenna type: Quadrifilar Helical Antenna (QHA), deployable Flight heritage: Since December 2018, multiple missions ## Navishield Anti-Jam / Anti-Spoofing GNSS Antenna — Deimos Space (Indra) [antennas] https://newspacemarket.com/products/deimos-space-navishield/ Flight heritage: 25+ years on the European Galileo programme ## Satellite Antennas — Celestial Space Technologies [antennas] https://newspacemarket.com/products/cst-sband-patch-antenna/ Mass: 50 g (max) Mass: 40 g (max) @ (variant 2) ## Ka-Band High-Gain Antenna — Anywaves [antennas] https://newspacemarket.com/products/ka-band-high-gain-antenna/ Gain: 30 (min) Mass: 500 g (max) ## S-Band TT&C Antenna — Anywaves [antennas] https://newspacemarket.com/products/s-band-ttc-antenna/ Envelope (L×W×H): L 84.3 x W 84.3 x H 12.1 mm³ TRL: 9 Connector: 136 g ## GNSS Antenna for Small Satellites — Anywaves [antennas] https://newspacemarket.com/products/gnss-antenna-for-small-satellites/ Gain: 3 (min) Mass: 30 g (max) Operating temperature: -40-85 °C ## Horn Arrays — Optisys [antennas] https://newspacemarket.com/products/optisys-horn-arrays/ Flight heritage: Multiple designs on orbit ## BeamBox Expandable Antenna Communication Payload — NSLComm (BeetleSat) [antennas] https://newspacemarket.com/products/nslcomm-beambox-expandable-antenna-payload/ Antenna type: Proprietary deployable/expandable antenna ## Dual Band Helical Antenna — MMA Design [antennas] https://newspacemarket.com/products/mma-dual-band-helical-antenna/ Gain: 10 (min) Power consumption: 100 W Mass: 1500 g TRL: 8 ## NeuSAR — Deployable SAR Small Satellite Antenna — MMA Design [antennas] https://newspacemarket.com/products/mma-neusar-sar-antenna/ Mass: 160000 g Antenna type: Fully polarimetric SAR ## L.Garde Deployable Antennas — L.Garde Inc [antennas] https://newspacemarket.com/products/lgarde-inflatable-deployable-antennas/ Flight heritage: STS-77 (Inflatable Antenna Experiment - IAE) ## UDAN Deployable UHF-Helix Antenna — HPS High Performance Space Structure Systems [antennas] https://newspacemarket.com/products/hps-udan-uhf-antenna/ Envelope (L×W×H): 1U cube, <0.3 kg (antenna only) Gain: 10 (min) Design lifetime: 5 years Envelope (L×W×H): 50 cm height x 90 cm diameter @ (variant 2) ## Ku GEO User Terminal (Ku GEO 9dB/K) — Greenerwave [antennas] https://newspacemarket.com/products/greenerwave-ku-geo-terminal/ Envelope (L×W×H): ~54 x 63 x 11 cm Operating temperature: -40 °C Survival temperature: -40 °C ## Inflatable Antenna System — FreeFall Aerospace [antennas] https://newspacemarket.com/products/freefall-inflatable-antenna/ Antenna type: Spherical, inflatable membrane ## CatSat 10 GHz Patch Antenna — FreeFall Aerospace [antennas] https://newspacemarket.com/products/freefall-catsat-patch-antenna/ Antenna type: Patch antenna Flight heritage: Operational on CatSat since July 2024 ## SATCOM/VSAT Antenna Terminals — EUROSATCOM [antennas] https://newspacemarket.com/products/eurosatcom-satcom-vsat-terminals/ Envelope (L×W×H): 60 cm, 80 cm, 100 cm, 130 cm ## BADGER Broad Area Deployable Ground Terminal — AeroVironment (Tomahawk Robotics) [antennas] https://newspacemarket.com/products/bluehalo-badger-ground-terminal/ Operating temperature: -40 °C ## Curvalux 2 Active Antenna (WiFi 5-6.4 GHz) — Curvalux [antennas] https://newspacemarket.com/products/curvalux-2-active-antenna-wifi-5-6-4-ghz/ Power consumption: 100 W ## GA120C Geesatcom Satellite Antenna — Geespace [antennas] https://newspacemarket.com/products/ga120c-geesatcom-satellite-antenna/ Power consumption: 5 W (max) Envelope (L×W×H): 130 mm×130 mm×33 mm ## GA080L Geesatcom Satellite Antenna — Geespace [antennas] https://newspacemarket.com/products/ga080l-geesatcom-satellite-antenna/ Antenna type: Rod-type antenna with a compact and durable structure Power consumption: 5 W Envelope (L×W×H): Ø18 mm x 85 mm ## Ku GEO — Greenerwave [antennas] https://newspacemarket.com/products/ku-geo-user-terminal/ Envelope (L×W×H): ~ 54 cm x 63 cm x 11 cm Operating temperature: -40 °C Survival temperature: -40 °C ## Ku GEO/LEO 9 dB/K — Greenerwave [antennas] https://newspacemarket.com/products/ku-geo-leo-multi-orbit-user-terminal-9-db-k/ Envelope (L×W×H): ~ 54 cm x 63 cm x 11 cm Operating temperature: -40 °C Survival temperature: -40 °C ## Reshapable Mesh Reflector Antenna — Mithril Technologies [antennas] https://newspacemarket.com/products/mithril-reshapable-mesh-reflector-antenna/ Envelope (L×W×H): 1-meter ## Vast Parabolic Satellite Antenna — Shaanxi NewStar Communications [antennas] https://newspacemarket.com/products/shaanxi-newstar-vast-antenna/ Antenna type: Parabolic dish antennas, ground station equipment ## Comsat Systems Satellite Communication Antenna Systems — Comsat Systems [antennas] https://newspacemarket.com/products/comsat-systems-satcom-equipment/ Antenna type: Fixed, Static, Non-penetrating, Transportable, Mobile (including Mobile VSATs for SNG and OB vans) Envelope (L×W×H): Over 20,000 sq. ft. ## KSPA-U UHF/VHF Patch Antenna — Kairo Space [antennas] https://newspacemarket.com/products/kairo-space-kspa-u/ Antenna type: Patch antenna ## Liquid Crystal Flat Panel Antenna — ALCAN Systems [antennas] https://newspacemarket.com/products/alcan-systems-lc-antenna/ Antenna type: Electronically steerable flat-panel (liquid crystal phase shifters) ## Mobile VSAT Satellite Antenna Systems — C-COM Satellite Systems [antennas] https://newspacemarket.com/products/ccom-mobile-vsat/ Envelope (L×W×H): 75 cm – 1.2 m ## BeetleSat Expandable Ka-band Parabolic Antenna — NSLComm (BeetleSat) [antennas] https://newspacemarket.com/products/beetlesat-expandable-ka-band-antenna/ Antenna type: Ka-band deployable parabolic reflector ## S-Band Patch Antenna — Innovative Space Logistics [antennas] https://newspacemarket.com/products/s-band-patch-antenna-1478/ Mass: 60 g (max) Envelope (L×W×H): Diameter: 80 mm Envelope (L×W×H): Height (without connector): 5.0 mm @ (variant 2) Envelope (L×W×H): Connector height (straight ): 9.5 mm @ (variant 3) Operating temperature: -20-50 °C Power consumption: 2 W ## S-band TMTC antenna — Innovative Space Logistics [antennas] https://newspacemarket.com/products/isispace-s-band-tmtc-antenna-1478/ Mass: 60 g (max) Envelope (L×W×H): Diameter: 78 mm Height (with connector): 16.0 mm Operating temperature: -20-60 °C Gain: 6 (min) Beamwidth: 100 Power consumption: 2 W ## ISISPACE GNSS Patch Antenna — Innovative Space Logistics [antennas] https://newspacemarket.com/products/isispace-gnss-patch-antenna-1478/ Mass: 20 g (max) Envelope (L×W×H): 58 x 58 x 9.7 mm Operating temperature: -20 °C Gain: 34.5 Supply voltage: 3-5 ## VHF/UHF antenna for 1U-3U — Innovative Space Logistics [antennas] https://newspacemarket.com/products/isispace-vhf-uhf-antenna-for-1u-3u-1478/ Mass: 90 g (max) Envelope (L×W×H): 98 x 98 x 7 mm Power consumption: 0.04 W (max) Supply voltage: 3 Power consumption: 0.06 W (max) @ (variant 2) Supply voltage: 5 @ (variant 2) Power consumption: 2 W Operating temperature: -20 °C Operating temperature: -5 °C @ (variant 2) ## VHF/UHF Antenna for 6U+ — Innovative Space Logistics [antennas] https://newspacemarket.com/products/vhf-uhf-antenna-for-6u-1478/ Mass: 90-115 g Envelope (L×W×H): 98×98 mm Power consumption: 0.08 W Power consumption: 2.3 W (max) Operating temperature: -20 °C Operating temperature: -5 °C @ (variant 2) Gain: 0 Gain: 0 @ (variant 2) Power consumption: 2 W @ (variant 2) ## VHF/UHF Antenna for 6U+ — ISISPACE Group [antennas] https://newspacemarket.com/products/vhf-uhf-antenna-for-6u/ Envelope (L×W×H): 98×98 mm (height depends on configuration) Power consumption: 0.08 W Power consumption: 2.3 W (max) Operating temperature: -20 °C Operating temperature: -5 °C @ (variant 2) ## S-Band Antenna Commercial — EnduroSat [antennas] https://newspacemarket.com/products/s-band-antenna-commercial/ Beamwidth: 70 Mass: 77.4 g ## UHF ANTENNA 2U — EnduroSat [antennas] https://newspacemarket.com/products/uhf-antenna-2u/ Antenna type: Omnidirectional Gain: 0 (min) Power consumption: 2 W Mass: 210 g ## S-BAND ANTENNA WIDEBAND — EnduroSat [antennas] https://newspacemarket.com/products/s-band-antenna-wideband/ Beamwidth: 70 Gain: 5 ## X-Band Patch Antenna — EnduroSat [antennas] https://newspacemarket.com/products/x-band-patch-antenna/ Connector: SMP (SMA for 8x12 Array) Antenna type: 6 dBi Antenna type: 74° @ (variant 2) Antenna type: 24 mm x 24 mm x 5.62 mm @ (variant 3) Antenna type: 2.2 g @ (variant 4) Antenna type: 12 dBi @ (variant 5) Antenna type: 16 dBi @ (variant 6) ## K-BAND 4×4 PATCH ARRAY — EnduroSat [antennas] https://newspacemarket.com/products/k-band-4x4-patch-array/ Beamwidth: 16 Mass: 76 g ## S-Band Antenna ISM — EnduroSat [antennas] https://newspacemarket.com/products/s-band-antenna-ism/ Beamwidth: 71 Gain: 7.5 (min) Mass: 71 g ## Compact S-Band TT&C Antenna — Anywaves [antennas] https://newspacemarket.com/products/compact-s-band-ttc-antenna/ Envelope (L×W×H): L 70.9 × W 70.9 × H 30.33 mm (connectors included) TRL: 8 Connector: < 106 g ## Compact X-Band Payload Telemetry Antenna — Anywaves [antennas] https://newspacemarket.com/products/compact-x-band-payload-telemetry-antenna/ Envelope (L×W×H): L 100 × W 100 × H 16.2 mm (protruding height: 6.5 mm) Gain: 15.5 TRL: 9 Connector: 67.5 g (±4 g) ## Choke Ring Ka-band TT&C Antenna — Anywaves [antennas] https://newspacemarket.com/products/choke-ring-ka-band-ttc-antenna/ TRL: 7 Envelope (L×W×H): Option 1 : (Rx) 108 × 108 × 44 mm Option 2 : (Tx) 150 × 150 × 60 mm Option 3 : (Rx/Tx) 90 × 90 × 40 mm ## High Gain X-Band Payload Telemetry Antenna — Anywaves [antennas] https://newspacemarket.com/products/high-gain-x-band-payload-telemetry-antenna/ Gain: 20 (min) Envelope (L×W×H): L 200 × W 200 × H 16 mm TRL: 5 Connector: 503 g ± 20% ## Wide Beam X-Band Payload Telemetry Antenna — Anywaves [antennas] https://newspacemarket.com/products/wide-beam-x-band-payload-telemetry-antenna/ Envelope (L×W×H): L 100 × W 100 × H 16.2 mm TRL: 8 Connector: 67.5 g (±3 g) ## GNSS All-Bands Antenna with LNA Integrated Board — Anywaves [antennas] https://newspacemarket.com/products/gnss-all-bands-antenna-with-lna-integrated-board/ Envelope (L×W×H): L 99 × W 99 × H 58 mm TRL: 7 Mass: 285 g ## GNSS L1/E1 Bands Antenna — Anywaves [antennas] https://newspacemarket.com/products/gnss-l1-e1-bands-antenna/ Envelope (L×W×H): L 96.6 × W 96.6 × H 23.75 mm TRL: 8 Connector: 103 g ± 5 g ## GNSS All-Bands Launcher Antenna — Anywaves [antennas] https://newspacemarket.com/products/gnss-all-bands-launcher-antenna/ Envelope (L×W×H): 150 × 150 × 30 mm TRL: 8 Connector: Antenna: 162 g ± 8 g Flat mechanical bracket: 106 g Thermal shield: 62 g ## GNSS All-Bands Antenna — Anywaves [antennas] https://newspacemarket.com/products/gnss-all-bands-antenna/ Envelope (L×W×H): 99.4 × 99.4 × 16.2 mm (external protruding height: 8.6 mm) TRL: 9 Connector: 125.7 g ± 6 g ## Compact X-Band Dual Polarized Antenna — Anywaves [antennas] https://newspacemarket.com/products/compact-x-band-dual-polarized-antenna/ Envelope (L×W×H): L 100 × W 100 × H 26.8 mm (external protruding height: 9.31 mm) TRL: 7 Connector: 153.5 g ± 8 g ## Slotted Waveguide Array Antenna — Anywaves [antennas] https://newspacemarket.com/products/slotted-waveguide-array-antenna/ TRL: 5 ## Reflectarray Antenna — Anywaves [antennas] https://newspacemarket.com/products/reflectarray-antenna/ Envelope (L×W×H): 360 × 210 × 30 mm (compact stowed volume for launch) TRL: 9 ## Quad-Ridged Horn Antenna — Anywaves [antennas] https://newspacemarket.com/products/quad-ridged-horn-antenna/ Envelope (L×W×H): S+C band version: < 110 × 110 × 200 mm C+X band version: < 60 × 60 × 150 mm TRL: 8 ## Compact Wideband Antennas — Anywaves [antennas] https://newspacemarket.com/products/compact-wideband-antennas/ Envelope (L×W×H): <1U footprint TRL: 9 ## Quadrifilar Helix Antenna — Anywaves [antennas] https://newspacemarket.com/products/quadrifilar-helix-antenna/ TRL: 9 ## NanoCom AM2150-P/PS — GomSpace [antennas] https://newspacemarket.com/products/nanocom-am2150-p-ps/ Gain: -12 (min) Gain: 0 (min) @ (variant 2) Connector: MCX Coaxial Mass: 100 g (max) ## Deployable Helical Antennas — Oxford Space Systems [antennas] https://newspacemarket.com/products/deployable-helical-antennas/ Flight heritage: Yes (In-Space Missions) ## piPATCH-AllBand/FM (Flight Model) — SkyFox Labs s.r.o. [antennas] https://newspacemarket.com/products/pipatch-allband-fm-flight-model/ Envelope (L×W×H): 98x82.6 mm Mass: 133 g ## piPATCH-DualBand/FM (Flight Model) — SkyFox Labs s.r.o. [antennas] https://newspacemarket.com/products/pipatch-dualband-fm-flight-model/ Envelope (L×W×H): 98x82.6 mm Mass: 75 g Connector: MCX-F ## piPATCH-L1L2/FM (Flight Model) — SkyFox Labs s.r.o. [antennas] https://newspacemarket.com/products/pipatch-l1l2-fm-flight-model/ Mass: 70 g Envelope (L×W×H): 98x82.6 mm Connector: MCX-F ## nanoPATCH-L1/FM (Flight Model) — SkyFox Labs s.r.o. [antennas] https://newspacemarket.com/products/nanopatch-l1-fm-flight-model/ Envelope (L×W×H): 50x50 mm TRL: 9 ## piPATCH-L1E1/FM (Flight Model) — SkyFox Labs s.r.o. [antennas] https://newspacemarket.com/products/pipatch-l1e1-fm-flight-model/ Envelope (L×W×H): 98x98 mm, low profile, MCX-F connector TRL: 9 ## piPATCH-LG/FM (Flight Model) — SkyFox Labs s.r.o. [antennas] https://newspacemarket.com/products/pipatch-lg-fm-flight-model/ Envelope (L×W×H): 98x98 mm, low profile TRL: 9 Connector: MCX-F ## miniPATCH-L1/FM (Flight Model) — SkyFox Labs s.r.o. [antennas] https://newspacemarket.com/products/minipatch-l1-fm-flight-model/ Envelope (L×W×H): 75x75 mm TRL: 9 ## piPATCH-MAX/FM (Flight Model) — SkyFox Labs s.r.o. [antennas] https://newspacemarket.com/products/pipatch-max-fm-flight-model/ Envelope (L×W×H): 74x74x13 mm Connector: Female SMA straight RF TRL: 9 ## microPATCH-L1/FM (Flight Model) — SkyFox Labs s.r.o. [antennas] https://newspacemarket.com/products/micropatch-l1-fm-flight-model/ Antenna type: ACTIVE Antenna with LNA Envelope (L×W×H): 82x36 mm, low profile Connector: MCX connector ## High-capacity Rechargeable Battery for Power Supply of Spacecraft and Ground Infrastructure — Glavkosmos [batteries] https://newspacemarket.com/products/high-capacity-rechargeable-battery-for-power-supply-of-spacecraft-and-ground-infrastructure/ Design lifetime: 5 years Lead time: 4 Capacity: 90 Wh Supply voltage: 27.6 Capacity: 30.3 Wh @ (variant 2) Capacity: 34.6 Wh @ (variant 3) Envelope (L×W×H): 500 x 278 x 619 mm Mass: 82000 g ## Nanosatellite Battery Array — Glavkosmos [batteries] https://newspacemarket.com/products/nanosatellite-battery-array/ Design lifetime: 1 years Lead time: 6 Supply voltage: 14.8 ## Rechargeable Battery for Power Supply of Spacecraft and Ground Infrastructure — Glavkosmos [batteries] https://newspacemarket.com/products/rechargeable-battery-for-power-supply-of-spacecraft-and-ground-infrastructure/ Design lifetime: 5 years Lead time: 4 Capacity: 20 Wh Supply voltage: 23.8 Envelope (L×W×H): 472 x 264 x 82.5 mm Mass: 14500 g ## Rechargeable Battery for Power Supply of Spacecraft — Glavkosmos [batteries] https://newspacemarket.com/products/rechargeable-battery-for-power-supply-of-spacecraft/ Design lifetime: 2 years Lead time: 4 Capacity: 90 Wh Supply voltage: 28.8 Capacity: 35 Wh @ (variant 2) Capacity: 37.8 Wh @ (variant 3) Envelope (L×W×H): 465 x 530 x 278 mm Mass: 74000 g ## BAT module — Space Inventor ApS [batteries] https://newspacemarket.com/products/battery-bat-28-p4/ Supply voltage: 14.4 Supply voltage: 28.8 @ (variant 2) Capacity: 100 Wh ## EXA BA0x High Energy Density Battery Array — EXA (Ecuadorian Space Agency) [batteries] https://newspacemarket.com/products/exa-ba0x-high-energy-density-battery-array/ Lead time: 4-6 ## EXA TITAN-1 350Whr High Energy Density Battery Matrix — EXA (Ecuadorian Space Agency) [batteries] https://newspacemarket.com/products/exa-titan-1-350whr-high-energy-density-battery-matrix/ Lead time: 6-8 ## B14-M45/M90 14V Modular SmallSat Battery — ibeos [batteries] https://newspacemarket.com/products/ibeos-b14-m45-m90-14v-battery/ Supply voltage: 13.2-16.8 Power consumption: 8 W Envelope (L×W×H): 94.5 x 84.1 x 23.1 mm Mass: 375 g (max) Operating temperature: 10-45 °C Operating temperature: 0-45 °C @ (variant 2) Radiation tolerance (TID): 30 krad TRL: 9 ## B28-135 28V SmallSat Battery — ibeos [batteries] https://newspacemarket.com/products/ibeos-b28-135-battery/ Capacity: 135 Wh Supply voltage: 22-33.6 Power consumption: 20 W Envelope (L×W×H): 94.5 x 88.7 x 51 mm Mass: 850 g (max) Operating temperature: 0-45 °C Radiation tolerance (TID): 30 krad Connector: 21-Pin Micro-D ## B28-M275/550/825/1100 28V Modular Battery Series — ibeos [batteries] https://newspacemarket.com/products/ibeos-b28-m-modular-battery/ Supply voltage: 24-33.6 Mass: 2100-7800 g Radiation tolerance (TID): 30 krad TRL: 9 ## B50-412/825/1237 50V Modular Battery Series — ibeos [batteries] https://newspacemarket.com/products/ibeos-b50-modular-battery/ Supply voltage: 36-50.4 Mass: 3000-8800 g Radiation tolerance (TID): 30 krad ## VES16 Cell — Saft [batteries] https://newspacemarket.com/products/saft-ves16-cell/ Cell chemistry: Li-ion NCA Capacity: 4.5 Wh Capacity: 16 Wh @ (variant 2) Capacity: 155 Wh (min) Supply voltage: 2.7-4.1 Mass: 112 g (max) Design lifetime: 12 years (min) ## 4S1P VES16 Battery — Saft [batteries] https://newspacemarket.com/products/saft-4s1p-ves16-battery/ Cell chemistry: Li-ion Capacity: 4.5 Wh Capacity: 64 Wh @ (variant 2) Supply voltage: 13.2-16.4 Mass: 700 g Design lifetime: 5 years (min) Survival temperature: -20-40 °C Connector: MDMA 37P ## VES16 8S4P Battery — Saft [batteries] https://newspacemarket.com/products/saft-ves16-8s4p-battery/ Cell chemistry: Li-ion Capacity: 18 Wh Capacity: 512 Wh @ (variant 2) Supply voltage: 25-32.8 Mass: 5000 g ## VES16 11S16P Battery — Saft [batteries] https://newspacemarket.com/products/saft-ves16-11s16p-battery/ Cell chemistry: Li-ion Capacity: 288 Wh Capacity: 11264 Wh @ (variant 2) Supply voltage: 29.7-45.1 Mass: 28800 g ## MP & VL Batteries for Launchers — Saft [batteries] https://newspacemarket.com/products/saft-mp-vl-batteries-launchers/ Cell chemistry: Li-ion Operating temperature: -20-60 °C Operating temperature: -50-60 °C @ (variant 2) ## VL51ES Li-Ion Battery for GEO and MEO — Saft [batteries] https://newspacemarket.com/products/saft-vl51es-battery-geo-meo/ Cell chemistry: VL51ES Li-ion cylindrical cell ## 1U Battery Board — CubeSat Aerospace [batteries] https://newspacemarket.com/products/1u-battery-board-3654/ Connector: FFC ribbon cable to avionics and power bus ## Lithium-Ion Battery Pack — Shenzhen MagicCubeSat Technology (MCS) [batteries] https://newspacemarket.com/products/mcs-lithium-ion-battery-pack/ Cell chemistry: Lithium-ion ## 50V Battery — ibeos [batteries] https://newspacemarket.com/products/50v-battery/ Supply voltage: 50 ## Satellite Multiband Imaging System — Glavkosmos [cameras] https://newspacemarket.com/products/satellite-multiband-imaging-system/ Lead time: 24 Swath width: 2 km ## Space-borne Television System — Glavkosmos [cameras] https://newspacemarket.com/products/space-borne-television-system/ Design lifetime: 5 years Lead time: 24 Envelope (L×W×H): up to 2048 × 2048 ## CASPEX 4Mpx Space Camera Head — 3D Plus (HEICO) [cameras] https://newspacemarket.com/products/3d-plus-caspex-4mpx-space-camera-head/ Operating temperature: -40 °C Radiation tolerance (TID): 30 krad (min) Envelope (L×W×H): 35 × 35 × 23 mm³ Mass: 64 g ## CASPEX 12Mpx Space Camera Head — 3D Plus (HEICO) [cameras] https://newspacemarket.com/products/3d-plus-caspex-12mpx-space-camera-head/ Operating temperature: -55 °C Radiation tolerance (TID): 40 krad (min) Envelope (L×W×H): 40 × 40 × 39 mm³ Mass: 120 g ## CASPEX 1.3Mpx SWIR Space Camera Head — 3D Plus (HEICO) [cameras] https://newspacemarket.com/products/3d-plus-caspex-1-3mpx-swir-space-camera-head/ Operating temperature: -55 °C Radiation tolerance (TID): 40 krad (min) Envelope (L×W×H): 40 × 40 × 44 mm³ Mass: 140 g ## Enabler Multispectral Telescope — Aistech Space [cameras] https://newspacemarket.com/products/aistech-enabler-telescope/ Swath width: 7 km Swath width: 18 km @ (variant 2) ## C3D CubeSat Camera — XCAM [cameras] https://newspacemarket.com/products/xcam-c3d-cubesat-camera/ Envelope (L×W×H): 5.3 um Sensor resolution: 1280 Envelope (L×W×H): 9.5 x 9.1 x 2.7 cm @ (variant 2) Mass: 85 g Power consumption: 0.845 W Operating temperature: -25-65 °C Survival temperature: -35-75 °C TRL: 9 ## NuSCIS Space Camera — XCAM [cameras] https://newspacemarket.com/products/xcam-nuscis-space-camera/ Envelope (L×W×H): 9.5 x 9.1 x 2.7 cm Power consumption: 4 W Operating temperature: -30-65 °C Survival temperature: -40-85 °C Design lifetime: 3 years ## SMC — Spacecraft Monitoring Camera — Tsd-space [cameras] https://newspacemarket.com/products/tsd-space-smc-spacecraft-monitoring-camera/ Power consumption: 5 W (max) ## SMC – Spacecraft Monitoring Camera — Tsd-space [cameras] https://newspacemarket.com/products/tsd-space-prisma-camera-system/ Envelope (L×W×H): ~1U Mass: 900 g Power consumption: 5 W (max) Radiation tolerance (TID): 20 krad (min) Flight heritage: Successfully launched aboard the HERA Spacecraft in October 2024 ## 710 Series Hyperspectral Cameras (HyCore / OmniCore VNIR) — Surface Optics Corporation [cameras] https://newspacemarket.com/products/surface-optics-710-series-hyperspectral-cameras/ Spectral bands: 784 Spectral bands: 1500 @ (variant 2) Connector: USB 3.0 Micro-B ## TriScape50 — Simera Sense [cameras] https://newspacemarket.com/products/simera-sense-triscape50/ Ground sample distance: 30 m Swath width: 120 km Focal length: 93.9 Envelope (L×W×H): 5.5 µm Operating temperature: -10 °C ## TriScape100 — Simera Sense [cameras] https://newspacemarket.com/products/simera-sense-triscape100/ Ground sample distance: 4.75 m Swath width: 19.4 km Focal length: 580 Envelope (L×W×H): 5.5 µm Operating temperature: -10 °C ## MultiScape50 — Simera Sense [cameras] https://newspacemarket.com/products/simera-sense-multiscape50/ Ground sample distance: 30 m Swath width: 120 km Focal length: 93.9 Envelope (L×W×H): 5.5 µm Operating temperature: -10 °C ## MultiScape100 — Simera Sense [cameras] https://newspacemarket.com/products/simera-sense-multiscape100/ Focal length: 580 Envelope (L×W×H): 5.5 µm Operating temperature: -10 °C ## HyperScape50 — Simera Sense [cameras] https://newspacemarket.com/products/simera-sense-hyperscape50/ Focal length: 93.9 Envelope (L×W×H): 5.5 µm Operating temperature: -10 °C Spectral bands: 32 ## HyperScape100 — Simera Sense [cameras] https://newspacemarket.com/products/simera-sense-hyperscape100/ Ground sample distance: 4.75 m Swath width: 19.4 km Focal length: 580 Envelope (L×W×H): 5.5 µm Operating temperature: -10 °C ## Holmes Mk2 Non-Earth Imaging Camera — HEO Robotics [cameras] https://newspacemarket.com/products/heo-robotics-holmes-mk2/ Ground sample distance: 0.34 m Mass: 3800 g Power consumption: 7 W ## Adler Mk2 Non-Earth Imaging Camera — HEO Robotics [cameras] https://newspacemarket.com/products/heo-robotics-adler-mk2/ Ground sample distance: 0.22 m Mass: 8500 g Power consumption: 7 W ## Scanway Camera System (SCS) — Scanway S.A. [cameras] https://newspacemarket.com/products/scanway-camera-system-scs/ Lead time: 0 ## Eagle 47-10 Space Camera — Raptor Photonics [cameras] https://newspacemarket.com/products/raptor-eagle-47-10/ Envelope (L×W×H): 13 µm x 13 µm Flight heritage: Flying on multiple LEO CubeSat missions (160–2,000 km), >36 months operational ## RCMOS Space Camera — Raptor Photonics [cameras] https://newspacemarket.com/products/raptor-rcmos-space-camera/ Flight heritage: Operational on LEO CubeSat missions ## Crystalspace C1U CubeSat Camera — Crystal Space [cameras] https://newspacemarket.com/products/cs-101-kikas-micro-camera-system/ Mass: 50 g (max) Envelope (L×W×H): 42 x 25 x 45 mm Power consumption: 0.075 W Power consumption: 0.24 W @ (variant 2) Operating temperature: -30-75 °C TRL: 9 ## CS-151 Kodas Monitoring Camera — Crystal Space [cameras] https://newspacemarket.com/products/cs-151-kodas-monitoring-camera/ Mass: 270 g Envelope (L×W×H): 82 x 88 x 39 mm Power consumption: 0.5 W Power consumption: 1 W @ (variant 2) Operating temperature: -30-75 °C Flight heritage: Maxar SAMPLR lunar lander (NASA Artemis) ## Lynx4MP — Infinity Avionics [cameras] https://newspacemarket.com/products/infinity-avionics-lynx4mp-10/ Envelope (L×W×H): 5.5 µm Power consumption: 2.75 W Envelope (L×W×H): 95 mm × 95 mm × 21 mm @ (variant 2) Mass: 255 g Operating temperature: -10 °C TRL: 9 Envelope (L×W×H): 5.5 µm @ (variant 3) Focal length: 10 Power consumption: 2.75 W @ (variant 2) Envelope (L×W×H): 95 mm × 95 mm × 101 mm @ (variant 4) Mass: 535 g @ (variant 2) Operating temperature: -10 °C @ (variant 2) TRL: 9 @ (variant 2) Envelope (L×W×H): 5.5 µm @ (variant 5) Focal length: 70 @ (variant 2) Power consumption: 2.75 W @ (variant 3) Envelope (L×W×H): 95 mm × 95 mm × 111 mm @ (variant 6) Mass: 595 g @ (variant 3) Operating temperature: -10 °C @ (variant 3) TRL: 9 @ (variant 3) Focal length: 550 @ (variant 3) Envelope (L×W×H): 100 mm x 100 mm x 250 mm @ (variant 7) Mass: 1500 g @ (variant 4) ## Scanway Optical Payload (SOP) — Scanway S.A. [cameras] https://newspacemarket.com/products/scanway-sop-200/ Ground sample distance: 1-25 m Lead time: 0 ## HRVI-2HD High-Resolution Imager — Berlin Space Technologies [cameras] https://newspacemarket.com/products/bst-hrvi-2hd-camera/ Swath width: 15 km Mass: 19000 g ## HRVI-6HD 2nd Gen High-Resolution Imager — Berlin Space Technologies [cameras] https://newspacemarket.com/products/bst-hrvi-6hd-camera/ Swath width: 70 km Mass: 10450 g ## ContextCAM — HD Real-Time Ethernet Video Camera — MVP Aerospace [cameras] https://newspacemarket.com/products/mvp-aerospace-contextcam/ Mass: 12 g Envelope (L×W×H): 45 × 35 × 17 mm ## HyperScout 2 — cosine (Berlin Adlershof) [cameras] https://newspacemarket.com/products/cosine-hyperscout-2/ Ground sample distance: 75 m Ground sample distance: 490 m @ (variant 2) Swath width: 310 km Mass: 1700 g Power consumption: 12 W ## T-Scout — cosine (Berlin Adlershof) [cameras] https://newspacemarket.com/products/cosine-tscout/ Focal length: 100 Envelope (L×W×H): 17 µm Envelope (L×W×H): 95 x 95 x 160 mm @ (variant 2) Power consumption: 10 W Mass: 1800 g ## 5m panchromatic(PAN) & 8-Band multispectral(MS) camera — MinoSpace [cameras] https://newspacemarket.com/products/minospace-camera-5m-pan-8band-ms/ Spectral bands: 8 ## XIOPM Space Optical Instruments — Xi’an Institute of Optics and Precision Mechanics (XIOPM) [cameras] https://newspacemarket.com/products/xiopm-space-optical-instruments/ Flight heritage: Earth observation, lunar missions, Tiangong Space Station ## KSOI-22 Optical Imager (22 mm) — Kairo Space [cameras] https://newspacemarket.com/products/kairo-space-ksoi-22/ Focal length: 22 ## KSOI-22C Optical Imager (22 mm Compact) — Kairo Space [cameras] https://newspacemarket.com/products/kairo-space-ksoi-22c/ Focal length: 22 ## C-RED New Space SWIR Camera Core — First Light Imaging [cameras] https://newspacemarket.com/products/first-light-imaging-c-red-new-space/ Envelope (L×W×H): 640 x 512 pixels (0.3 Mp), InGaAs ## C-RED 2 SWIR Camera — First Light Imaging [cameras] https://newspacemarket.com/products/first-light-imaging-c-red-2/ Envelope (L×W×H): 640 x 512 pixels, InGaAs PIN photodiode ## C-RED 2 ER Extended SWIR Camera — First Light Imaging [cameras] https://newspacemarket.com/products/first-light-imaging-c-red-2-er/ Envelope (L×W×H): 640 x 512 pixels ER-InGaAs ## C-RED 2 Lite SWIR Camera — First Light Imaging [cameras] https://newspacemarket.com/products/first-light-imaging-c-red-2-lite/ Envelope (L×W×H): 640 x 512 pixels, InGaAs PIN photodiode ## C-RED 3 SWIR Camera — First Light Imaging [cameras] https://newspacemarket.com/products/first-light-imaging-c-red-3/ Envelope (L×W×H): 640 x 512 pixels, InGaAs PIN photodiode ## CubeSat Camera- RavenEye16 — CAVU Aerospace [cameras] https://newspacemarket.com/products/cubesat-camera-raveneye16/ Mass: 1100 g Envelope (L×W×H): 60 mm Envelope (L×W×H): 3.4 µm @ (variant 2) Ground sample distance: 4.25 m Swath width: 10.4 km Envelope (L×W×H): 200 mm ☓ 96 mm ☓ 96 mm @ (variant 3) Supply voltage: 12 Radiation tolerance (TID): 30 krad ## piCAM/FM (Flight Model) — SkyFox Labs s.r.o. [cameras] https://newspacemarket.com/products/picam-fm-flight-model/ Connector: 6 pin Molex Envelope (L×W×H): 33x33x19 mm body + optics TRL: 9 ## Leo2MP Monitor Camera with Image Streaming — Infinity Avionics [cameras] https://newspacemarket.com/products/leo2mp-monitor-camera-with-image-streaming/ Envelope (L×W×H): 2.2 µm Focal length: 1 Envelope (L×W×H): 45 mm × 45 mm × 20 mm @ (variant 2) Mass: 65 g Operating temperature: -20 °C ## QuadPack Deployer — ISISPACE Group [deployers] https://newspacemarket.com/products/isispace-quadpack-deployer/ Mass: 6600-8100 g Envelope (L×W×H): 12UXL: 272 x 273 x 434.4 mm; 16U: 272 x 273 x 524.5 mm Envelope (L×W×H): 12UXL: 365.4 x 273 x 547.7 mm; 16U: 365.4 x 273 x 635.8 mm @ (variant 2) Flight heritage: 10+ years, 100% success rate ## DuoPack Deployer — ISISPACE Group [deployers] https://newspacemarket.com/products/isispace-duopack-deployer/ Mass: 4100-4800 g Envelope (L×W×H): 272 x 193.4 x 445.7 mm Envelope (L×W×H): 272 x 146.7 x 432.4 mm @ (variant 2) Flight heritage: 10+ years ## Manual Deployer of Pico and Nanosatellites — Glavkosmos [deployers] https://newspacemarket.com/products/manual-deployer-of-pico-and-nanosatellites/ Design lifetime: 5 years Lead time: 6 Separation velocity: 0.25-0.5 m/s Actuation: 2.5 Envelope (L×W×H): 400 × 435 × 160 mm ## Retractable Mast Mechanism — Glavkosmos [deployers] https://newspacemarket.com/products/retractable-mast-mechanism/ Design lifetime: 10 years Lead time: 6 Operating temperature: -40-50 °C Design lifetime: 10 years @ (variant 2) Design lifetime: 14.5 years @ (variant 3) Envelope (L×W×H): 252 × 252 × 4100 mm Mass: 12000 g ## Single-actuation Drive. Type 1 — Glavkosmos [deployers] https://newspacemarket.com/products/single-actuation-drive-type-1/ Lead time: 6 Actuation: 50-75 Operating temperature: -50-60 °C Envelope (L×W×H): 70 × 94 × 92 mm Mass: 750 g ## Single-actuation Drive. Type 2 — Glavkosmos [deployers] https://newspacemarket.com/products/single-actuation-drive-type-2/ Lead time: 6 Actuation: 45-80 Operating temperature: -50-70 °C Envelope (L×W×H): 75 × 90 × 70 mm Mass: 600 g ## Single-actuation Drive. Type 3 — Glavkosmos [deployers] https://newspacemarket.com/products/single-actuation-drive-type-3/ Lead time: 6 Actuation: 50-75 Operating temperature: -50-60 °C Envelope (L×W×H): 70 × 94 × 92 mm Mass: 760 g ## Single-actuation Drive. Type 4 — Glavkosmos [deployers] https://newspacemarket.com/products/single-actuation-drive-type-4/ Lead time: 6 Actuation: 100-140 Operating temperature: -50-70 °C Envelope (L×W×H): 60 × 60 × 145 mm Mass: 700 g ## Single-Actuation Drive. Type 5 — Glavkosmos [deployers] https://newspacemarket.com/products/single-actuation-drive-type-5/ Lead time: 12 Actuation: 35-40 Operating temperature: -60-60 °C Envelope (L×W×H): 85 × 93 × 80 mm Mass: 750 g ## Single-Actuation Drive. Type 6 — Glavkosmos [deployers] https://newspacemarket.com/products/single-actuation-drive-type-6/ Lead time: 12 Actuation: 130-150 Operating temperature: -60-60 °C Envelope (L×W×H): 90 × 90 × 160 mm Mass: 1290 g ## Solar Panels Hold-down Lock (mechanical) — Glavkosmos [deployers] https://newspacemarket.com/products/solar-panels-hold-down-lock-mechanical/ Design lifetime: 15 years Lead time: 4 Operating temperature: -100-100 °C Actuation: 50 Mass: 800 g ## Deployment Mechanism of Large Flat Antenna — Glavkosmos [deployers] https://newspacemarket.com/products/deployment-mechanism-of-large-flat-antenna/ Mass: 1200000 g (max) Envelope (L×W×H): ≤ ø4450 mm ## CubeSat Deployment System (TPK) — Orbital Systems [deployers] https://newspacemarket.com/products/orbital-systems-cubesat-deployment-system-tpk/ Flight heritage: Soyuz-2 + Fregat, since 2020 ## Deployment Mechanisms for Satellites (Solar Arrays, Antennas & Instruments) — Arquimea [deployers] https://newspacemarket.com/products/arquimea-deployment-mechanisms-satellites/ Operating temperature: -40 °C ## Claymore 6P PocketQube Deployer — Wyrm Engineering [deployers] https://newspacemarket.com/products/wyrm-claymore-6p-deployer/ Envelope (L×W×H): 10 mm envelope for larger mechanisms ## 1p VibePOD — Wyrm Engineering [deployers] https://newspacemarket.com/products/wyrm-1p-vibepod/ Flight heritage: FOSSA 1P for Rocketlab “Running out of fingers” mission in Q4 2019 Envelope (L×W×H): 98.00 mm x 97.00 mm x 83.00 mm ## CAVE Deployer — TRL Space [deployers] https://newspacemarket.com/products/trl-space-cave-deployer/ Capacity: 6-16 Capacity: 28 Lead time: 18 ## SlingShot — SEOPS [deployers] https://newspacemarket.com/products/seops-slingshot/ Capacity: 12 Flight heritage: First flown February 2019 on Cygnus NG-10; also flown on NG-11 (2019) and NG-16 (2021); 4 missions completed with 100% mission success ## FANTM-RAiL Deployer — Xtenti [deployers] https://newspacemarket.com/products/xtenti-fantm-rail-deployer/ Flight heritage: 100% successful in-space deployment record across multiple missions ## Deployment Mechanisms & Space Instruments — Astronika [deployers] https://newspacemarket.com/products/astronika-deployment-mechanisms/ Flight heritage: NASA InSight Mars lander (MOLE mechanism) ## OPER CubeSat Deployer — 2NDSpace Srl [deployers] https://newspacemarket.com/products/opera-12u-16u-cubesat-deployer/ Capacity: 12 ## Keystone — SEOPS [deployers] https://newspacemarket.com/products/keystone-separation-system/ Operating temperature: -150 °C ## DSOD Satellite Orbital Deployer Series — Dhruva Space [deployers] https://newspacemarket.com/products/dhruva-space-dsod-deployer-series/ Flight heritage: ISRO PSLV (PSLV-C53 1U; PSLV-C55 3U/6U) ## Redwire XPOD CubeSat Deployer — Redwire Corporation [deployers] https://newspacemarket.com/products/redwire-xpod-cubesat-deployer/ Flight heritage: ORS-3, Spaceflight SSO-A, SpaceX Rideshare, Spaceflight GTO-1, SpaceIL Lunar Lander ## Common Space Vehicle Mechanisms — Northrop Grumman Space Systems [deployers] https://newspacemarket.com/products/ngc-caspr-actuators/ Flight heritage: 40+ years, 100% mission success, over 50 missions TRL: 9 TRL: 9 @ (variant 2) ## Boom System — Frond Space Systems [deployers] https://newspacemarket.com/products/frond-boom-systems/ Operating temperature: -30 °C ## JACK — SMA Pin-Puller Actuator for Satellites and Rovers — Nimesis Technology [deployers] https://newspacemarket.com/products/nimesis-jack-sma-pin-puller-actuator/ TRL: 3 Operating temperature: -120 °C ## SATLATCH — Rotary Deployment and Latching Mechanism — Nimesis Technology [deployers] https://newspacemarket.com/products/nimesis-satlatch-rotary-deployment-mechanism/ TRL: 8 Mass: 60 g (max) Envelope (L×W×H): 40 mm wide × 8.6 mm thick Operating temperature: -120 °C Supply voltage: 7-16.8 ## HECTOR — SMA Rotary Actuator for Structural Deployment — Nimesis Technology [deployers] https://newspacemarket.com/products/nimesis-hector-sma-rotary-actuator/ TRL: 7 ## Stand-Off Mechanism (SOM) — MMA Design [deployers] https://newspacemarket.com/products/mma-stand-off-mechanism/ Flight heritage: Confirmed ## ADEO Deployable Deorbit Sails — HPS High Performance Space Structure Systems [deployers] https://newspacemarket.com/products/hps-adeo-deorbit-sails/ Flight heritage: ION-SVC-003 deployment (Dec 2022) ## Astrix Inflatable Deployment System — Astrix Astronautics [deployers] https://newspacemarket.com/products/astrix-copia-inflatable-solar-arrays/ Flight heritage: Yes ## 6U MyPOD2 — Gran Systems [deployers] https://newspacemarket.com/products/6u-mypod2/ Operating temperature: -50 °C Capacity: 100.8 Mass: 8500 g Max payload mass: 12000 g ## Deployable Space Structures — Prosix Engineering [deployers] https://newspacemarket.com/products/prosix-engineering-hybrid-cfrp-struts/ Flight heritage: Longest, stiffest, lightest, European mast deployed in 0 g conditions ## FANTM-RiDE — Xtenti [deployers] https://newspacemarket.com/products/xtenti-fantm-ride/ Flight heritage: Selected for Firefly Aerospace Elytra/Alpha responsive space demonstration supporting NRO (announced 2023) ## FANTM-RAiL — Xtenti [deployers] https://newspacemarket.com/products/xtenti-fantm-rail/ Max payload mass: 60000 g ## QuadPack Deployer — Innovative Space Logistics [deployers] https://newspacemarket.com/products/quadpack-deployer-1478/ Flight heritage: over a decade ## 1U Quad CubeSat Boom Deployer — CTD (Composite Technology Development) [deployers] https://newspacemarket.com/products/ctd-1u-quad-cubesat-boom-deployer/ Capacity: 1 ## DSOD-1U — Dhruva Space [deployers] https://newspacemarket.com/products/dsod-1u/ Mass: 3200 g Mass: 2000 g @ (variant 2) TRL: 9 ## SmallSat EPS 2.0 — NanoAvionics [eps] https://newspacemarket.com/products/nanoavionics-smallsat-eps-2/ Flight heritage: 60+ satellites launched, 300+ in production (per nanoavionics.com) ## SXC-PSS-03 Electrical Power System (with Battery Pack) — SPUTNIX [eps] https://newspacemarket.com/products/sputnix-sxc-pss-03-power-system/ Envelope (L×W×H): 96 × 89 × 14 mm ## ARC Regulation and Control Equipment for Manned and Cargo Spacecraft — Glavkosmos [eps] https://newspacemarket.com/products/arc-regulation-and-control-equipment-for-manned-and-cargo-spacecraft/ Design lifetime: 5 years Lead time: 18 Radiation tolerance (TID): 20 krad Output rails: 32 V Power consumption: 2.8 W Mass: 26000 g Power consumption: 107 W @ (variant 2) ## High Voltage Power Supply System kit KPVS — Glavkosmos [eps] https://newspacemarket.com/products/high-voltage-power-supply-system-kit-kpvs/ Design lifetime: 17 years Lead time: 18 Output rails: 120 V 28.5 V ## Nanosatellite Electrical Power System — Glavkosmos [eps] https://newspacemarket.com/products/nanosatellite-electrical-power-system/ Design lifetime: 1 years Lead time: 6 Output rails: 3.3 / 5 V ## Power Supply System [with battery unit] — Glavkosmos [eps] https://newspacemarket.com/products/power-supply-system-with-battery-unit/ Design lifetime: 1 years Lead time: 2 Envelope (L×W×H): 96 × 89 × 14 mm Mass: 58 g Supply voltage: 8 Power consumption: 0.16 W ## Regulation and Monitoring Equipment of Electric Power Supply System EPS) ARK-MKA — Glavkosmos [eps] https://newspacemarket.com/products/regulation-and-monitoring-equipment-of-electric-power-supply-system-eps-ark-mka/ Design lifetime: 9 years Lead time: 18 Radiation tolerance (TID): 100 krad Output rails: 32 V Power consumption: 700 W Mass: 12000 g Power consumption: 58 W @ (variant 2) ## Voltage Converter PN120/28 — Glavkosmos [eps] https://newspacemarket.com/products/voltage-converter-pn120-28/ Design lifetime: 15 years Lead time: 12 Radiation tolerance (TID): 4.5 krad Supply voltage: 110-180 Output rails: 28.5 V Power consumption: 1.5 W Conversion efficiency: 92 Mass: 15500 g Envelope (L×W×H): 340×250×290 mm ## Voltage Converter PN28/120 — Glavkosmos [eps] https://newspacemarket.com/products/voltage-converter-pn28-120/ Design lifetime: 15 years Lead time: 12 Radiation tolerance (TID): 4.5 krad Supply voltage: 28.5 Output rails: 120 V Power consumption: 2 W Conversion efficiency: 92 Mass: 25000 g Envelope (L×W×H): 340×252×310 mm ## Voltage Converter Single-phase, Upgraded POS-80-RNM — Glavkosmos [eps] https://newspacemarket.com/products/voltage-converter-single-phase-upgraded-pos-80-rnm/ Design lifetime: 10 years Lead time: 6 Radiation tolerance (TID): 4.5 krad Output rails: 24-34 V Output rails: 42 V @ (variant 2) Power consumption: 80 W Conversion efficiency: 85 Mass: 2500 g ## Unified DC-DC Conversion Module — Glavkosmos [eps] https://newspacemarket.com/products/unified-dc-dc-conversion-module/ Design lifetime: 3 years Lead time: 8 Mass: 30 g Output rails: 12 5 3.3 1.8 1.2 V Conversion efficiency: 85 Supply voltage: 5 ## Unified Power Management and Control Module — Glavkosmos [eps] https://newspacemarket.com/products/unified-power-management-and-control-module/ Design lifetime: 3 years Lead time: 8 Mass: 30 g ## DC/DC Converter — Glavkosmos [eps] https://newspacemarket.com/products/dc-dc-converter/ Supply voltage: 2.8-5.5 Output rails: 1.2–3.3 V Conversion efficiency: 60-75 Lead time: 12 ## SmallSat PCDU – STARBUCK-MINI — AAC Clyde Space [eps] https://newspacemarket.com/products/aac-smallsat-pcdu-starbuck-mini/ Design lifetime: 5-7 years Power consumption: 2.5 W Supply voltage: 22-34 Power consumption: 10 W @ (variant 2) Operating temperature: -30 °C Mass: 3900 g Mass: 11800 g @ (variant 2) TRL: 9 Lead time: 6 Lead time: 10 @ (variant 2) ## SmallSat PCDU – STARBUCK-Mini MCC — AAC Clyde Space [eps] https://newspacemarket.com/products/aac-smallsat-pcdu-starbuck-mini-mcc/ Design lifetime: 5-7 years Power consumption: 2.5 W Supply voltage: 22-34 Power consumption: 10 W @ (variant 2) Operating temperature: -30 °C Mass: 3900 g Mass: 11800 g @ (variant 2) TRL: 9 Lead time: 6 Lead time: 10 @ (variant 2) ## VPCDU-1 Power Control and Distribution Unit — VECTRONIC Aerospace GmbH [eps] https://newspacemarket.com/products/vectronic-vpcdu-1/ Envelope (L×W×H): 220 mm x 160 mm x 117.4 mm Mass: 4140 g Power consumption: 2.5 W Supply voltage: 22.5 Supply voltage: 22.5 @ (variant 2) Power consumption: 360 W @ (variant 2) Power consumption: 540 W @ (variant 3) Connector: SUB D & SUB HD Radiation tolerance (TID): 20 krad (min) ## NANOeps — SkyLabs d.o.o. [eps] https://newspacemarket.com/products/skylabs-nanoeps/ TRL: 9 ## Regulation and control equipment — SPUTNIX [eps] https://newspacemarket.com/products/regulation-and-control-equipment/ Envelope (L×W×H): 306 x 161 x 140 (without fasteners) mm Mass: 7000 g ## High-power distribution and control unit — SPUTNIX [eps] https://newspacemarket.com/products/high-power-distribution-and-control-unit/ Envelope (L×W×H): 244 x 171 x 45 (without fasteners) mm Mass: 1100 g ## Power supply system (with battery unit) — SPUTNIX [eps] https://newspacemarket.com/products/power-supply-system-with-battery-unit-2/ Envelope (L×W×H): 98.4 x 96 x 19 mm (±0.2 mm) Supply voltage: 4.5-5.5 Power consumption: 0.2 W (max) Envelope (L×W×H): 95 x 97 x 34 mm (±0.2 mm, ±1 mm for Z) @ (variant 2) Mass: 360 g Protections: 5.0 A (typ.) Protections: 5.0 V, 8.5 V @ (variant 2) ## High-power Multi-channel Electrical Power System Module (EPSM1) — Pumpkin, Inc. [eps] https://newspacemarket.com/products/pumpkin-epsm1-power-system-module/ Output power (total): 480 W Supply voltage: 28 Supply voltage: 28 @ (variant 2) ## SOLO Cubesat EPS — 2NDSpace Srl [eps] https://newspacemarket.com/products/solo-cubesat-eps/ Flight heritage: Yes ## Modular Power Platform (MPP) — Space Inventor ApS [eps] https://newspacemarket.com/products/modular-power-platform-mpp/ Power consumption: 110 W Power consumption: 408 W @ (variant 2) Power consumption: 220 W @ (variant 3) Power consumption: 408 W @ (variant 4) Power consumption: 440 W @ (variant 5) Power consumption: 720 W @ (variant 6) Power consumption: 1100 W @ (variant 7) Power consumption: 2040 W @ (variant 8) Power consumption: 2200 W @ (variant 9) Power consumption: 4080 W @ (variant 10) ## Crystalspace P1U “Vasik” — Crystal Space [eps] https://newspacemarket.com/products/crystalspace-p1u-vasik/ Lead time: 6-8 ## GEMINI EPS — NPC Spacemind [eps] https://newspacemarket.com/products/npc-spacemind-gemini-cubesat-eps/ Protections: Full protection (OV, OC, OP); Configurable interfaces Mass: 300 g ## CubeSat Electrical Power System 1.0 (EPS) — NanoAvionics [eps] https://newspacemarket.com/products/nanoavionics-eps-1/ Output power (total): 175 W Protections: Yes Protections: Yes @ (variant 2) Protections: Yes @ (variant 3) ## NART-EPS Electric Power Subsystem (EPS) — Gumush [eps] https://newspacemarket.com/products/gumush-n-art-eps/ Supply voltage: 20 Mass: 103 g Envelope (L×W×H): 86 x 93 x 21 mm ## E14-150 14V SmallSat Electric Power System — ibeos [eps] https://newspacemarket.com/products/ibeos-e14-150-eps/ Conversion efficiency: 96 Supply voltage: 16.8 Output rails: 10x (10 mOhm typical) Power consumption: 1.8 W Envelope (L×W×H): 96 x 90 x 14.5 mm Mass: 140 g Operating temperature: -40-105 °C Radiation tolerance (TID): 30 krad TRL: 9 ## E28-200 28V SmallSat Electric Power System — ibeos [eps] https://newspacemarket.com/products/ibeos-e28-200-eps/ Conversion efficiency: 96 Supply voltage: 33.6 Output rails: 10x (10 mOhm typical) Power consumption: 2.5 W Envelope (L×W×H): 96 x 90 x 14.5 mm Mass: 140 g Operating temperature: -40-105 °C Radiation tolerance (TID): 30 krad TRL: 9 ## PureLine Topaz/THORs Power Processing Unit — Airbus Defence and Space [eps] https://newspacemarket.com/products/airbus-elektro-ppu/ Design lifetime: 10 years Random vibration: 20 Power consumption: 300 W Supply voltage: 27-38 Design lifetime: 10 years @ LEO ## Power Conditioning and Distribution Units (PCDU) — Airbus Defence and Space [eps] https://newspacemarket.com/products/airbus-evo-pcdu/ Flight heritage: Onboard Alphabus, E3000, E3000-NEO and Galileo, selected by major operators and other spacecraft manufacturers Flight heritage: More than 80 units in flight on several platforms in the world @ (variant 2) ## PDUFA1000 Power Conditioning and Distribution Unit — ZIN Technologies [eps] https://newspacemarket.com/products/zin-technologies-pdufa1000/ Flight heritage: ISS, Space Shuttle, NASA Artemis (Lunar Gateway) ## PPS Power Distribution Units — Kayser Space [eps] https://newspacemarket.com/products/kayser-pps-power-distribution/ Output rails: 28 Vdc (PPS mk1/mk2, VMU PCU) Flight heritage: ISS Columbus Module, multiple ESA programs ## Space-Grade DC-DC Converters — EUROSATCOM [eps] https://newspacemarket.com/products/eurosatcom-space-dc-dc-converters/ Power consumption: 2.5 W ## PPS mk1 — Kayser Space [eps] https://newspacemarket.com/products/kayser-power-unit/ Supply voltage: 28 Flight heritage: ISS Columbus Module and multiple ESA programs ## CubeSat Power Systems (EPS and Batteries) — AAC Clyde Space [eps] https://newspacemarket.com/products/clyde-space-eps/ Flight heritage: Hundreds of CubeSat missions (NASA, ESA, Planet, Spire, JAXA, others) ## PCDU — Power Conditioning and Distribution Unit — Terma [eps] https://newspacemarket.com/products/terma-pcdu/ Conversion efficiency: 95 (min) Flight heritage: Rosetta, Mars Express, Venus Express, Galileo, BepiColombo, Euclid, Plato, OneWeb, Small GEO ## Integrated EPS/OBC Bus Module — Aphelion Orbitals [eps] https://newspacemarket.com/products/integrated-eps-obc-bus-module-3474/ Output rails: 7 independently controlled and monitored ## NEA® 8020 Series Battery Cell Bypass Switch — Ensign-Bickford Aerospace & Defense (EBAD) [eps] https://newspacemarket.com/products/nea-8020-series-battery-cell-bypass-switch/ Operating temperature: -55 °C Mass: 130 g ## NEA® 8030 Series Battery Cell Bypass Switch — Ensign-Bickford Aerospace & Defense (EBAD) [eps] https://newspacemarket.com/products/nea-8030-series-battery-cell-bypass-switch/ Operating temperature: -55 °C Mass: 130 g ## NEA® 8040 Series Battery Cell Bypass Switch — Ensign-Bickford Aerospace & Defense (EBAD) [eps] https://newspacemarket.com/products/nea-8040-series-battery-cell-bypass-switch/ Operating temperature: -55 °C ## Power VPX — CAVU Aerospace [eps] https://newspacemarket.com/products/power-vpx/ Envelope (L×W×H): 3.94 in W × 6.63 in L × 2.00 in H Survival temperature: -55 °C ## Ibeos Modular Power System (MPS) — ibeos [eps] https://newspacemarket.com/products/ibeos-modular-power-system-mps/ Power consumption: 500-2000 W TRL: 9 ## AX Electrical Power System (EPS) — HEX20 [eps] https://newspacemarket.com/products/ax-electrical-power-system-eps/ Supply voltage: 16.8 Supply voltage: 18 (min) Output rails: 16.8 V ## N-SPHERE – High-End GNSS Receiver — Syrlinks [gnss-receivers] https://newspacemarket.com/products/syrlinks-n-sphere-gnss-receiver/ Constellations: GPS, GALILEO, BeiDou & GLONASS Design lifetime: 2 years @ LEO missions Design lifetime: 5 years @ LEO missions (variant 2) Flight heritage: Yes ## GNSS Receiver in a Secure Enclosure — Glavkosmos [gnss-receivers] https://newspacemarket.com/products/gnss-receiver-in-a-secure-enclosure/ Design lifetime: 3 years Lead time: 6 Envelope (L×W×H): 71×51×12 mm Mass: 50 g Operating temperature: -40-85 °C Channels: 16 Constellations: 9 m Constellations: 14 m @ (variant 2) Position accuracy: 25 m Position accuracy: 0.1 m @ (variant 2) Position accuracy: 0.1 m @ (variant 3) Position accuracy: 10 m @ (variant 4) Position accuracy: 1 m @ (variant 5) Position accuracy: 0.03 m @ (variant 6) Time to first fix (cold): 10 s Time to first fix (cold): 120 s @ (variant 2) Time to first fix (cold): 30 s @ (variant 3) Power consumption: 0.65 W TRL: 9 ## GNSS Receiver — Glavkosmos [gnss-receivers] https://newspacemarket.com/products/gnss-receiver/ Design lifetime: 3 years Lead time: 7 Mass: 3 g Supply voltage: 1.8 Operating temperature: -40-85 °C Channels: 44 Constellations: 2.5 m Constellations: 4 m @ (variant 2) Constellations: 0.03 m @ (variant 3) Position accuracy: 1.5 m Time to first fix (cold): 27 s Power consumption: 0.13 W Power consumption: 0.07 W @ (variant 2) Power consumption: 0.015 W @ (variant 3) Time to first fix (cold): -155 s @ (variant 2) ## High Precision GNSS Module — Glavkosmos [gnss-receivers] https://newspacemarket.com/products/high-precison-gnss-module/ Design lifetime: 3 years Lead time: 8 Envelope (L×W×H): 120×90×40 mm Mass: 120 g Supply voltage: 9-36 Operating temperature: -40-85 °C Power consumption: 20 W (max) Position accuracy: 0.01 m (max) Position accuracy: 0.2 m (max) @ (variant 2) TRL: 9 ## On-board GNSS Receiver with Interface Outputs — Glavkosmos [gnss-receivers] https://newspacemarket.com/products/on-board-gnss-receiver-with-interface-outputs/ Design lifetime: 3 years Lead time: 7 Envelope (L×W×H): 71×51×12 mm Mass: 10 g Operating temperature: -40-85 °C Channels: 44 Constellations: 2.5 m Position accuracy: 4 m Position accuracy: 0.03 m @ (variant 2) Position accuracy: 1.5 m @ (variant 3) Time to first fix (cold): 2 s Time to first fix (cold): 27 s @ (variant 2) Power consumption: 0.07 W Power consumption: 0.13 W @ (variant 2) Power consumption: 0.015 W @ (variant 3) Time to first fix (cold): -155 s @ (variant 3) TRL: 9 ## PORTABLE RECEIVER-INDICATOR GN — Glavkosmos [gnss-receivers] https://newspacemarket.com/products/portable-receiver-indicator-gn/ Lead time: 8 Mass: 2700 g Power consumption: 4 W Channels: 1.6 ## Small-sized navigation equipment GM — Glavkosmos [gnss-receivers] https://newspacemarket.com/products/small-sized-navigation-equipment-gm/ Mass: 320 g Power consumption: 1 W Channels: 1.6 Lead time: 8 ## Transportable Receiver-Indicator GV — Glavkosmos [gnss-receivers] https://newspacemarket.com/products/transportable-receiver-idicator-gv/ Lead time: 8 Channels: 64 Mass: 1800 g ## VLSI kit for low-power GLONASS / GPS navigation receiver — Glavkosmos [gnss-receivers] https://newspacemarket.com/products/vlsi-kit-for-low-power-glonass-gps-navigation-receiver/ Envelope (L×W×H): 6×6×1 mm Mass: 1 g Operating temperature: -40 °C Channels: 36 Power consumption: 0.07 W Design lifetime: 3 years Lead time: 10 ## VLSI SIC for GNSS receiver — Glavkosmos [gnss-receivers] https://newspacemarket.com/products/vlsi-sic-for-gnss-receiver/ Design lifetime: 3 years Lead time: 6 Mass: 1 g ## GNSS-701 Satellite GNSS Receiver — AAC SpaceQuest (AAC Clyde Space subsidiary) [gnss-receivers] https://newspacemarket.com/products/aac-spacequest-gnss-701/ Flight heritage: Bestselling component, flight proven ## WARPSPACE GPS Module — WARPSPACE Inc. [gnss-receivers] https://newspacemarket.com/products/warpspace-gps-module/ Envelope (L×W×H): 24.0 x 20.0 x 5.3 mm Mass: 3 g ## CHCNAV i93 — CHC Navigation / Huace Daohang [gnss-receivers] https://newspacemarket.com/products/chc-navigation-i93/ Constellations: GPS, GLONASS, Galileo, BeiDou, QZSS, SBAS, NavIC/IRNSS Channels: 1892 Position accuracy: 0.008 m Position accuracy: 0.015 m @ (variant 2) Operating temperature: -40 °C Mass: 1150 g ## Satellite navigation equipment — SPUTNIX [gnss-receivers] https://newspacemarket.com/products/satellite-navigation-equipment/ Envelope (L×W×H): 171 x 111 x 51 (without fasteners) mm Mass: 700 g ## Q40 MicroPNT GNSS Receiver — QinetiQ Space [gnss-receivers] https://newspacemarket.com/products/qinetiq-q40-micropnt/ Position accuracy: 5 m (max) Constellations: Multi-constellation (GPS, Galileo) ## GNSS systems — Indra Sistemas [gnss-receivers] https://newspacemarket.com/products/galileo-gnss-navishield-indra/ Constellations: 100+ ## JAVAD GNSS — JAVAD GNSS [gnss-receivers] https://newspacemarket.com/products/javad-triumph-3-receiver/ Channels: 874 ## TR-2S LEO — JAVAD GNSS [gnss-receivers] https://newspacemarket.com/products/javad-delta-series-receiver/ Channels: 874 ## AST-500 Multi-GNSS Baseband SoC — Accord [gnss-receivers] https://newspacemarket.com/products/accord-ast500-gnss-soc/ Constellations: GPS, GLONASS, NavIC, BeiDou, Galileo, QZSS, GAGAN Operating temperature: -40 °C Supply voltage: 2.7 ## NAVLAN-IG3 Multi-Constellation GNSS Receiver — Accord [gnss-receivers] https://newspacemarket.com/products/accord-navlan-ig3-gnss-receiver/ Constellations: IRNSS L5, GPS L1, GLONASS L1, GAGAN L1 ## GT1005 Space-Time Capsule Positioning Terminal Assembly — Geespace [gnss-receivers] https://newspacemarket.com/products/geesatcom-e-link-gt1005/ Envelope (L×W×H): Φ80 mm × 23 mm (D×H) ## N-SPHERE Space GNSS Receiver — Safran Electronics Defense Space [gnss-receivers] https://newspacemarket.com/products/safran-nsphere-gnss-receiver/ Constellations: GPS, GALILEO, BeiDou, GLONASS Radiation tolerance (TID): 15 krad Flight heritage: LeoStella LS-300 selected 2024 ## Trimble R12i GNSS System — Trimble [gnss-receivers] https://newspacemarket.com/products/trimble-r12i-gnss/ Position accuracy: 0.02 m Channels: 672 Constellations: GPS, GLONASS, Galileo, BeiDou, NavIC, QZSS, SBAS Mass: 1120 g Envelope (L×W×H): 11.9 cm × 13.6 cm ## Trimble R980 GNSS System — Trimble [gnss-receivers] https://newspacemarket.com/products/trimble-r980-gnss/ Position accuracy: 0.02 m Channels: 672 Constellations: GPS, GLONASS, Galileo, BeiDou, NavIC, QZSS, SBAS Mass: 1130 g Envelope (L×W×H): 11.9 cm × 13.6 cm ## BeiDou GNSS Receivers and Navigation Modules — BDStar Navigation (Beidou Xingtong) [gnss-receivers] https://newspacemarket.com/products/bdstar-beidou-receivers/ Constellations: BeiDou-3 (primary), GPS, GLONASS, Galileo (multi-constellation) ## High-Precision GNSS Survey Receivers — CHC Navigation / Huace Daohang [gnss-receivers] https://newspacemarket.com/products/chc-navigation-gnss-receivers/ Export status: 140 ## OrbFIX — High-Accuracy GNSS Receiver for Space — RoInSpace (RISE, Romanian InSpace Engineering) [gnss-receivers] https://newspacemarket.com/products/roinspace-orbfix-gnss-receiver/ Constellations: GPS, GLONASS, Galileo, BeiDou ## AmbaSat-1 Sensor 08 — AmbaSat [gnss-receivers] https://newspacemarket.com/products/ambasat-1-sensor-08-3465/ Envelope (L×W×H): 9.7x10.1 mm ## GNSS Patch Antenna L1/E1 — EnduroSat [gnss-receivers] https://newspacemarket.com/products/gnss-patch-antenna-l1-e1/ Mass: 17 g ## GNSS Patch Antenna L1+L2+L5 — EnduroSat [gnss-receivers] https://newspacemarket.com/products/gnss-patch-antenna-l1l2l5/ Mass: 38.5 g Connector: SMP ## piNAV-NG/FM (Flight Model) — SkyFox Labs s.r.o. [gnss-receivers] https://newspacemarket.com/products/pinav-ng-fm-flight-model/ Constellations: L1 C/A, 15 channels TRL: 9 ## SGRS-12P Ground Station — Satrev (SatRevolution) [ground-stations] https://newspacemarket.com/products/satrev-sgrs-12p-ground-station/ Frequency band: UHF @ uplink Frequency band: S @ downlink Frequency: 2000-2300 MHz Antenna diameter: 3 m Operating temperature: -20-55 °C Envelope (L×W×H): 3 m (diameter) Mass: 60000 g Connector: N Female ## Zavitok Satellite Ground Station (M / S-L) — SPUTNIX [ground-stations] https://newspacemarket.com/products/sputnix-zavitok-ground-station/ Power consumption: 10 W ## Antenna Feeder Device 3 — Glavkosmos [ground-stations] https://newspacemarket.com/products/antenna-feeder-device-3/ Design lifetime: 15 years Lead time: 9 Antenna diameter: 3.7 m ## Antenna Feeder Device 4 — Glavkosmos [ground-stations] https://newspacemarket.com/products/antenna-feeder-device-4/ Design lifetime: 15 years Lead time: 9 Antenna diameter: 4.5 m ## Antenna Feeder Device AC-25KRL-Ku/S — Glavkosmos [ground-stations] https://newspacemarket.com/products/antenna-feeder-device-ac-25krl-ku-s/ Design lifetime: 15 years Lead time: 9 Antenna diameter: 2.4 m ## Antenna feeder device — Glavkosmos [ground-stations] https://newspacemarket.com/products/antenna-feeder-device/ Design lifetime: 15 years Lead time: 9 Antenna diameter: 2.4 m ## Antenna-feeder System 9.3 m — Glavkosmos [ground-stations] https://newspacemarket.com/products/antenna-feeder-system-9-3-m/ Design lifetime: 15 years Lead time: 12 Antenna diameter: 9.3 m ## Antenna Post L- and S-bands — Glavkosmos [ground-stations] https://newspacemarket.com/products/antenna-post-l-and-s-bands/ Design lifetime: 10 years Lead time: 12 Antenna diameter: 6 m ## Antenna System 4,1 meters Ka — Glavkosmos [ground-stations] https://newspacemarket.com/products/antenna-system-41-meters-ka/ Design lifetime: 15 years Lead time: 9 Antenna diameter: 4.1 m ## Antenna System 7.2 m C/Ku — Glavkosmos [ground-stations] https://newspacemarket.com/products/antenna-system-7-2-m-c-ku/ Design lifetime: 10 years Lead time: 12 Antenna diameter: 7.2 m ## Antenna System 7.2 m C/Ku/Ka — Glavkosmos [ground-stations] https://newspacemarket.com/products/antenna-system-7-2-m-c-ku-ka/ Antenna diameter: 7.2 m Design lifetime: 10 years Lead time: 12 ## Antenna System 7.2 m L/S/X — Glavkosmos [ground-stations] https://newspacemarket.com/products/antenna-system-7-2-m-l-s-x/ Design lifetime: 10 years Lead time: 12 Antenna diameter: 7.2 m ## Antenna System 7.2 m — Glavkosmos [ground-stations] https://newspacemarket.com/products/antenna-system-7-2-m/ Design lifetime: 15 years Lead time: 12 Antenna diameter: 7.2 m ## Antenna System 9.3 M AC93R-C/Ku — Glavkosmos [ground-stations] https://newspacemarket.com/products/antenna-system-9-3-m-ac93r-c-ku/ Design lifetime: 15 years Lead time: 12 Antenna diameter: 9.3 m ## Ground Antenna System 11 / 4-2.5 — Glavkosmos [ground-stations] https://newspacemarket.com/products/ground-antenna-system-11-4-2-5/ Design lifetime: 15 years Lead time: 9 Antenna diameter: 2.5 m ## Ground Antenna System 2 — Glavkosmos [ground-stations] https://newspacemarket.com/products/ground-antenna-system-2/ Design lifetime: 15 years Lead time: 9 Antenna diameter: 2.5 m ## Ground Antenna System L/S/C/X/Ku/Ka -bands AFS-12 — Glavkosmos [ground-stations] https://newspacemarket.com/products/ground-antenna-system-l-s-c-x-ku-ka-bands-afs-12/ Design lifetime: 15 years Lead time: 18 Antenna diameter: 12 m ## Ground Antenna System NAS 11-14-2.4 — Glavkosmos [ground-stations] https://newspacemarket.com/products/ground-antenna-system-nas-11-14-2-4/ Design lifetime: 15 years Lead time: 9 Antenna diameter: 2.4 m ## Ground Antenna System TAS 4 / 6-6.0 m — Glavkosmos [ground-stations] https://newspacemarket.com/products/ground-antenna-system-tas-4-6-6-0-m/ Design lifetime: 15 years Lead time: 12 Antenna diameter: 6 m ## Ground Antenna System TAS 4/6-11/14-6.0 m — Glavkosmos [ground-stations] https://newspacemarket.com/products/ground-antenna-system-tas-4-6-11-14-6-0-m/ Design lifetime: 15 years Lead time: 12 Antenna diameter: 6 m ## Ground Antenna System US 11 / 14-3.7 — Glavkosmos [ground-stations] https://newspacemarket.com/products/ground-antenna-system-us-11-14-3-7/ Design lifetime: 15 years Lead time: 9 Antenna diameter: 2.5 m ## Mobile Ground Satellite Communication Station ZSSS-L — Glavkosmos [ground-stations] https://newspacemarket.com/products/mobile-ground-satellite-communication-station-zsss-l/ Design lifetime: 10 years Lead time: 12 Antenna diameter: 2.4 m ## S-band Part-turn Antenna System — Glavkosmos [ground-stations] https://newspacemarket.com/products/s-band-part-turn-antenna-system/ Design lifetime: 10 years Lead time: 9 Antenna diameter: 2.5 m ## Transportable Ground Station — Glavkosmos [ground-stations] https://newspacemarket.com/products/transportable-ground-station/ Design lifetime: 10 years Lead time: 18 Antenna diameter: 7 m EIRP: 65 dBW (min) ## Data Receiving and Satellites Controlling Station — Glavkosmos [ground-stations] https://newspacemarket.com/products/data-receiving-and-satellites-controlling-station/ Design lifetime: 1 years Lead time: 3 Power consumption: 4 W ## Ground Station — Glavkosmos [ground-stations] https://newspacemarket.com/products/ground-station/ Design lifetime: 1 years Lead time: 6 Power consumption: 20 W ## Satellite Data Receiving Training Station — Glavkosmos [ground-stations] https://newspacemarket.com/products/satellite-data-receiving-training-station/ Design lifetime: 1 years Lead time: 1 ## Optical Ground Stations — General Atomics Synopta GmbH [ground-stations] https://newspacemarket.com/products/synopta-optical-ground-stations/ Envelope (L×W×H): > Ø 0.5 m Envelope (L×W×H): Ø 0.25 m to Ø 1 m @ (variant 2) ## BusCORE Groundstation — SkyFox Labs s.r.o. [ground-stations] https://newspacemarket.com/products/skyfox-labs-buscore-groundstation/ Connector: 1x N-Female UHF antenna port, 1x N-Female UHF monitor port, Amphenol 60V/26A power connector Operating temperature: 0-70 °C ## RBC Signals Fractional & Dynamic Spectrum Leasing and Ground Stations as a Service (GSaaS) — RBC Signals [ground-stations] https://newspacemarket.com/products/rbc-signals-storm/ Envelope (L×W×H): Over 80 antennas ## Satellite Ground Systems — Kongsberg Defence & Aerospace — Space Division [ground-stations] https://newspacemarket.com/products/kongsberg-satellite-ground-systems/ Flight heritage: NorSat-1/2/3, AISSat-1/2, Copernicus ground segment ## Enterprise NGSO Terminal — ALCAN Systems [ground-stations] https://newspacemarket.com/products/alcan-enterprise-ngso-terminal/ Envelope (L×W×H): 55 cm x 99 cm x 9 cm Mass: 20000 g (max) ## BUC/SSPA Amplifiers (C/X/Ku/Ka Band) — EUROSATCOM [ground-stations] https://newspacemarket.com/products/eurosatcom-buc-sspa-amplifiers/ Power consumption: 400 W Power consumption: 20 W @ (variant 2) Power consumption: 4 W @ (variant 3) Power consumption: 5 W @ (variant 4) ## BridgeComm Optical Ground Terminal / Optical Ground Station (OGT/OGS) — BridgeComm, Inc. [ground-stations] https://newspacemarket.com/products/bridgecomm-optical-ground-stations/ Flight heritage: Initial Spacecraft DTE terminal launched in 2017 to ISS Flight heritage: Additional Terminals and Modems awarded by AFRL in 2019 @ (variant 2) Flight heritage: IC program space DTE terminal delivered in 2021 @ (variant 3) ## Thai National Radio Telescope — NARIT (National Astronomical Research Institute of Thailand) [ground-stations] https://newspacemarket.com/products/13m-vgos-radio-station/ Antenna diameter: 40 m ## Kestrel u5 — Kymeta [ground-stations] https://newspacemarket.com/products/kymeta-flat-panel-antenna/ Power consumption: 100 W ## ATCi Parabolic Antenna 3.7m C/Ku-Band Prime Focus Rx — ATCi [ground-stations] https://newspacemarket.com/products/atci-parabolic-37m-cku-rx/ Antenna diameter: 3.7 m ## ATCi Parabolic Antenna 4.5m C/Ku-Band Prime Focus Rx — ATCi [ground-stations] https://newspacemarket.com/products/atci-parabolic-45m-cku-rx/ Antenna diameter: 4.5 m ## 9.2m Satcom Antenna — Calian (SatService) [ground-stations] https://newspacemarket.com/products/calian-9-2m-satcom-antenna/ Antenna diameter: 9.2 m Operating temperature: -30-60 °C Survival temperature: -40-70 °C ## 9.2m LEO Earth Station Antenna — Calian (SatService) [ground-stations] https://newspacemarket.com/products/calian-9-2m-leo-earth-station-antenna/ Antenna diameter: 9.2 m Operating temperature: -30-60 °C Survival temperature: -40-70 °C ## 7m Satcom Antenna — Calian (SatService) [ground-stations] https://newspacemarket.com/products/calian-7m-satcom-antenna/ Antenna diameter: 7 m Operating temperature: -30-60 °C Survival temperature: -40-70 °C ## 7m LEO Earth Station Antenna — Calian (SatService) [ground-stations] https://newspacemarket.com/products/calian-7m-leo-earth-station-antenna/ Antenna diameter: 7 m Operating temperature: -30-60 °C Survival temperature: -40-70 °C ## 4m Satcom Antenna — Calian (SatService) [ground-stations] https://newspacemarket.com/products/calian-4m-satcom-antenna/ Antenna diameter: 4 m Operating temperature: -30-60 °C Survival temperature: -40-70 °C ## Ka/Q/V-Band Gateway Antenna — Calian (SatService) [ground-stations] https://newspacemarket.com/products/calian-ka-qv-band-gateway-antenna/ Antenna diameter: 10 m ## Integrated TT&C and Data Transmission Ground System — Emposat Co., Ltd. [ground-stations] https://newspacemarket.com/products/emposat-12m-x-band-tt-c-ground-station/ Antenna diameter: 12 m Antenna diameter: 4.5 m @ (variant 2) Antenna diameter: 8 m @ (variant 3) ## SCOUT — Arctic Space Technologies [ground-stations] https://newspacemarket.com/products/scout-3484/ Antenna diameter: 2.4 m Operating temperature: -40 °C ## GaN DBS SSPA/BUC 200W/300W/550W Indoor — TTI Norte [ground-stations] https://newspacemarket.com/products/gan-dbs-sspa-buc-200w-300w-550w-indoor/ Supply voltage: 90-264 Power consumption: 1700 W (max) Power consumption: 2700 W Envelope (L×W×H): 483 x 266 x 560 mm Mass: 48000 g ## GaN DBS SSPA/BUC 200W Outdoor — TTI Norte [ground-stations] https://newspacemarket.com/products/gan-dbs-sspa-buc-200w-outdoor/ Power consumption: 200 W Power consumption: 200 W @ (variant 2) Envelope (L×W×H): 400 x 274 x 220 mm ## GaN DBS SSPA/BUC 300W Outdoor — TTI Norte [ground-stations] https://newspacemarket.com/products/gan-dbs-sspa-buc-300w-outdoor/ Power consumption: 300 W Power consumption: 300 W @ (variant 2) Envelope (L×W×H): 550 x 450 x 278 mm ## GaN DBS SSPA/BUC 550W Outdoor — TTI Norte [ground-stations] https://newspacemarket.com/products/gan-dbs-sspa-buc-550w-outdoor/ Power consumption: 550 W Power consumption: 550 W @ (variant 2) Envelope (L×W×H): 550 x 450 x 278 mm ## GaN Ku SSPA/BUC 325W Outdoor — TTI Norte [ground-stations] https://newspacemarket.com/products/gan-ku-sspa-buc-325w-outdoor/ Power consumption: 325 W Power consumption: 325 W @ (variant 2) Supply voltage: 90-264 Power consumption: 1400 W @ (variant 3) Envelope (L×W×H): 550 x 360 x 289 mm Mass: 68500 g ## GaN Ku SSPA/BUC 600W Outdoor — TTI Norte [ground-stations] https://newspacemarket.com/products/gan-ku-sspa-buc-600w-outdoor/ Power consumption: 600 W Power consumption: 600 W @ (variant 2) Supply voltage: 90-264 Power consumption: 2600 W @ (variant 3) Envelope (L×W×H): 550 x 360 x 289 mm Mass: 68500 g ## GaN Ku SSPA/BUC 150W/325W/600W STANDALONE – Indoor — TTI Norte [ground-stations] https://newspacemarket.com/products/gan-ku-sspa-buc-150w-325w-600w-standalone-indoor/ Supply voltage: 90-264 Envelope (L×W×H): 483 x 266 x 601 mm (including handles) - RF unit 6RU panel height Mass: 45000 g ## GaN C SSPA/BUC 800W Indoor — TTI Norte [ground-stations] https://newspacemarket.com/products/gan-c-sspa-buc-800w-indoor/ Supply voltage: 90-264 Power consumption: 3000 W (max) Envelope (L×W×H): 483 x 266 x 518 mm - RF unit 6RU panel height Mass: 35000 g ## GaN Ku SSPA/BUC 150W/325W/600W 2:1 REDUNDANCY SYSTEM – Indoor — TTI Norte [ground-stations] https://newspacemarket.com/products/gan-ku-sspa-buc-150w-325w-600w-21-redundancy-system-indoor/ Power consumption: 150 W Envelope (L×W×H): 19” Envelope (L×W×H): 19” Rack 42 U (H) x 1 m (D) @ (variant 2) ## GaN Ku SSPA/BUC 150W/325W/600W 1:1 REDUNDANCY SYSTEM – Indoor — TTI Norte [ground-stations] https://newspacemarket.com/products/gan-ku-sspa-buc-150w-325w-600w-11-redundancy-system-indoor/ Power consumption: 150 W Envelope (L×W×H): 19” Envelope (L×W×H): 19” Rack 42 U (H) x 1 m (D) @ (variant 2) ## Kratos 4.6 Meter Trifold™ Transportable Satellite Antenna — Kratos Defense & Security Solutions [ground-stations] https://newspacemarket.com/products/kratos-4-6-meter-trifold-transportable-satellite-antenna/ Envelope (L×W×H): stainless steel, passivated per MIL-F-14072-E300 Envelope (L×W×H): hot-dipped galvanized stainless steel, passivated per ASTM-A123 @ (variant 2) ## Kratos 3.9 Meter Trifold™ Transportable Satellite Antenna System — Kratos Defense & Security Solutions [ground-stations] https://newspacemarket.com/products/kratos-3-9-meter-trifold-transportable-satellite-antenna-system/ Envelope (L×W×H): stainless steel, passivated per MIL-F-14072-E300 Envelope (L×W×H): hot-dipped galvanized stainless steel, passivated per ASTM-A123 @ (variant 2) ## Kratos 2.4m Nomadic Antenna — Kratos Defense & Security Solutions [ground-stations] https://newspacemarket.com/products/kratos-2-4m-nomadic-antenna/ Antenna diameter: 2.4 m Operating temperature: -40 °C Operating temperature: -58 °C @ (variant 2) Envelope (L×W×H): 38” x 14” x 12” (96 cm x 36 cm x 30 cm) Supply voltage: 24 ## Kratos 2.5m Nomadic Antenna — Kratos Defense & Security Solutions [ground-stations] https://newspacemarket.com/products/kratos-2-5m-nomadic-antenna/ Antenna diameter: 2.5 m Operating temperature: -40 °C Operating temperature: -58 °C @ (variant 2) Envelope (L×W×H): 38” x 14” x 12” (96 cm x 36 cm x 30 cm) Supply voltage: 24 ## Kratos KPBESA40M.C2 4.0 Meter Earth Station Antenna — Kratos Defense & Security Solutions [ground-stations] https://newspacemarket.com/products/kratos-kpbesa40m-c2-4-0-meter-earth-station-antenna/ Antenna diameter: 1.22 m Envelope (L×W×H): 0.61 m (24 in) Envelope (L×W×H): stainless steel, passivated per MIL-F-14072-E300 @ (variant 2) Envelope (L×W×H): hot-dipped galvanized stainless steel, passivated per ASTM-A123 @ (variant 3) ## Kratos MILSAT KPBESA40MLQD.C2 4.0 Meter Light Quick Deploy Antenna — Kratos Defense & Security Solutions [ground-stations] https://newspacemarket.com/products/kratos-milsat-kpbesa40mlqd-c2-4-0-meter-light-quick-deploy-antenna/ Antenna diameter: 4 m Operating temperature: -40 °C Operating temperature: -58 °C @ (variant 2) Supply voltage: 24 ## Kratos NOMADIC MILSAT 4.0 Meter Carbon Fiber Antenna — Kratos Defense & Security Solutions [ground-stations] https://newspacemarket.com/products/kratos-nomadic-milsat-4-0-meter-carbon-fiber-antenna/ Antenna diameter: 4 m Operating temperature: -40 °C Operating temperature: -58 °C @ (variant 2) Supply voltage: 24 ## Ground Stations — Dhruva Space [ground-stations] https://newspacemarket.com/products/ground-stations/ Operating temperature: -10-55 °C ## GS-KIT — Alén Space [ground-stations] https://newspacemarket.com/products/gs-kit/ TRL: 9 ## SDR-RACK S-BAND — Alén Space [ground-stations] https://newspacemarket.com/products/sdr-rack-s-band/ TRL: 9 ## SDR-RACK UHF, VHF AND S-BAND — Alén Space [ground-stations] https://newspacemarket.com/products/sdr-rack-uhf-vhf-and-s-band/ TRL: 9 Power consumption: 50 W Power consumption: 50 W @ (variant 2) ## S-band Ground Station System — Groundcom.space [ground-stations] https://newspacemarket.com/products/s-band-ground-station-system/ Antenna diameter: 3 m EIRP: 49 dBW G/T: 11 ## VHF/UHF Ground Station — Groundcom.space [ground-stations] https://newspacemarket.com/products/vhf-uhf-ground-station/ G/T: -12 G/T: -11 @ (variant 2) ## Dual S/X-band Ground Station System — Groundcom.space [ground-stations] https://newspacemarket.com/products/dual-s-x-band-ground-station-system/ EIRP: 49 dBW G/T: 24.5 Antenna diameter: 3 m ## Backup Inertial Measuring Device — Glavkosmos [imus-gyros] https://newspacemarket.com/products/backup-inertial-measuring-device/ Design lifetime: 10 years ## Gyroscope Sensor for Measuring Angular Velocity Vector Projections 1 — Glavkosmos [imus-gyros] https://newspacemarket.com/products/gyroscope-sensor-for-measuring-angular-velocity-vector-projections-1/ Design lifetime: 15 years Lead time: 18 Mass: 12900 g Power consumption: 69 W ## Gyroscope Sensor for Measuring Angular Velocity Vector Projections 2 — Glavkosmos [imus-gyros] https://newspacemarket.com/products/gyroscope-sensor-for-measuring-angular-velocity-vector-projections-2/ Design lifetime: 15 years Lead time: 18 Mass: 12900 g Power consumption: 71 W ## Gyroscope Sensor for Measuring Angular Velocity Vector Projections 3 — Glavkosmos [imus-gyros] https://newspacemarket.com/products/gyroscope-sensor-for-measuring-angular-velocity-vector-projections-3/ Design lifetime: 10 years Mass: 1800 g ## Gyroscope Sensor for Measuring Angular Velocity Vector Projections-4 — Glavkosmos [imus-gyros] https://newspacemarket.com/products/gyroscope-sensor-for-measuring-angular-velocity-vector-projections-4/ Design lifetime: 17 years Mass: 13000 g ## Inertial Measurement Unit — Glavkosmos [imus-gyros] https://newspacemarket.com/products/inertial-measurement-unit/ Design lifetime: 15 years ## Angular accelerometer — Glavkosmos [imus-gyros] https://newspacemarket.com/products/angular-accelerometer/ Design lifetime: 17 years Lead time: 7 Mass: 300 g ## String accelerometer — Glavkosmos [imus-gyros] https://newspacemarket.com/products/string-accelerometer/ Design lifetime: 15 years Lead time: 6 Mass: 80 g ## TensorADCS-10m — Tensor Tech [imus-gyros] https://newspacemarket.com/products/tensor-tech-adcs-10m/ Envelope (L×W×H): 94 x 92 x 73.5 mm3; 1 Tuna-can + 0.25U Mass: 495 g Power consumption: 2.6 W ## Angular velocity sensor — SPUTNIX [imus-gyros] https://newspacemarket.com/products/angular-velocity-sensor/ Envelope (L×W×H): 54 x 52 x 20 (without fasteners) mm Mass: 75 g Bias instability: 2 °/h ## Fibre-Optic Gyroscope — SPUTNIX [imus-gyros] https://newspacemarket.com/products/fibre-optic-gyroscope/ Envelope (L×W×H): 275 x 275 x 160 mm (without fasteners) Envelope (L×W×H): 171 x 111 x 44 mm (without fasteners) @ (variant 2) Mass: 1700 g Bias instability: 0.005 °/h (max) Bias instability: 0.02 °/h (max) @ (variant 2) ## IMU (Inertial Measurement Unit) — Micro Aerospace Solutions [imus-gyros] https://newspacemarket.com/products/mas-masimu01-imu/ Power consumption: 0.6 W Mass: 40 g Mass: 80 g @ (variant 2) Supply voltage: 5-12 Envelope (L×W×H): 2.5 x 2.2 x 1.4" Bias instability: 1 °/h Power consumption: 0.6 W @ (variant 2) Mass: 20 g @ (variant 3) Mass: 60 g @ (variant 4) Supply voltage: 5-12 @ (variant 2) Envelope (L×W×H): 2 x 2 x 1.5" @ (variant 2) Bias instability: 0.2 °/h @ (variant 2) Power consumption: 1.3 W @ (variant 3) Mass: 100 g @ (variant 5) Mass: 150 g @ (variant 6) Supply voltage: 5-12 @ (variant 3) Envelope (L×W×H): 4 x 3 x 1.5" @ (variant 3) Bias instability: 0.013 °/h (max) ## MASIMU Inertial Measurement Units (IMU) — Micro Aerospace Solutions [imus-gyros] https://newspacemarket.com/products/mas-masimu02-imu/ Power consumption: 0.6 W Mass: 40 g Mass: 80 g @ (variant 2) Supply voltage: 5-12 Envelope (L×W×H): 2.5 x 2.2 x 1.4" Bias instability: 1 °/h Power consumption: 0.6 W @ (variant 2) Mass: 20 g @ (variant 3) Mass: 60 g @ (variant 4) Supply voltage: 5-12 @ (variant 2) Envelope (L×W×H): 2 x 2 x 1.5" @ (variant 2) Bias instability: 0.2 °/h @ (variant 2) Power consumption: 1.3 W @ (variant 3) Mass: 100 g @ (variant 5) Mass: 150 g @ (variant 6) Supply voltage: 5-12 @ (variant 3) Envelope (L×W×H): 4 x 3 x 1.5" @ (variant 3) Bias instability: 0.013 °/h (max) Flight heritage: MASIMU01 flew on University of Texas' FASTRAC microsatellite for AFRL ## ARIETIS — Innalabs [imus-gyros] https://newspacemarket.com/products/innalabs-arietis-gyro/ Angle random walk: 0.005 (max) Bias instability: 0.1 °/h (max) Bias instability: 1.5 °/h (max) @ (variant 2) Bias instability: 0.3 °/h (max) @ (variant 3) Power consumption: 8 W Random vibration: 26.2 ## ARS-16 Angular Rate Sensor / Dynapak-16 — AeroVironment (Tomahawk Robotics) [imus-gyros] https://newspacemarket.com/products/bluehalo-ars16-angular-rate-sensor/ Gyro range: 120 (min) ## STIM210 MEMS Gyroscope Module — Safran Electronics Defense Space [imus-gyros] https://newspacemarket.com/products/safran-stim210-mems-gyro/ Bias instability: 0.3 °/h Angle random walk: 0.15 Mass: 52 g Power consumption: 1.3 W Radiation tolerance (TID): 5-7 krad Flight heritage: 30+ satellite programs since 2012 ## GI-CVG-A23XXD A-Series 3-Axis CVG Digital Gyroscope — Innalabs [imus-gyros] https://newspacemarket.com/products/innalabs-gi-cvg-a23xxd-3axis/ Angle random walk: 0.01 Power consumption: 6 W (max) Mass: 1300 g (max) Envelope (L×W×H): 107 × 107 × 68 mm Connector: MIL-DTL-38999 Series III (13-pin) ## GI-CVG-N-Series 1 & 2-Axis Gyroscope (Tactical/Industrial Grade) — Innalabs [imus-gyros] https://newspacemarket.com/products/innalabs-gi-cvg-n-series/ Bias instability: 0.22 °/h (max) Bias instability: 10 °/h (max) @ (variant 2) Bias instability: 50 °/h (max) @ (variant 3) Mass: 71 g Mass: 105 g @ (variant 2) Mass: 115 g @ (variant 3) Envelope (L×W×H): H25 x D29.4 mm ## GI-CVG-U-Series 1 & 2-Axis Gyroscope — Innalabs [imus-gyros] https://newspacemarket.com/products/innalabs-gi-cvg-u-series/ Bias instability: 0.22 °/h (max) Bias instability: 10 °/h (max) @ (variant 2) Bias instability: 50 °/h (max) @ (variant 3) Mass: 1100 g Mass: 1200 g @ (variant 2) Envelope (L×W×H): H68 × L107 × W107 mm ## ARIETIS-NS 3-Axis Rad-Tolerant Space Gyroscope System — Innalabs [imus-gyros] https://newspacemarket.com/products/innalabs-arietis-ns/ Angle random walk: 0.005 (max) Bias instability: 0.1 °/h (max) Mass: 1200 g (max) Mass: 2300 g (max) @ (variant 2) Power consumption: 7 W (max) Operating temperature: -25 °C Random vibration: 18 Design lifetime: 16 years Design lifetime: 6 years @ (variant 2) ## Boreas A70 & A90 — Advanced Navigation [imus-gyros] https://newspacemarket.com/products/boreas-a70-a90/ Bias instability: 0.01 °/h Bias instability: 0.001 °/h @ (variant 2) ## Magnetometer — SPUTNIX [magnetometers] https://newspacemarket.com/products/magnetometer/ Envelope (L×W×H): 54 x 52 x 16 (without fasteners) mm Mass: 70 g Noise density: 100 nT ## Magnetometer (Compact & Deployable) — CubeSpace ADCS [magnetometers] https://newspacemarket.com/products/magnetometer-compact-deployable/ Envelope (L×W×H): 17x82x6.5* (Magnetometer Deployable) mm Envelope (L×W×H): 24×7.8×24 (Magnetometer Compact) mm @ (variant 2) Connector: Molex Micro-Lock Plus (Magnetometer Deployable) Connector: Molex Micro-Lock Plus (Magnetometer Compact) @ (variant 2) ## Microsatellite Magnetometer SX-SBOX-MAG-01 — SPUTNIX [magnetometers] https://newspacemarket.com/products/sputnix-sx-sbox-mag-01-magnetometer/ Envelope (L×W×H): 54 × 52 × 16 mm Mass: 70 g Noise density: 100 nT Power consumption: 0.8 W ## Emtech Space Snapshot Multi-Magnetometer Facility (Snapshot-MMF) — Emtech Space [magnetometers] https://newspacemarket.com/products/emtech-space-satellite-components/ Resolution: 18 nT ## Science Magnetometer (Space Payload Fluxgate Magnetometer) — Magson GmbH [magnetometers] https://newspacemarket.com/products/magson-science-magnetometer/ Flight heritage: BepiColombo, JUICE, Rosetta Lander, Venus Express, Themis, Double Star, MASCOT/Hayabusa2 ## Ship-Board Magnetometer — Magson GmbH [magnetometers] https://newspacemarket.com/products/magson-ship-board-magnetometer/ Flight heritage: RV Polarstern, RV Sonne ## Tow Fish Magnetometer — Magson GmbH [magnetometers] https://newspacemarket.com/products/magson-tow-fish-magnetometer/ Flight heritage: RV Sonne (BGR), Ben-Gurion University of the Negev ## Mag644 — Bartington Instruments [magnetometers] https://newspacemarket.com/products/mag644/ Operating temperature: -20 °C Measurement range: -20 µT Operating temperature: -20 °C (min) Operating temperature: 70 °C (max) Survival temperature: -20 °C (min) Survival temperature: 70 °C (max) Envelope (L×W×H): 24 x 12 x 5 Mass: 6 g (max) ## Electromagnetic Unit (EMU) – Magnetic Torquer for Nanosatellites — Glavkosmos [magnetorquers] https://newspacemarket.com/products/electromagnetic-unit-emu-magnetic-torquer-for-nanosatellites/ Design lifetime: 5 years Lead time: 3 Mass: 27 g Magnetic dipole moment: 0.001 A·m² (max) Power consumption: 0.2 W (max) Envelope (L×W×H): Ø9 × 64 mm ## Electromagnetic Unit (EMU) – Magnetic Torquer — Glavkosmos [magnetorquers] https://newspacemarket.com/products/electromagnetic-unit-emu-magnetic-torquer/ Design lifetime: 5 years Lead time: 6 Mass: 480 g Magnetic dipole moment: 0.05 A·m² (max) Power consumption: 2 W (max) Envelope (L×W×H): Ø17 × 345 mm ## Kinetic Moment Reset System — Glavkosmos [magnetorquers] https://newspacemarket.com/products/kinetic-moment-reset-system/ Design lifetime: 10 years Lead time: 14 Flight heritage: As part of the Resurs-DK spacecraft Mass: 50000 g Power consumption: 50 W Magnetic dipole moment: 1000 A·m² ## MM200 — AAC Clyde Space [magnetorquers] https://newspacemarket.com/products/aac-mm200/ Supply voltage: 3.3 Power consumption: 0.02 W (max) Operating temperature: -40 °C Radiation tolerance (TID): 30 krad @ up to Export status: ITAR free ## Zenno Astronautics Z01 Supertorquer — Zenno Astronautics [magnetorquers] https://newspacemarket.com/products/zenno-astronautics-z01-supertorquer/ Magnetic dipole moment: 2000 A·m² Magnetic dipole moment: 4000 A·m² @ (variant 2) Magnetic dipole moment: 8000 A·m² @ (variant 3) Mass: 3800 g Mass: 7500 g @ (variant 2) Mass: 15000 g @ (variant 3) Mass: 15000 g @ (variant 4) Mass: 30000 g @ (variant 5) Mass: 60000 g @ (variant 6) Mass: 8000 g @ (variant 7) Mass: 10000 g @ (variant 8) Mass: 16000 g @ (variant 9) Power consumption: 40 W Power consumption: 45 W @ (variant 2) Power consumption: 50 W @ (variant 3) Envelope (L×W×H): 150 x 260 x 295 mm Envelope (L×W×H): 150 x 300 x 360 mm @ (variant 2) Envelope (L×W×H): 160 x 400 x 440 mm @ (variant 3) Flight heritage: Since 2023 (Numero Uno, Vincent Freeman, Almighty Magnet missions) ## Zenno Astronautics Z01 Crew — Zenno Astronautics [magnetorquers] https://newspacemarket.com/products/zenno-astronautics-z01-crew/ Magnetic dipole moment: 100 A·m² Magnetic dipole moment: 300 A·m² @ (variant 2) Mass: 12000 g Mass: 14500 g @ (variant 2) Power consumption: 45 W Power consumption: 55 W @ (variant 2) Envelope (L×W×H): 400 x 200 x 200 mm Envelope (L×W×H): 420 x 220 x 220 mm @ (variant 2) Radiation tolerance (TID): 12 krad ## Magnetorquers — Tensor Tech [magnetorquers] https://newspacemarket.com/products/tensor-tech-mtq-board/ Power consumption: 1 W (max) Mass: 205 g (max) Envelope (L×W×H): 94 x 90 x 19 mm3 Connector: Molex Pico-Blade ## Magnetorquers (MTQ Board & TensorMTQ series) — Tensor Tech [magnetorquers] https://newspacemarket.com/products/tensor-tech-mtq-2/ Power consumption: 1 W (max) Mass: 205 g (max) Envelope (L×W×H): 94 x 90 x 19 mm3 Connector: Molex Pico-Blade ## Magnetic torquers control unit — SPUTNIX [magnetorquers] https://newspacemarket.com/products/magnetic-torquers-control-unit/ Envelope (L×W×H): 54 x 48 x 20 (without fasteners) mm Mass: 85 g ## EXA MT01 Compact Magnetorquer — EXA (Ecuadorian Space Agency) [magnetorquers] https://newspacemarket.com/products/exa-mt01-compact-magnetorquer/ Lead time: 2 ## Magnetorquer Rods (CR0002-CR0020) — CubeSpace ADCS [magnetorquers] https://newspacemarket.com/products/magnetorquer-rods-cr0002-cr0020/ Magnetic dipole moment: 0.2 A·m² Magnetic dipole moment: 0.3 A·m² @ (variant 2) Magnetic dipole moment: 0.4 A·m² @ (variant 3) Magnetic dipole moment: 0.63 A·m² @ (variant 4) Magnetic dipole moment: 0.8 A·m² @ (variant 5) Magnetic dipole moment: 1 A·m² @ (variant 6) Magnetic dipole moment: 1.2 A·m² @ (variant 7) Magnetic dipole moment: 2 A·m² @ (variant 8) Envelope (L×W×H): 10.5x47x10.5 Envelope (L×W×H): 10.5x59x10.5 @ (variant 2) Envelope (L×W×H): 10.5x59x10.5 @ (variant 3) Envelope (L×W×H): 10.5x77x10.5 @ (variant 4) Envelope (L×W×H): 10.5x92x10.5 @ (variant 5) Envelope (L×W×H): 10.5x92x10.5 @ (variant 6) Envelope (L×W×H): 13x122x13 @ (variant 7) Envelope (L×W×H): 13x152x13 @ (variant 8) Connector: Molex Pico-Look Connector: Molex Pico-Look @ (variant 2) Connector: Molex Pico-Look @ (variant 3) Connector: Molex Pico-Look @ (variant 4) Connector: Molex Pico-Look @ (variant 5) Connector: Molex Pico-Look @ (variant 6) Connector: Molex Pico-Look @ (variant 7) Connector: Molex Pico-Look @ (variant 8) ## Magnetorquers MTQ M6P & MTQ MP42 — NanoAvionics [magnetorquers] https://newspacemarket.com/products/nanoavionics-magnetorquers-mtq/ Mass: 205 g Magnetic dipole moment: 0.3 A·m² Magnetic dipole moment: 0.34 A·m² @ (variant 2) Connector: 3× 1.5 mm PicoLock™ (one per axis) Magnetic dipole moment: 2.5 A·m² @ (variant 3) Magnetic dipole moment: 5 A·m² @ (variant 4) Power consumption: 2.5 W ## Microsatellite Magnetic Torquers SX-MT Series — SPUTNIX [magnetorquers] https://newspacemarket.com/products/sputnix-sx-mt-series-magnetorquers/ Magnetic dipole moment: 1-30 A·m² Mass: 200-1200 g ## Magnetorquer Rods — NewSpace Systems (NSS) [magnetorquers] https://newspacemarket.com/products/nss-magnetorquer-rods/ TRL: 9 ## Torque Rods — Gimbal Space [magnetorquers] https://newspacemarket.com/products/gimbalspace-torque-rods/ Envelope (L×W×H): Multiple sizes ## Magnetorquer — Galamad Aerospace [magnetorquers] https://newspacemarket.com/products/16u-satellite-platform/ Power consumption: 1 W (max) ## Onboard Computer (OBC) — EnduroSat [obc-computers] https://newspacemarket.com/products/endurosat-onboard-computer/ Processor: ARM Cortex M7 RAM: 2 MB Storage: 2 GB Supply voltage: 12 Mass: 123 g Mass: 173 g @ (variant 2) ## Motherboard (w/Raspberry-Pi, Soft, and ADCS-controller) — Glavkosmos [obc-computers] https://newspacemarket.com/products/motherboard-w-raspberry-pi-soft-and-adcs-controller/ Operating system: Satellite control with ADCS — stabilization and target algorithm execution, three-axis orientation and stabilization Design lifetime: 1 years Lead time: 2 Envelope (L×W×H): 86.2 × 93.6 × 14 mm Mass: 60 g Supply voltage: 5-14 Power consumption: 1.7 W Operating temperature: -40-60 °C Random vibration: 12 TRL: 6 ## Motherboard (w/set of Sensors, Raspberry-Pi and Soft) — Glavkosmos [obc-computers] https://newspacemarket.com/products/motherboard-w-set-of-sensors-raspberry-pi-and-soft/ Operating system: Designed for satellite control. Provides satellite stabilization and target algorythms performance. Design lifetime: 1 years Lead time: 2 Operating system: No @ (variant 2) Envelope (L×W×H): 86.2 × 93.6 × 14 mm Mass: 59 g Power consumption: 0.9 W Random vibration: 12 ## Motherboard — Glavkosmos [obc-computers] https://newspacemarket.com/products/motherboard/ Operating system: Designed for satellite control. Provides satellite stabilization. Design lifetime: 1 years Lead time: 2 Operating system: No @ (variant 2) Envelope (L×W×H): 86.2 × 93.6 × 14 mm Mass: 55 g Power consumption: 0.25 W Random vibration: 12 ## Nanosatellite Onboard Computer — Glavkosmos [obc-computers] https://newspacemarket.com/products/nanosatellite-onboard-computer/ Design lifetime: 1 years Lead time: 6 Operating system: Yes CPU clock: 8 MHz Operating system: 16 Bit @ (variant 2) Operating system: 250 °/s @ (variant 3) ## Digital signal Processor 1879 VM 6Y — Glavkosmos [obc-computers] https://newspacemarket.com/products/digital-signal-processor-1879-%d0%b2%d0%bc-6y/ CPU clock: 500 MHz ## Integrated Circuit 1879 VM8Y — Glavkosmos [obc-computers] https://newspacemarket.com/products/integrated-circuit-1879-%d0%b2%d0%bc8y/ Operating temperature: -60 °C ## Integrated Circuit 1888 TX 018 — Glavkosmos [obc-computers] https://newspacemarket.com/products/integrated-circuit-1888-tx-018/ Operating system: Onboard multimedia processing, video/audio encoding/decoding, ARINC 818 interface switching for aircraft and vehicles Operating temperature: -50-70 °C CPU clock: 800 MHz CPU clock: 400 MHz @ (variant 2) Operating system: 3.3 V @ (variant 2) Supply voltage: 1.5 Supply voltage: 1 @ (variant 2) Supply voltage: 1.8 @ (variant 3) TRL: 8 ## VLSI SoCs with Integrated Microprocessor Cores — Glavkosmos [obc-computers] https://newspacemarket.com/products/vlsi-socs-with-integrated-microprocessor-cores/ Operating system: Demanding systems, digital signal processing systems Design lifetime: 3 years Lead time: 12 Operating system: No @ (variant 2) Mass: 10 g Operating temperature: -40-85 °C Processor: 32-bit RISC ## NxA-ECM — Aethero [obc-computers] https://newspacemarket.com/products/aethero-nxa-ecm/ Processor: Nvidia AGX Thor or Orin Radiation tolerance (TID): 50 krad TRL: 8 Envelope (L×W×H): Yes ## NxN-ECM — Aethero [obc-computers] https://newspacemarket.com/products/aethero-nxn-ecm/ Processor: Nvidia Orin NX or Nano Radiation tolerance (TID): 50 krad TRL: 9 Envelope (L×W×H): Yes ## DARA OBC — On-Board Computer — Alén Space [obc-computers] https://newspacemarket.com/products/alen-dara-obc/ Processor: ARM Cortex-M7, up to 280 MHz Operating system: FreeRTOS (CSP compatible) Power consumption: 0.28 W Operating system: 3-axis @ (variant 2) ## NxN-ECM (Nvidia-NX/Nano Edge Computing Module) — Aethero [obc-computers] https://newspacemarket.com/products/aethero-phobos-platform/ Processor: Nvidia Orin NX or Nano TRL: 9 ## Fusio RT Space Computer Core — 3D Plus (HEICO) [obc-computers] https://newspacemarket.com/products/3d-plus-fusio-rt-space-computer-core/ Operating system: 263 Storage: 64 GB RAM: 2048 MB Envelope (L×W×H): 32 × 32 mm² Operating temperature: -40 °C Radiation tolerance (TID): 40 krad (min) ## SP1-S Aquarius™ Radiation Tolerant 3U SpaceVPX SBC — Aitech Systems [obc-computers] https://newspacemarket.com/products/aitech-sp1-s/ Processor: NXP Layerscape LS1046A SoC Processor: Four 64-bit ARM Cortex-A72 @ (variant 2) CPU clock: 1800 MHz Power consumption: 50 W (max) Operating system: 100 krad (Si) Operating system: Linux, VxWorks RTOS @ (variant 2) ## SP0-S Radiation Tolerant 3U CompactPCI SBC — Aitech Systems [obc-computers] https://newspacemarket.com/products/aitech-sp0-s/ Processor: NXP PowerQUICC III MPC8548E CPU clock: 1000 MHz Storage: 1 GB Operating system: VxWorks 6.7 or 6.9 Operating system: >100 krad (Si) @ (variant 2) ## S-A2300 Radiation Tolerant COTS AI Supercomputer — Aitech Systems [obc-computers] https://newspacemarket.com/products/aitech-s-a2300/ Processor: 12-core ARM v8.2 64-bit Operating system: 20 krad (Si) ## S-A1760 Venus Space GPGPU — Aitech Systems [obc-computers] https://newspacemarket.com/products/aitech-s-a1760/ Processor: NVIDIA Denver 2 Dual-Core ARM + Cortex A57 Quad-Core ARM Storage: 32 GB Mass: 1000 g (max) ## On-Board Data Handling — VECTRONIC Aerospace GmbH [obc-computers] https://newspacemarket.com/products/vectronic-obdh/ Flight heritage: 7 slightly different On-Board Data Handling systems in Orbit and several others waiting for launch ## Unibap iX10 Space Computer — Unibap Space Solutions AB [obc-computers] https://newspacemarket.com/products/unibap-ix10/ Mass: 1400 g Processor: AMD Ryzen V1000 CPU RAM: 24576 MB Storage: 4096 GB Storage: 128 GB @ (variant 2) Operating system: Unibap OS (Linux) Mass: 1600 g @ without enclosure Envelope (L×W×H): 125 (W) x 125 (H) x 75 (D) [mm] Supply voltage: 12 Power consumption: 20 W (min) @ Depending on processing and storage load Power consumption: 40 W (max) @ Depending on processing and storage load Data interface: CAN Data interface: Ethernet @ (variant 2) Data interface: I2C @ (variant 3) Data interface: RS-422 @ (variant 4) Data interface: RS-485 @ (variant 5) Data interface: SpaceWire @ (variant 6) Data interface: USB @ (variant 7) Operating temperature: -20 °C (min) Operating temperature: 55 °C (max) ## iX5 — Unibap Space Solutions AB [obc-computers] https://newspacemarket.com/products/unibap-ix5/ Processor: Unibap Qseven e2160 compute module Processor: AMD Steppe Eagle CPU @ (variant 2) Processor: AMD Radeon CPU @ (variant 3) Processor: Intel Movidius Myriad X @ (variant 4) RAM: 2048 MB Storage: 120 GB Data interface: CAN Data interface: Ethernet @ (variant 2) Data interface: I2C @ (variant 3) Data interface: RS-422 @ (variant 4) Data interface: RS-232 @ (variant 5) Data interface: SpaceWire @ (variant 6) Data interface: SPI @ (variant 7) Data interface: ADC inputs @ (variant 8) Data interface: USB @ (variant 9) Mass: 421 g Envelope (L×W×H): 100 (W) × 100 (H) × 50 (D) [mm] Power consumption: 10 W @ min Power consumption: 30 W @ max Supply voltage: 12 Operating system: Unibap OS (Linux) Flight heritage: 5 missions launched Power consumption: 10-30 W Operating temperature: -20 °C ## TetraPLEX — TelePIX [obc-computers] https://newspacemarket.com/products/telepix-chouette-tma/ Flight heritage: 2024 Processor: RISC-V FPGA SoC+ 4-core Envelope (L×W×H): 100 mm x 100 mm x 90 mm Mass: 500 g ## DP-OBC-0402 On Board Computer — Data Patterns (India) Ltd. [obc-computers] https://newspacemarket.com/products/data-patterns-india-dp-obc-0402/ Processor: e200 core processor, dual core Flight heritage: NIUSAT, INS-1A, INS-1B, INS-1C (ISRO nanosatellite missions) ## SC-OBC Module A1 — Space Cubics Inc. [obc-computers] https://newspacemarket.com/products/space-cubics-sc-obc-module-a1/ Processor: Xilinx Artix-7 FPGA Processor: Cortex-M3 / MicroBlaze-V @ (variant 2) Operating system: Zephyr RTOS CPU clock: 24 MHz RAM: 4 MB RAM: 32 MB @ (variant 2) RAM: 0.5 MB @ (variant 3) Connector: 80 pin, 0.5 mm pitch Power consumption: 2 W Envelope (L×W×H): 70 x 70 x 9.6 mm Mass: 30 g ## SC-OBC Module V1 — Space Cubics Inc. [obc-computers] https://newspacemarket.com/products/space-cubics-sc-obc-module-v1/ Processor: AMD Versal AI Edge Series VE2302 Processor: Dual core Arm Cortex-A72 up to 1.3 GHz (48/32 KByte L1 with parity and ECC, 1 MByte L2 with ECC) @ (variant 2) Processor: Dual core Arm Cortex-R5F up to 600 MHz (32/32 KByte L1, 256 KByte TCM with ECC) @ (variant 3) Processor: Microchip IGLOO2 @ (variant 4) Operating system: Linux on APU, Zephyr RTOS on RPU Operating temperature: -40-80 °C Envelope (L×W×H): 100 x 150 mm Mass: 110 g ## Robust On-Board Data Handling Unit — S4 – Smart Small Satellite Systems GmbH [obc-computers] https://newspacemarket.com/products/s4-3-axis-attitude-control-reaction-wheel/ Flight heritage: More than 5 years without any interruption of service in polar LEO CPU clock: 19000 MHz Mass: 20 g (max) Envelope (L×W×H): 20x20x20 mm Supply voltage: 5 Supply voltage: 3.3-8.4 Power consumption: 0.4 W (max) Power consumption: 1 W (max) @ (variant 2) Operating temperature: -50-50 °C Survival temperature: -60-100 °C Design lifetime: 5 years ## NANOobc-2 — SkyLabs d.o.o. [obc-computers] https://newspacemarket.com/products/skylabs-nanoobc-2/ TRL: 9 Processor: PicoSkyFT 8/16-bit core with single precision FPU ## NANOhpm-obc — SkyLabs d.o.o. [obc-computers] https://newspacemarket.com/products/skylabs-nanohpm-obc/ TRL: 9 Processor: NOEL-V 32-bit core (RV32IMAFD) with FPU ## NANOhpc-obc — SkyLabs d.o.o. [obc-computers] https://newspacemarket.com/products/skylabs-nanohpc-obc/ TRL: 9 Processor: 4x RISC-V 64-bit processors @ max 600 MHz RAM: 4096 MB ## NANOhpc-DPU — SkyLabs d.o.o. [obc-computers] https://newspacemarket.com/products/skylabs-nanohpc-dpu/ TRL: 5 RAM: 32768 MB RAM: 32768 MB @ (variant 2) Processor: 4x RISC-V 64-bit processors @ max 600 MHz ## NANOhpc-AI — SkyLabs d.o.o. [obc-computers] https://newspacemarket.com/products/skylabs-nanohpc-ai/ TRL: 5 Processor: 4x RISC-V 64-bit processors @ max 600 MHz ## picoRTU system — SkyLabs d.o.o. [obc-computers] https://newspacemarket.com/products/skylabs-picortu-system/ TRL: 7 ## Scalable Compute Platform — Rogue Space Systems Corp. [obc-computers] https://newspacemarket.com/products/rogue-space-scalable-compute-platform-scp/ Flight heritage: Flight-demonstrated on OTP-2 ## On-board computer (with a set of sensors and ADC controller) — SPUTNIX [obc-computers] https://newspacemarket.com/products/on-board-computer-with-a-set-of-sensors-and-adc-controller/ Envelope (L×W×H): 84 x 94 x 19 mm (±0.2 mm) Processor: attitude rate sensor, magnetometers, EM-torquer driver, detumbling mode, bootloader Processor: ADCS control, bootloader @ (variant 2) ## SpaceWire-router and on-board storage device of the on-board computer complex — SPUTNIX [obc-computers] https://newspacemarket.com/products/spacewire-router-and-on-board-storage-device-of-the-on-board-computer-complex/ Envelope (L×W×H): 117 x 111 x 51 (without fasteners) mm Mass: 960 g RAM: 8 MB ## Pluggable Socketed Processor Module D (PSPM D) — Pumpkin, Inc. [obc-computers] https://newspacemarket.com/products/pumpkin-pluggable-socketed-processor-module-d-pspm-d/ Processor: Microchip PIC24FJ256GA110 (16-bit MCU) or Microchip dsPIC33FJ256GP710 (16-bit DSC) Processor: 100-pin ZIF (Zero Insertion Force) socket @ (variant 2) ## Pluggable Processor Module D2 (PPM D2) — Pumpkin, Inc. [obc-computers] https://newspacemarket.com/products/pumpkin-pluggable-processor-module-d2-ppm-d2/ Processor: Microchip dsPIC33FJ256GP710 (16-bit DSC, soldered) RAM: 0.25 MB RAM: 30720 MB @ (variant 2) CPU clock: 20 MHz ## Pluggable Socketed Processor Module E (PSPM E) — Pumpkin, Inc. [obc-computers] https://newspacemarket.com/products/pumpkin-pluggable-socketed-processor-module-e-pspm-e/ Processor: Microchip PIC24FJ256GB210 (16-bit MCU) Processor: 100-pin ZIF (Zero Insertion Force) socket @ (variant 2) RAM: 0.25 MB RAM: 0.0938 MB @ (variant 2) CPU clock: 16 MHz Connector: Micro-B USB ## Pluggable Processor Module D1 (PPM D1) — Pumpkin, Inc. [obc-computers] https://newspacemarket.com/products/pumpkin-pluggable-processor-module-d1-ppm-d1/ Processor: Microchip PIC24FJ256GA110 (16-bit MCU, soldered) RAM: 0.25 MB RAM: 0.0156 MB @ (variant 2) CPU clock: 16 MHz ## Pluggable Processor Module E1 (PPM E1) — Pumpkin, Inc. [obc-computers] https://newspacemarket.com/products/pumpkin-pluggable-processor-module-e1-ppm-e1/ Processor: Microchip PIC24FJ256GB210 (16-bit MCU, soldered) RAM: 0.25 MB RAM: 0.0938 MB @ (variant 2) CPU clock: 16 MHz ## On-Board Computer (OBC) — Terma [obc-computers] https://newspacemarket.com/products/terma-obc/ Processor: LEON2/3/4 (SPARC V8/V9 ISA) ## MASTER II Next Generation Satellite OBC — 2NDSpace Srl [obc-computers] https://newspacemarket.com/products/master-ii-next-generation-satellite-obc/ Processor: PolarFire SoC with integrated FPGA fabric ## Nexus-01 Edge-AI Onboard Computer — Akula Tech [obc-computers] https://newspacemarket.com/products/akula-tech-nexus-01-obc/ Flight heritage: Nexus-01 mission, SpaceX Falcon 9 via Dhruva Space LEAP-1 ## TILE — Thermal Integrated LEO Edge Compute Module — Sophia Space [obc-computers] https://newspacemarket.com/products/sophia-space-tile/ Envelope (L×W×H): ~1 m² surface area, ~1 cm thick (foldable) Operating system: SOOS (Sophia Orbital Operating System) — scheduling, thermal, firmware, fault routing Flight heritage: Spun out of Mandala Space Ventures; commercializes Caltech/JPL orbital compute technology; team of former JPL engineers ## OBC — Space Inventor ApS [obc-computers] https://newspacemarket.com/products/obc/ Operating system: FreeRTOS ## Z7000-P4 — Space Inventor ApS [obc-computers] https://newspacemarket.com/products/z7000-p4/ Processor: Dual-core ARM Cortex-A9 MP-Core with NEON SIMD Operating system: FreeRTOS (Linux also supported) ## Proton100k Single Board Computer — Voyager Technologies [obc-computers] https://newspacemarket.com/products/spacemicro-proton100k-single-board-computer/ Operating system: Linux and real-time OS options ## SP0 Rad-Tolerant 3U CompactPCI SBC — Aitech Systems [obc-computers] https://newspacemarket.com/products/sp0-radiation-tolerant-3u-compactpci-sbc/ Processor: PowerQUICC-III MPC8548E @ 833 MHz, 1.0 or 1.2 GHz CPU clock: 333 MHz Operating system: VxWorks 6.x Power consumption: 10 W ## S950 — Aitech Systems [obc-computers] https://newspacemarket.com/products/s950-radiation-tolerant-3u-compactpci-sbc/ Processor: High Performance PowerPC® 750FX Processor CPU clock: 1000 MHz Operating system: Greater than 15 krad (Si) (unshielded) ## SBC-1461 — CesiumAstro [obc-computers] https://newspacemarket.com/products/sbc-1461-single-board-computer/ TRL: 9 ## SBCFA1000 Single-Board Computer — ZIN Technologies [obc-computers] https://newspacemarket.com/products/zin-technologies-sbcfa1000/ Flight heritage: NASA ISS research activities (400+ experiments) ## SP240 On-Board Computer — Novi [obc-computers] https://newspacemarket.com/products/novi-space-sp240-on-board-computer/ Flight heritage: ISS, SpaceX Transporter-12 and prior missions ## ICE Cube — On-Board Computer Unit (OBCU) — N7 Space [obc-computers] https://newspacemarket.com/products/n7space-ice-cube-obcu/ Processor: LEON3 SPARC V8 Operating system: RTEMS ## Sparrow OBC Node — Needronix [obc-computers] https://newspacemarket.com/products/needronix-sparrow-obc-node/ Operating system: RTOS ## Gaisler Embedded Computer Systems and Microelectronics — Gaisler [obc-computers] https://newspacemarket.com/products/gaisler-gr712rc-processor/ Flight heritage: Millions of flight hours since 2001 ## GR740 Module (ICU CPU Module) — EREMS [obc-computers] https://newspacemarket.com/products/erems-gr740-module/ Processor: GR740 ## Modular ICU (On-Board Computer Architecture) — EREMS [obc-computers] https://newspacemarket.com/products/erems-modular-icu/ Processor: GR740 microprocessor Processor: NG-ULTRA MPSoC @ (variant 2) ## LCS MiniNODE Industrial Computing System — LiquidCool Solutions [obc-computers] https://newspacemarket.com/products/liquidcool-mininode-industrial-pc/ Processor: AMD Ryzen 5 5600G (6C/12T, 4.4 GHz boost) Storage: 1024 GB Envelope (L×W×H): 16″ W × 18″ D × 4.5″ H Operating temperature: 0 °C Operating system: Windows, Linux ## Satellite Attitude Control Computer — MinoSpace [obc-computers] https://newspacemarket.com/products/minospace-attitude-control-computer/ Envelope (L×W×H): Standard 3U Mass: 50000-200000 g ## ZHP Payload Computer — Serenum Space [obc-computers] https://newspacemarket.com/products/serenum-zhp-payload-computer/ Processor: Zynq 7015, dual-core Cortex-A9 up to 766 MHz, with FPGA Connector: 2x CAN, I2C, power, PPS (configurable in/out) Operating system: Linux (Yocto-based) RAM: 1024 MB Storage: 2 GB Power consumption: 2.8 W Power consumption: 3.5-7 W Operating temperature: -20 °C ## Rugged Embedded Computing for Space — Curtiss-Wright Defense Solutions [obc-computers] https://newspacemarket.com/products/curtiss-wright-space-computing/ Processor: Intel Xeon-D, NXP PowerPC (radiation-tolerant variants) ## AI-Powered On-Board Satellite Data Processing — KP Labs [obc-computers] https://newspacemarket.com/products/kp-labs-onboard-ai/ Flight heritage: ESA Φsat-2 (Phisat-2) mission, 2024 (Europe's AI-in-space demonstrator) ## PyCubed Plus–based Avionics Board — CubeSat Aerospace [obc-computers] https://newspacemarket.com/products/pycubed-plus-based-avionics-board-3654/ Processor: STM32F765 ARM Cortex-M7, 216 MHz Connector: 6× 10-pin FFC for solar panels (X+/X–, Y+/Y–, Z+/Z–) Connector: 2× 20-pin FFC (for Communication and Payload Boards) @ (variant 2) Flight heritage: In-orbit heritage through open-source community and academic missions ## On Board Computer — Alba Orbital [obc-computers] https://newspacemarket.com/products/on-board-computer-1479/ Envelope (L×W×H): 42 mm x 42 mm ## Constellation Remote Terminal Unit (cRTU) — Beyond Gravity (ex-RUAG Space) [obc-computers] https://newspacemarket.com/products/beyond-gravity-crtu-constellation-remote-terminal-unit/ Radiation tolerance (TID): 30 krad @ > Supply voltage: 28 Supply voltage: 5 @ (variant 2) Supply voltage: 28 @ (variant 3) Supply voltage: 28 @ (variant 4) Operating temperature: -20-60 °C Random vibration: 15 ## CFC-400XS Compact Flight Computer — Innoflight [obc-computers] https://newspacemarket.com/products/innoflight-cfc-400xs-flight-computer/ Processor: Defense-grade Xilinx UltraScale+ MPSoC (GPP + FPGA) TRL: 9 Flight heritage: Since 2021 ## MNE-405 / MNE-410 Mission Networking Electronics — Innoflight [obc-computers] https://newspacemarket.com/products/innoflight-mne-405-410-mission-networking-electronics/ Envelope (L×W×H): 197 x 150 x 82 mm Mass: 2700 g Power consumption: 40 W TRL: 9 Flight heritage: Since 2025 ## CFC-405XP / CFC-450XP Compact Flight Computer — Innoflight [obc-computers] https://newspacemarket.com/products/innoflight-cfc-405xp-450xp-flight-computer/ Processor: Defense-grade Xilinx UltraScale+ MPSoC (GPP + FPGA) Mass: 547 g Power consumption: 18-25 W TRL: 9 Flight heritage: Since 2025 ## CFC-510P Compact Flight Computer — Innoflight [obc-computers] https://newspacemarket.com/products/innoflight-cfc-510p-flight-computer/ Processor: AMD Ryzen GPU Flight heritage: CFC-500S / CFC-500P (NVIDIA Tegra K1 GPU) Mass: 539 g Power consumption: 40 W TRL: 9 Flight heritage: Since 2025 @ (variant 2) ## CFC-600P Compact Flight Computer (AI/ML) — Innoflight [obc-computers] https://newspacemarket.com/products/innoflight-cfc-600p-flight-computer/ Processor: Defense-grade AMD Versal AI Edge adaptive SoC Mass: 500 g Power consumption: 70 W TRL: 5 ## Typhoon Edge — CAVU Aerospace [obc-computers] https://newspacemarket.com/products/typhoon-edge/ Processor: NVIDIA JETSON ORIN AGX Industrial & Microchip PolarFire SoC MPFS460T RAM: 65536 MB RAM: 209715.2 MB @ (variant 2) Supply voltage: 12 Power consumption: 150 W Envelope (L×W×H): 220 mm × 130 mm × 46 mm Operating temperature: -40 °C Processor: 12-core Arm Cortex-A78AE v8.2 64-bit CPU @ (variant 2) ## OBC-Hyper-Polar — CAVU Aerospace [obc-computers] https://newspacemarket.com/products/obc-hyper-polar/ Processor: RISC-V MSS: 4× 64-bit U54 application cores + 1× E51 monitor core ## OBC-Cube-Polar — CAVU Aerospace [obc-computers] https://newspacemarket.com/products/obc-cube-polar/ Processor: Microchip PolarFire SoC Flash Based FPGA SoC Processor: Quad 64-bit RISC-V on FPGA + 1 RISC-V Monitoring Core @ (variant 2) Mass: 80 g ## OBC-104 — CAVU Aerospace [obc-computers] https://newspacemarket.com/products/obc-104/ Processor: ARM Cortex-M3 on FPGA Processor: Microchip/Microsemi SmartFuion2 Flash Based FPGA @ (variant 2) Processor: 150 DMIPS @ 128 MHz @ (variant 3) RAM: 0.5 MB Storage: 0.25 GB ## OBC PolarFire VPX — CAVU Aerospace [obc-computers] https://newspacemarket.com/products/obc-polarfire-vpx/ Processor: Microchip MPFS460T-1FCG1152I / MPFS460TS-1FCG1152I (with security) Envelope (L×W×H): 100 × 160 mm (220 mm depth option) ## CDH-FS — CAVU Aerospace [obc-computers] https://newspacemarket.com/products/cdh-fs/ Operating system: 30Krad (Si)/yr Operating temperature: -40 °C Design lifetime: 3-5 years Envelope (L×W×H): 205x203x87 mm Mass: 4250 g Supply voltage: 5 Power consumption: 3 W ## OBC-64 — CAVU Aerospace [obc-computers] https://newspacemarket.com/products/obc-64/ Processor: PIC64-HPSC1000 / PIC64-HPSC1100 family (RISC-V vector compute) Processor: 8× RISC-V SiFive® X280 vector cores + S7 system controller @ (variant 2) Envelope (L×W×H): ~100 × 160 × 25 mm ## Gigabit Ethernet (GbE) Space Switch — IQ Spacecom [obc-computers] https://newspacemarket.com/products/gigabit-ethernet-gbe-space-switch/ Mass: 150 g Supply voltage: 9-36 Power consumption: 3.5 W Operating temperature: -20 °C ## Antelope — KP Labs [obc-computers] https://newspacemarket.com/products/antelope/ Envelope (L×W×H): 13.24 x 95.9 x 90.1 mm ## EDGE-1100 — ibeos [obc-computers] https://newspacemarket.com/products/edge-1100/ Processor: Quad-core, 8-threaded x86 ## On-board Computer — DSI Aerospace Technology [obc-computers] https://newspacemarket.com/products/on-board-computer-2/ Processor: 160 MIPS/FLOPS ## GSC6203 6U OpenVPX GPGPU Coprocessing Board — Mercury Systems [obc-computers] https://newspacemarket.com/products/gsc6203-6u-openvpx-gpgpu-coprocessing-board/ RAM: 32768 MB Power consumption: 150 W ## Mechanical Unit of Antenna Pointing System. Type 1 — Glavkosmos [pointing-mechanisms] https://newspacemarket.com/products/mechanical-unit-of-antenna-pointing-system-type-1/ Operating temperature: -50-50 °C Design lifetime: 10 years Design lifetime: 14 years @ (variant 2) Lead time: 6 ## Mechanical Unit of Antenna Pointing System. Type 2 — Glavkosmos [pointing-mechanisms] https://newspacemarket.com/products/mechanical-unit-of-antenna-pointing-system-type-2/ Lead time: 6 Operating temperature: -50-50 °C Design lifetime: 10 years Design lifetime: 14 years @ (variant 2) ## Mechanical Unit of Antenna Pointing System. Type 3 — Glavkosmos [pointing-mechanisms] https://newspacemarket.com/products/mechanical-unit-of-antenna-pointing-system-type-3/ Operating temperature: -40-50 °C Design lifetime: 15 years Design lifetime: 19 years @ (variant 2) ## Mechanical Unit of Antenna Pointing System. Type 4 — Glavkosmos [pointing-mechanisms] https://newspacemarket.com/products/mechanical-unit-of-antenna-pointing-system-type-4/ Design lifetime: 15 years Lead time: 6 Operating temperature: -30-60 °C Design lifetime: 15 years @ (variant 2) Design lifetime: 19.5 years @ (variant 3) ## Reflector Drive Mechanism — Glavkosmos [pointing-mechanisms] https://newspacemarket.com/products/reflector-drive-mechanism/ Design lifetime: 10 years Lead time: 6 Operating temperature: -30-60 °C Envelope (L×W×H): 410 x 255 x 220 mm Mass: 12000 g ## Reflector Transfer Mechanism — Glavkosmos [pointing-mechanisms] https://newspacemarket.com/products/reflector-transfer-mechanism/ Design lifetime: 10 years Lead time: 6 Operating temperature: -40-50 °C Envelope (L×W×H): 320 × 230 × 230 mm Mass: 7000 g Design lifetime: 15 years @ (variant 2) ## Two-degree-of-freedom Antenna Pointing Device. Type 1 — Glavkosmos [pointing-mechanisms] https://newspacemarket.com/products/two-degree-of-freedom-antenna-pointing-device-type-1/ Design lifetime: 10 years Lead time: 6 Operating temperature: -40-50 °C Design lifetime: 10 years @ (variant 2) Envelope (L×W×H): 370 x 370 x 250 mm Mass: 7000 g ## Two-degree-of-freedom Device for Antenna Pointing. Type 2 — Glavkosmos [pointing-mechanisms] https://newspacemarket.com/products/two-degree-of-freedom-device-for-antenna-pointing-type-2/ Design lifetime: 5 years Lead time: 6 Design lifetime: 5 years @ (variant 2) Envelope (L×W×H): 855 × 725 × 233 mm Mass: 21000 g ## Two-degree-of-freedom Device for Antenna Pointing. Type 3 — Glavkosmos [pointing-mechanisms] https://newspacemarket.com/products/two-degree-of-freedom-device-for-antenna-pointing-type-3/ Design lifetime: 5 years Lead time: 6 Design lifetime: 5 years @ (variant 2) Envelope (L×W×H): 565 × 500 × 210 mm, not exceeding Mass: 13000 g ## Two-degree-of-freedom device for antenna pointing. Type 4 — Glavkosmos [pointing-mechanisms] https://newspacemarket.com/products/two-degree-of-freedom-device-for-antenna-pointing-type-4/ Design lifetime: 10 years Lead time: 6 Operating temperature: -20-50 °C Design lifetime: 10 years @ (variant 2) Envelope (L×W×H): 442 x 362 x 164 mm Mass: 8400 g ## COBRA™ Gimbal — Tethers Unlimited, Inc. (AMERGINT) [pointing-mechanisms] https://newspacemarket.com/products/tethers-unlimited-cobra-uhpx-gimbal/ Flight heritage: ! Mass: 276 g Angular resolution: 0.0767 deg (min) Mass: 491 g @ (variant 2) Angular resolution: 0.0008 deg (min) @ (variant 2) ## 3POD — Comat [pointing-mechanisms] https://newspacemarket.com/products/comat-3pod-antenna-pointing-mechanism/ Travel range: 360 Design lifetime: 10 years ## MaalonDrive Rotary Micro-Positioning Drive — Micromotion GmbH [pointing-mechanisms] https://newspacemarket.com/products/micromotion-maalondrive-rotary/ Envelope (L×W×H): 6 mm, 8 mm, 10 mm ## RasuunDrive Linear Spindle Drive — Micromotion GmbH [pointing-mechanisms] https://newspacemarket.com/products/micromotion-rasuundrive-linear/ Travel range: 3 (min) ## Mars 2020 Perseverance Rover’s Primary Robotic Arm — Motiv Space Systems [pointing-mechanisms] https://newspacemarket.com/products/mars-2020-perseverance-rover-robotic-arm/ Angular resolution: 1 deg (max) Mass: 76000 g ## xLink™ System — Motiv Space Systems [pointing-mechanisms] https://newspacemarket.com/products/xlink-robotic-arm-system/ Flight heritage: Developed by the same team that built the robotic arm for NASA/JPL’s Mars 2020 Perseverance rover Mass: 22700 g Supply voltage: 28 ## Custom Mechanisms (Mastcam-Z, SOMS Filter Wheel, Mastcam-Z Filter Wheel) — Motiv Space Systems [pointing-mechanisms] https://newspacemarket.com/products/mastcam-z-optomechanical-mechanisms/ Flight heritage: Mars 2020 Perseverance Rover (Mastcam-Z, Mastcam-Z Filter Wheel) Flight heritage: Earth orbit imaging platform (SOMS Filter Wheel) @ (variant 2) ## Space Mechanisms and Solar Array Systems — SENER Aeroespacial [pointing-mechanisms] https://newspacemarket.com/products/sener-space-mechanisms/ Flight heritage: Solar Orbiter, JUICE, Sentinel-1/2/3, Ariane 5/6 ## Space Mechanisms (SADA, Gimbals, Rotary Actuators) — Moog Space Defense Group [pointing-mechanisms] https://newspacemarket.com/products/moog-space-mechanisms/ Flight heritage: Apollo, Pioneer, Cassini, Hubble, Galileo (navigation), Europa Clipper, Gateway ## Microwave Electrothermal Thruster (MET) — Momentus Space [propulsion] https://newspacemarket.com/products/momentus-microwave-electrothermal-thruster-met/ Propellant: Distilled water ## MULTI-LAYER BELLOWS — Glavkosmos [propulsion] https://newspacemarket.com/products/multi-layer-bellows/ Design lifetime: 6 years Lead time: 2 ## WELDED STEEL DIAPHRAGM BELLOWS — Glavkosmos [propulsion] https://newspacemarket.com/products/welded-steel-diaphragm-bellows/ Design lifetime: 6 years Lead time: 2 ## Attitude Control Propulsion Unit — Glavkosmos [propulsion] https://newspacemarket.com/products/attitude-control-propulsion-unit/ Design lifetime: 19 years Lead time: 7 Propellant: Xenon (State Standard GOST 10219-77) Design lifetime: 15.5 years @ (variant 2) Mass: 330 g ## 3TU Thruster Unit — Glavkosmos [propulsion] https://newspacemarket.com/products/3tu-thruster-unit/ Design lifetime: 10.5 years Lead time: 12 Power consumption: 14.6 W Envelope (L×W×H): 344 × 344 × 185 mm Mass: 5700 g ## Adjustment and Braking Engine — Glavkosmos [propulsion] https://newspacemarket.com/products/adjustment-and-braking-engine/ Propellant: UDMH/NTO Specific impulse: 2855 Feed/tank pressure: 14.7 bar Feed/tank pressure: 1.37 bar @ (variant 2) Supply voltage: 27 Mass: 8000 g Thrust: 464000 mN Thrust: 116000 mN @ (variant 2) ## Attitude Control Thruster Unit Based on Modified Thermocatalytic Low Thrusters — Glavkosmos [propulsion] https://newspacemarket.com/products/attitude-control-thruster-unit-based-on-modified-thermocatalytic-low-thrusters/ Design lifetime: 10 years Lead time: 12 Power consumption: 14.6 W Envelope (L×W×H): 208 × 150 × 128 mm Mass: 1550 g ## Attitude Control Thruster Unit Based on Thermocatalytic Low Thrusters — Glavkosmos [propulsion] https://newspacemarket.com/products/attitude-control-thruster-unit-based-on-thermocatalytic-low-thrusters/ Design lifetime: 10.5 years Lead time: 12 Power consumption: 14.6 W Envelope (L×W×H): 208 × 150 × 128 mm Mass: 1900 g ## Bipropellant Thruster 11d — Glavkosmos [propulsion] https://newspacemarket.com/products/bipropellant-thruster-11d/ Thrust: 53900 mN Propellant: UDMH/NTO Specific impulse: 2842 Feed/tank pressure: 11.8 bar Feed/tank pressure: 1.03 bar @ (variant 2) Supply voltage: 27 Mass: 1500 g ## Bipropellant Thruster 17D — Glavkosmos [propulsion] https://newspacemarket.com/products/bipropellant-thruster-17d/ Flight heritage: ALMAZ orbital station; BRIZ booster units; KVANT-2, KRISTALL, SPEKTR, PRIRODA (MIR station modules); Russia ZARYA module (ISS); STRELA launcher upper stage Propellant: UDMH / NTO Specific impulse: 2688 Feed/tank pressure: 14.7 bar Feed/tank pressure: 7.8-34.3 bar Supply voltage: 27 Thrust: 13300 mN ## Cold Ammonia Corrective Propulsion System — Glavkosmos [propulsion] https://newspacemarket.com/products/cold-ammonia-corrective-propulsion-system/ Design lifetime: 5 years Lead time: 12 ## Cool Gas Thruster — Glavkosmos [propulsion] https://newspacemarket.com/products/cool-gas-thruster/ Specific impulse: 1657.9 Feed/tank pressure: 17.65 bar Feed/tank pressure: 1.47 bar @ (variant 2) Supply voltage: 27 Mass: 105 g ## Correction Unit (CU) based on Stationary Plasma Thruster with a Nominal Discharge Power of 1350 W and XFC Unit — Glavkosmos [propulsion] https://newspacemarket.com/products/correction-unit-cu-based-on-stationary-plasma-thruster-with-a-nominal-discharge-power-of-1350-w-and-xfc-unit/ Lead time: 10 Power consumption: 1350 W Supply voltage: 300 Specific impulse: 1600 Power consumption: 208 W @ (variant 2) Total impulse: 2.6 N·s (min) Mass: 6500 g Thrust: 83 mN ## Corrective Propulsion System 95 — Glavkosmos [propulsion] https://newspacemarket.com/products/corrective-propulsion-system-95/ Thrust: 16200000 mN Thrust: 3.2 mN @ (variant 2) Design lifetime: 7 years Lead time: 12 Specific impulse: 1.4 Power consumption: 180 W Mass: 20000 g Supply voltage: 26-34 ## Corrective Propulsion System UD-AIPD — Glavkosmos [propulsion] https://newspacemarket.com/products/corrective-propulsion-system/ Design lifetime: 15 years Lead time: 12 Specific impulse: 1.35 Power consumption: 150 W Mass: 8000 g Supply voltage: 26-34 Thrust: 20000000 mN Thrust: 3 mN @ (variant 2) ## Dual-mode Stationary Plasma Thruster with a Nominal Discharge Power of 2500/1350 W — Glavkosmos [propulsion] https://newspacemarket.com/products/dual-mode-stationary-plasma-thruster-with-a-nominal-discharge-power-of-2500-1350-w/ Lead time: 10 Specific impulse: 2200 Total impulse: 4.5 N·s (min) Mass: 5700 g ## Electric Thruster for Spacecraft with Mass up to 1500 kg — Glavkosmos [propulsion] https://newspacemarket.com/products/electric-thruster-for-spacecraft-with-mass-up-to-1500-kg/ Lead time: 12 Power consumption: 0.93 W (max) Specific impulse: 1860 Mass: 3100 g Thrust: 42 mN ## Electric Thruster for Spacecraft with Mass up to 2500-3000 kg — Glavkosmos [propulsion] https://newspacemarket.com/products/electric-thruster-for-spacecraft-with-mass-up-to-2500-3000-kg/ Thrust: 95 mN Lead time: 12 Power consumption: 2.4 W (max) Specific impulse: 2680 Mass: 5250 g ## Electric Thruster for Spacecraft with Mass up to 3000 kg 1 — Glavkosmos [propulsion] https://newspacemarket.com/products/electric-thruster-for-spacecraft-with-mass-up-to-3000-kg-1/ Lead time: 12 Specific impulse: 1550 (min) Mass: 5200 g ## Electric Thruster for Spacecraft with Mass up to 3000 kg — Glavkosmos [propulsion] https://newspacemarket.com/products/electric-thruster-for-spacecraft-with-mass-up-to-3000-kg/ Lead time: 12 Power consumption: 1.65 W Specific impulse: 2680 Mass: 6000 g Thrust: 72 mN ## Electric Thruster for Spacecraft with Mass up to 500 kg — Glavkosmos [propulsion] https://newspacemarket.com/products/electric-thruster-for-spacecraft-with-mass-up-to-500-kg/ Thrust: 18 mN Lead time: 12 Power consumption: 0.35 W Specific impulse: 1450 Mass: 2000 g ## Electrically Powered Cruise Engine — Glavkosmos [propulsion] https://newspacemarket.com/products/electrically-powered-cruise-engine/ Lead time: 12 Power consumption: 10.5 W Specific impulse: 2580 Mass: 11800 g Thrust: 520 mN ## High-powered Electric Thruster for Spacecraft with Mass up to 3000 kg — Glavkosmos [propulsion] https://newspacemarket.com/products/high-powered-electric-thruster-for-spacecraft-with-mass-up-to-3000-kg/ Lead time: 12 Specific impulse: 1700 Mass: 8000 g ## Integrated Thruster Unit 13 — Glavkosmos [propulsion] https://newspacemarket.com/products/integrated-thruster-unit-13/ Design lifetime: 15 years Lead time: 14 Power consumption: 50 W (max) Envelope (L×W×H): 776 × 760 × 420 mm Mass: 31000 g (max) ## Integrated Thruster Unit ITU-5000M — Glavkosmos [propulsion] https://newspacemarket.com/products/integrated-thruster-unit/ Design lifetime: 15 years Lead time: 14 Power consumption: 50 W (max) Envelope (L×W×H): 776 × 760 × 416 mm Mass: 31000 g (max) ## Low Power Stationary Plasma Thruster with 50 mm Diameter of the Accelerating Channel — Glavkosmos [propulsion] https://newspacemarket.com/products/low-power-stationary-plasma-thruster-with-50-mm-diameter-of-the-accelerating-channel/ Lead time: 10 Power consumption: 220 W Supply voltage: 180 Specific impulse: 860 Power consumption: 179 W @ (variant 2) Total impulse: 0.13 N·s (min) Mass: 1230 g Thrust: 14 mN ## Low Power Stationary Plasma Thruster with 70 mm Diameter of the Accelerating Channel — Glavkosmos [propulsion] https://newspacemarket.com/products/low-power-stationary-plasma-thruster-with-70-mm-diameter-of-the-accelerating-channel/ Thrust: 39 mN Lead time: 10 Power consumption: 669 W Supply voltage: 300 Specific impulse: 1470 Power consumption: 446 W @ (variant 2) Total impulse: 0.49 N·s (min) Mass: 1500 g ## Low Power Stationary Plasma Thruster — Glavkosmos [propulsion] https://newspacemarket.com/products/low-power-stationary-plasma-thruster/ Lead time: 10 Specific impulse: 1000 Total impulse: 0.04 N·s (min) Mass: 1100 g ## Modified Low Power Stationary Plasma Thruster with 50 mm Diameter of the Accelerating Channel — Glavkosmos [propulsion] https://newspacemarket.com/products/modified-low-power-stationary-plasma-thruster-with-50-mm-diameter-of-the-accelerating-channel/ Lead time: 10 Specific impulse: 930 Total impulse: 0.27 N·s (min) Mass: 1320 g ## Modified Low Power Stationary Plasma Thruster with 70 mm Diameter of the Accelerating Channel — Glavkosmos [propulsion] https://newspacemarket.com/products/modified-low-power-stationary-plasma-thruster-with-70-mm-diameter-of-the-accelerating-channel/ Lead time: 10 Power consumption: 660 W Supply voltage: 300 Specific impulse: 1500 Power consumption: 275 W @ (variant 2) Total impulse: 1 N·s (min) Mass: 2400 g Thrust: 40 mN ## Modified Stationary Plasma Thruster with a Discharge Power of up to 5 kW — Glavkosmos [propulsion] https://newspacemarket.com/products/modified-stationary-plasma-thruster-with-a-discharge-power-of-up-to-5-kw/ Lead time: 12 Specific impulse: 1900 Total impulse: 14 N·s (min) Mass: 8100 g ## Modified Stationary Plasma Thruster with a Nominal Discharge Power of 1350 W — Glavkosmos [propulsion] https://newspacemarket.com/products/modified-stationary-plasma-thruster-with-a-nominal-discharge-power-of-1350-w/ Lead time: 10 Power consumption: 1350 W Supply voltage: 300 Specific impulse: 1700 Power consumption: 329 W @ (variant 2) Total impulse: 4.5 N·s (min) Mass: 4100 g Thrust: 92 mN ## Modified Thermocatalytic Low Thruster — Glavkosmos [propulsion] https://newspacemarket.com/products/modified-thermocatalytic-low-thruster/ Design lifetime: 10.5 years Lead time: 10 Propellant: 20(35)/20 kg Envelope (L×W×H): 112 × 70 × 38 mm Mass: 200 g Propellant: Hydrazine @ (variant 2) ## Modified Thermocatalytic Thrusters — Glavkosmos [propulsion] https://newspacemarket.com/products/modified-thermocatalytic-thrusters/ Propellant: 20 kg Envelope (L×W×H): 110 × 102 × 54 mm Mass: 440 g ## Multichannel Electric Thruster — Glavkosmos [propulsion] https://newspacemarket.com/products/multichannel-electric-thruster/ Lead time: 12 Power consumption: 5-10 W Specific impulse: 1500-4000 Mass: 12000 g ## Propulsion System [PS] for Nanosatellite Platform — Glavkosmos [propulsion] https://newspacemarket.com/products/propulsion-system-ps-for-nanosatellite-platform/ Thrust: 3-10 mN Design lifetime: 3 years Lead time: 12 Mass: 1300 g Power consumption: 3-5 W Power consumption: 12 W Supply voltage: 5-12 Envelope (L×W×H): 91 × 96 × 130 mm ## Station Keeping Thruster Unit Based on Modified Thermocatalytic Thrusters — Glavkosmos [propulsion] https://newspacemarket.com/products/station-keeping-thruster-unit-based-on-modified-thermocatalytic-thrusters/ Design lifetime: 10 years Lead time: 12 Power consumption: 14.6 W Envelope (L×W×H): 176 × 217 × 130 mm Mass: 1700 g ## Station Keeping Thruster Unit Based on Thermocatalytic Thrusters — Glavkosmos [propulsion] https://newspacemarket.com/products/station-keeping-thruster-unit-based-on-thermocatalytic-thrusters/ Design lifetime: 7 years Lead time: 12 Power consumption: 14.6 W Envelope (L×W×H): 176 × 246 × 127 mm Mass: 1700 g ## Stationary Plasma Thruster with a Discharge Power of up to 25 kW — Glavkosmos [propulsion] https://newspacemarket.com/products/stationary-plasma-thruster-with-a-discharge-power-of-up-to-25-kw/ Lead time: 12 Power consumption: 25000 W (max) Supply voltage: 800 (max) Specific impulse: 3200 (max) Power consumption: 1000 W (max) @ (variant 2) Total impulse: 38 N·s (max) Mass: 25000 g Thrust: 1070 mN (max) ## Stationary Plasma Thruster with a Discharge Power of up to 5 kW — Glavkosmos [propulsion] https://newspacemarket.com/products/stationary-plasma-thruster-with-a-discharge-power-of-up-to-5-kw/ Lead time: 12 Supply voltage: 300 Specific impulse: 1680 Total impulse: 14 N·s (min) Mass: 8800 g ## Stationary Plasma Thruster with a Discharge Power of up to 6 kW — Glavkosmos [propulsion] https://newspacemarket.com/products/stationary-plasma-thruster-with-a-discharge-power-of-up-to-6-kw/ Lead time: 12 Specific impulse: 1850 Total impulse: 20 N·s (min) Mass: 8100 g Propellant: xenon ## Stationary Plasma Thruster with a Nominal Discharge Power of 1350 W — Glavkosmos [propulsion] https://newspacemarket.com/products/stationary-plasma-thruster-with-a-nominal-discharge-power-of-1350-w/ Lead time: 10 Power consumption: 1350 W Supply voltage: 300 Specific impulse: 1600 Power consumption: 386 W @ (variant 2) Total impulse: 2.6 N·s (min) Mass: 3500 g Propellant: xenon Thrust: 83 mN ## Thermocatalytic Low Thruster — Glavkosmos [propulsion] https://newspacemarket.com/products/thermocatalytic-low-thruster/ Design lifetime: 10.5 years Lead time: 10 Specific impulse: 216 Propellant: 20/50 kg Envelope (L×W×H): 131 × 130 × 45 mm Mass: 460 g Propellant: Hydrazine @ (variant 2) ## Thermocatalytic Thrusters — Glavkosmos [propulsion] https://newspacemarket.com/products/thermocatalytic-thrusters/ Specific impulse: 170 (min) Propellant: 20(150) kg Envelope (L×W×H): 110 × 129 × 67 mm Mass: 440 g ## Thrust Module (TM) Based on Thruster with 70 mm Diameter of the Accelerating Channel with Xenon Flow Controller Unit (XF — Glavkosmos [propulsion] https://newspacemarket.com/products/thrust-module-tm-based-on-thruster-with-70-mm-diameter-of-the-accelerating-channel-with-xenon-flow-controller-unit-xfc-unit/ Lead time: 12 Power consumption: 669 W Supply voltage: 300 Specific impulse: 1470 Power consumption: 238 W @ (variant 2) Total impulse: 0.5 N·s (min) Mass: 2800 g Thrust: 39 mN ## TU1 Thruster Unit Based on Modified Thermocatalytic Low Thruster — Glavkosmos [propulsion] https://newspacemarket.com/products/tu1-thruster-unit-based-on-modified-thermocatalytic-low-thruster/ Design lifetime: 5 years Lead time: 12 Power consumption: 7.3 W Envelope (L×W×H): 171 × 58 × 109 mm Mass: 590 g ## TU3 Truster Unit Based on Modified Thermocatalytic Low Thrusters — Glavkosmos [propulsion] https://newspacemarket.com/products/tu3-truster-unit-based-on-modified-thermocatalytic-low-thrusters/ Design lifetime: 5 years Lead time: 12 Power consumption: 7.3 W Envelope (L×W×H): 232 × 179.5 × 79.5 mm Mass: 1300 g ## Xenon Cold Gas Thruster — Glavkosmos [propulsion] https://newspacemarket.com/products/xenon-cold-gas-thruster/ Design lifetime: 10 years Lead time: 10 Specific impulse: 40 ## RD-120MS — Glavkosmos [propulsion] https://newspacemarket.com/products/rd-120ms/ Feed/tank pressure: 181.6 bar Envelope (L×W×H): 4714/2600 mm ## RD-171 M — Glavkosmos [propulsion] https://newspacemarket.com/products/rd-171-m/ Lead time: 22 Specific impulse: 309 Feed/tank pressure: 250 bar Envelope (L×W×H): 4150 / 3565 mm ## RD-180 — Glavkosmos [propulsion] https://newspacemarket.com/products/rd-180/ Design lifetime: 10 years Lead time: 18 Specific impulse: 311 Feed/tank pressure: 261.7 bar Envelope (L×W×H): 3600 / 3200 mm ## RD-181 — Glavkosmos [propulsion] https://newspacemarket.com/products/rd-181/ Design lifetime: 11 years Lead time: 14 Specific impulse: 311 Feed/tank pressure: 262.6 bar Envelope (L×W×H): 3680 / 2100 mm ## RD-182 (120M) — Glavkosmos [propulsion] https://newspacemarket.com/products/rd-182-120m/ Specific impulse: 298 Feed/tank pressure: 181.6 bar Envelope (L×W×H): 3653/2600 mm ## Bipropellant Thruster — Glavkosmos [propulsion] https://newspacemarket.com/products/bipropellant-thruster/ Propellant: UDMH/NTO Specific impulse: 2989 Feed/tank pressure: 14.7 bar Feed/tank pressure: 1.27 bar @ (variant 2) Supply voltage: 27 Mass: 3000 g Thrust: 392000 mN ## RS-25 Rocket Engine — Space Launch System Core Stage Propulsion — Aerojet Rocketdyne (L3Harris) [propulsion] https://newspacemarket.com/products/rs-25-rocket-engine-space-launch-system-core-stage-propulsion/ Propellant: Fuel: liquid hydrogen; Oxidizer: liquid oxygen; mixture ratio (O/F) 6.0 Feed/tank pressure: 206.4291 bar Envelope (L×W×H): Length 168 in; diameter 96 in Flight heritage: Evolved from SSME (135 shuttle flights); RS-25 and SSME have over 1.1 million seconds of firing time ## MUSIC Electric Propulsion System — aliena [propulsion] https://newspacemarket.com/products/aliena-music-eps/ Propellant: Xe / Kr gas Flight heritage: Self-ignition on a 3U nanosatellite January 2022; MUSIC-HM on a 12U satellite July 2023 ## AIS-VAT1-PQ Micro Vacuum Arc Thruster — Applied Ion Systems [propulsion] https://newspacemarket.com/products/applied-ion-systems-ais-vat1-pq/ Thrust: 0.0042 mN Thrust: 0.013 mN @ (variant 2) Thrust: 0.026 mN @ (variant 3) Total impulse: 0.13 N·s Specific impulse: 87 Envelope (L×W×H): 42x42x21 mm Mass: 56 g Propellant: Bismuth Lead time: 4 ## AIS-VAT1-DUO Dual Micro Vacuum Arc Thruster — Applied Ion Systems [propulsion] https://newspacemarket.com/products/applied-ion-systems-ais-vat1-duo/ Total impulse: 0.26 N·s Specific impulse: 87 Envelope (L×W×H): 84x42x21 mm Mass: 84 g Propellant: Bismuth Lead time: 4 Thrust: 0.0084 mN Thrust: 0.026 mN @ (variant 2) Thrust: 0.052 mN @ (variant 3) ## AIS-VAT1-QUAD Quad Micro Vacuum Arc Thruster — Applied Ion Systems [propulsion] https://newspacemarket.com/products/applied-ion-systems-ais-vat1-quad/ Thrust: 0.0168 mN Thrust: 0.052 mN @ (variant 2) Thrust: 0.104 mN @ (variant 3) Total impulse: 0.52 N·s Specific impulse: 87 Envelope (L×W×H): 84x84x21 mm Mass: 177 g Propellant: Bismuth Lead time: 4 ## AIS-VAT2 Vacuum Arc Thruster — Applied Ion Systems [propulsion] https://newspacemarket.com/products/applied-ion-systems-ais-vat2/ Power consumption: 20 W Total impulse: 8 N·s Envelope (L×W×H): 92x92x50 mm Mass: 700 g Propellant: Bismuth Thrust: 0.128 mN Thrust: 0.032 mN @ (variant 2) ## AIS-VAT3 Vacuum Arc Thruster — Applied Ion Systems [propulsion] https://newspacemarket.com/products/applied-ion-systems-ais-vat3/ Thrust: 0.256 mN Thrust: 0.064 mN @ (variant 2) Power consumption: 40 W Total impulse: 8 N·s Envelope (L×W×H): 92x92x75 mm Propellant: Bismuth ## AIS-SWAG1-PQ Sublimation Warm Gas Thruster — Applied Ion Systems [propulsion] https://newspacemarket.com/products/applied-ion-systems-ais-swag1-pq/ Thrust: 0.12 mN Propellant mass: 9.5 g Propellant: Solid Unpressurized Adamantane Power consumption: 5 W Total impulse: 3 N·s Specific impulse: 20 Envelope (L×W×H): 42x42x54 mm Mass: 214 g Propellant: 9.5 g @ (variant 2) Lead time: 4-6 ## AIS-VAT1-PQ — Applied Ion Systems [propulsion] https://newspacemarket.com/products/applied-ion-systems-ais-ilis0/ Total impulse: 0.13 N·s Specific impulse: 87 Envelope (L×W×H): 42x42x21 mm Mass: 56 g Propellant: Bismuth Lead time: 6 Thrust: 0.026 mN Thrust: 0.001 mN (max) ## AIS-SWAG1-QUAD — Applied Ion Systems [propulsion] https://newspacemarket.com/products/applied-ion-systems-ais-ilis2-b/ Thrust: 0.48 mN Propellant mass: 38 g Propellant: Solid Unpressurized Adamantane Power consumption: 20 W Total impulse: 12 N·s Specific impulse: 20 Envelope (L×W×H): 86x86x54 mm Mass: 860 g Propellant: 38 g @ (variant 2) Lead time: 8 ## URA HET (Hall-effect Thruster) – WETHET / AquaHET — URA Thrusters [propulsion] https://newspacemarket.com/products/ura-het-hall-effect-thruster/ Specific impulse: 3000 Power consumption: 2000 W Propellant: O2/H2 (water/oxygen electrolysis) Specific impulse: 3000 @ (variant 2) Power consumption: 5000 W @ (variant 2) Propellant: O2/H2 (water/oxygen electrolysis) @ (variant 2) Thrust: 48 mN Thrust: 120 mN @ (variant 2) ## URA ICE Thruster (Electrolysis Chip Thruster) — URA Thrusters [propulsion] https://newspacemarket.com/products/ura-ice-thruster/ Thrust: 10 mN Specific impulse: 310 Envelope (L×W×H): <4 U Mass: 8200 g (max) Propellant: H2O ## URA MET (Microwave Electrothermal Thruster) – AQUAMET / NMET / COMET / XMET / KMET — URA Thrusters [propulsion] https://newspacemarket.com/products/ura-met-microwave-electrothermal-thruster/ Specific impulse: 500-1000 Power consumption: 1000 W (max) Propellant: H2O Thrust: 30-150 mN ## URA HYDRA Hybrid Propulsion System — URA Thrusters [propulsion] https://newspacemarket.com/products/ura-hydra-hybrid-propulsion-system/ Propellant: Water (electrolysed on-board to O2/H2) ## VACCO CubeSat Propulsion and ChEMS Flow Control Modules — VACCO Industries [propulsion] https://newspacemarket.com/products/vacco-cubesat-propulsion-chems-flow-control-modules/ Flight heritage: JPL MarCO (first CubeSats to Mars), NEA Scout, CuSP, AFRL PUC Mass: 1600 g (max) Operating temperature: 0 °C Feed/tank pressure: 206.8428-0.6895 bar Feed/tank pressure: 310.2642 bar Feed/tank pressure: 517.107 bar @ (variant 2) Feed/tank pressure: 0-4.8263 bar @ (variant 2) Supply voltage: 0-130 Supply voltage: 24-33 @ (variant 2) Feed/tank pressure: 0-5 bar @ (variant 3) ## VACCO Space Component Integration Modules — VACCO Industries [propulsion] https://newspacemarket.com/products/vacco-space-component-integration-modules/ Flight heritage: JAXA ETS-VIII satellite Feed/tank pressure: 0-149.961 bar Feed/tank pressure: 220.6323 bar Feed/tank pressure: 372.317 bar @ (variant 2) Feed/tank pressure: 2.7579 bar @ (variant 3) Operating temperature: -17-70 °C ## VACCO Etched Disc Propellant and Pressurant Filters — VACCO Industries [propulsion] https://newspacemarket.com/products/vacco-etched-disc-filters/ Flight heritage: In production since 1961; 98% of NASA Space Shuttle filters; Mars Science Laboratory (Curiosity) Mass: 68 g Feed/tank pressure: 275.7904 bar Feed/tank pressure: 827.3712 bar @ (variant 2) Feed/tank pressure: 413.6856 bar @ (variant 3) Feed/tank pressure: 413.6856 bar @ (variant 4) ## VACCO Wintec Metal Mesh Filters — VACCO Industries [propulsion] https://newspacemarket.com/products/vacco-wintec-metal-mesh-filters/ Flight heritage: In production since 1964; Lockheed Martin A2100 satellite bus propulsion pressurant system ## Uvireso Bismuth Hall-Effect Thruster — UVIRESO Space [propulsion] https://newspacemarket.com/products/uvireso-bismuth-hall-effect-thruster/ Propellant: Bismuth (replaces xenon/krypton) Power at thrust: 100-500 W Power consumption: 100-500 W ## Green Propulsion System (4x1N HTP Monopropellant Module) — Thaliana Space [propulsion] https://newspacemarket.com/products/thaliana-space-green-propulsion-system/ Propellant: 98% HTP Mass: 25000 g (max) Mass: 12000 g (max) @ (variant 2) Total impulse: 14000 N·s Envelope (L×W×H): 380 x 380 x 380 [mm] Propellant: 9.63 L @ (variant 2) ## 1N HTP Monopropellant Thruster — Thaliana Space [propulsion] https://newspacemarket.com/products/thaliana-space-1n-htp-thruster/ Thrust: 1000 mN Propellant: 98% HTP (monopropellant) ## 420N HTP Bipropellant Kick-Stage Engine — Thaliana Space [propulsion] https://newspacemarket.com/products/thaliana-space-420n-htp-bipropellant-engine/ Flight heritage: ESA GRACE 1 & GRACE 2 programs, Łukasiewicz - ILOT ## Plugim Electrospray Thruster — XIROI [propulsion] https://newspacemarket.com/products/xiroi-plugim-electrospray-thruster/ Thrust: 0.35 mN (min) Total impulse: 2000 N·s (min) Specific impulse: 800 (min) Mass: 550 g (max) Envelope (L×W×H): < 9.5 cm x 9.5 cm x 5 cm (requirement) Envelope (L×W×H): 100 x 100 x 75 mm @ (variant 2) ## AERIS — Stars Edge [propulsion] https://newspacemarket.com/products/starsedge-aeris/ Propellant: Ionized residual atmospheric molecules ## STAR-3D Vortex-Hybrid Rocket Engine — Vaya Space [propulsion] https://newspacemarket.com/products/vaya-space-star-3d/ Propellant: Solid fuel grain, 3D-printed from recycled thermoplastics (spiral/vortex grain design) Thrust: 110000000 mN ## Arka Hall Effect Thruster Series — Bellatrix Aerospace [propulsion] https://newspacemarket.com/products/bellatrix-arka-hall-effect-thruster/ Thrust: 3 mN Thrust: 7 mN @ (variant 2) Thrust: 13.2 mN @ (variant 3) Thrust: 86 mN @ (variant 4) Thrust: 260 mN @ (variant 5) Power consumption: 50 W Specific impulse: 860 Power consumption: 100 W @ (variant 2) Specific impulse: 1000 @ (variant 2) Power consumption: 200 W @ (variant 3) Specific impulse: 1300 @ (variant 3) Power consumption: 1.5 W @ (variant 4) Specific impulse: 1600 @ (variant 4) Power consumption: 5 W @ (variant 5) Specific impulse: 2000 @ (variant 5) ## Rudra Green Propulsion Thruster Series — Bellatrix Aerospace [propulsion] https://newspacemarket.com/products/bellatrix-rudra-green-propulsion/ Min impulse bit: 50 mN·s (max) Specific impulse: 235 Min impulse bit: 100 mN·s (max) @ (variant 2) Specific impulse: 250 @ (variant 2) Min impulse bit: 2500 mN·s (max) @ (variant 3) Specific impulse: 255 @ (variant 3) Propellant: Green monopropellant (non-toxic alternative to hydrazine) Thrust: 1000 mN Thrust: 5000 mN @ (variant 2) Thrust: 100000 mN @ (variant 3) ## Jal Microwave Plasma Thruster — Bellatrix Aerospace [propulsion] https://newspacemarket.com/products/bellatrix-jal-microwave-plasma-thruster/ Thrust: 300 mN Power consumption: 5000 W Specific impulse: 1050 Propellant: Water Propellant: $0 @ (variant 2) ## BLUE 1S — Perigee Aerospace [propulsion] https://newspacemarket.com/products/perigee-blue-1s/ Propellant: LOX/LNG (liquid methane) Specific impulse: 324 Specific impulse: 362 @ (variant 2) Thrust: 34000000 mN Thrust: 38000000 mN @ (variant 2) ## CUBESAT THRUSTER — Perigee Aerospace [propulsion] https://newspacemarket.com/products/perigee-skyblue/ Thrust: 200 mN Thrust: 450 mN @ (variant 2) Propellant: R236fa Propellant: R236fa @ (variant 2) Specific impulse: 41 Specific impulse: 41 @ (variant 2) Mass: 1170 g Mass: 3360 g @ (variant 2) Total impulse: 250 N·s Total impulse: 800 N·s @ (variant 2) ## Hermes — Reaction Dynamics [propulsion] https://newspacemarket.com/products/reaction-dynamics-hermes/ Propellant: Hydrogen Peroxide (HTP) Propellant: Safer and REACH compliant alternative to hydrazine, safe to store @ (variant 2) ## Mira Orbital Transfer Vehicle — Impulse Space [propulsion] https://newspacemarket.com/products/impulse-space-mira/ Propellant: Ethane/LOX ## Hybrid Propulsion System (HIS) — DELTAV Space Technologies [propulsion] https://newspacemarket.com/products/deltav-space-technologies-hybrid-propulsion-system-his/ Specific impulse: 290 Propellant: 30 kg Mass: 60000 g Envelope (L×W×H): 1 m base diameter x 1 m height Flight heritage: In development for AYAP-1 lunar hard-landing mission; hybrid propulsion tested as second stage of SORS sounding rocket, exceeding 100 km altitude Thrust: 650000 mN Propellant mass: 30000 g ## Vigoride — Momentus Space [propulsion] https://newspacemarket.com/products/momentus-vigoride/ Flight heritage: Vigoride-3 (May 2022: solar array deployment anomaly, partial payload deployment); Vigoride-5 (Jan 2023: successful, hosted Caltech Space Solar Power Demonstrator); Vigoride-6 (Apr 2023: successful, minor software-error affected 2 NASA cubesats); Vigoride ## TILE Ionic Liquid Electrospray Thruster — Accion Systems [propulsion] https://newspacemarket.com/products/accion-systems-tile/ Specific impulse: 800-2000 Power consumption: 1-20 W Thrust: 0.05-1 mN ## Apollo Constellation Engine — Apollo Fusion (Astra) [propulsion] https://newspacemarket.com/products/apollo-fusion-apollo-constellation-engine/ Propellant: Krypton, Xenon, or proprietary propellants (multi-propellant capable) Flight heritage: Selected by York Space Systems for a 10+ satellite LEO constellation (2022); used on Spaceflight Inc. Sherpa-LTE orbital transfer vehicle; multiple on-orbit flights since ~2021 as Astra Spacecraft Engine; ground tested to 12,000+ cycles ## B20 Thruster — Dawn Aerospace [propulsion] https://newspacemarket.com/products/dawn-aerospace-b20-thruster/ Specific impulse: 240-285 Propellant: Nitrous oxide oxidizer / propene fuel, self-pressurizing non-toxic bipropellant Mass: 695 g Flight heritage: 160+ Dawn B-series thrusters launched to orbit on 55+ satellites via SpaceX Transporter, Starlink rideshare, Rocket Lab Electron, and Arianespace Vega; customers include Pixxel, Sidus Space, Blue Canyon Technologies, AstroForge, CNES, and ESA Thrust: 6460-18110 mN ## TunaCan Thruster — SteamJet Space [propulsion] https://newspacemarket.com/products/steamjet-tunacan-thruster/ Specific impulse: 172 Power consumption: 20 W (max) Propellant: Water (non-toxic, low-pressure) Envelope (L×W×H): 80 x 80 mm (cylindrical) Flight heritage: In-orbit since 2022; SatRevolution 'Above the Clouds' mission; multiple undisclosed LEO commercial deployments Thrust: 5-20 mN ## TunaTank Thruster — SteamJet Space [propulsion] https://newspacemarket.com/products/steamjet-tunatank-thruster/ Thrust: 5-20 mN Specific impulse: 172 Power consumption: 20 W (max) Propellant: Water; optional water-alcohol mixture (freezing point -30°C) Flight heritage: 7 legacy systems operational in orbit ## Thruster One — SteamJet Space [propulsion] https://newspacemarket.com/products/steamjet-thruster-one/ Specific impulse: 172 Total impulse: 1200 N·s Power consumption: 20 W (max) Propellant: Water / water-alcohol mixture Flight heritage: Six systems in orbit since 2022; 2023 MBRSC PHI-Demo mission; selected for NaraSpace K-RadCube mission on Artemis II Thrust: 5-20 mN ## Chimera LEO — Epic Aerospace [propulsion] https://newspacemarket.com/products/epic-aerospace-chimera-leo/ Propellant: In-house produced 95-98% concentrated hydrogen peroxide ## Chimera GEO — Epic Aerospace [propulsion] https://newspacemarket.com/products/epic-aerospace-chimera-geo/ Propellant: In-house produced 95-98% concentrated hydrogen peroxide ## Supernova — Portal Space Systems [propulsion] https://newspacemarket.com/products/portal-space-systems-supernova/ Propellant: Safe, storable monopropellant ## Starfire (Direct Fusion Drive) — Princeton Satellite Systems [propulsion] https://newspacemarket.com/products/starfire-direct-fusion-drive/ Power consumption: 1-10 W Propellant: Deuterium–Helium-3 (D-He3) ## Small Plasma Brake (APB-S) — Aurora Propulsion Technologies [propulsion] https://newspacemarket.com/products/aurora-apb-s/ Mass: 450 g (max) ## ARM-O (Aurora Resistojet Module for Orbit Control) — Aurora Propulsion Technologies [propulsion] https://newspacemarket.com/products/aurora-apb-l/ Propellant: Water ## Electric Propulsion Systems — ATI Space (Advanced Technology Institute) [propulsion] https://newspacemarket.com/products/ati-electric-propulsion/ Propellant: PTFE, ADN green, xenon ## ASCEND Propulsion System — Ascend Beyond Space [propulsion] https://newspacemarket.com/products/spark-battery-passivator/ Operating temperature: -40-85 °C ## Tempest Reaction Control System — Ascend Beyond Space [propulsion] https://newspacemarket.com/products/tempest-rcs/ Propellant: Cold gas / monopropellant ## Nereus 20 M — Pangea Aerospace [propulsion] https://newspacemarket.com/products/pangea-nereus-20-m/ Propellant: H2O2 (hydrogen peroxide) Thrust: 5000-22000 mN ## Nereus 20 B — Pangea Aerospace [propulsion] https://newspacemarket.com/products/pangea-nereus-20-b/ Thrust: 20000 mN Propellant: H2O2 / Jet A ## Nereus 200 — Pangea Aerospace [propulsion] https://newspacemarket.com/products/pangea-nereus-200/ Propellant: H2O2 / Jet A Thrust: 100000-240000 mN ## Cryox — Pangea Aerospace [propulsion] https://newspacemarket.com/products/pangea-cryox/ Thrust: 30000000 mN Propellant: LOX / Methane (methalox) ## Arcos — Pangea Aerospace [propulsion] https://newspacemarket.com/products/pangea-arcos/ Propellant: LOX / Methane (methalox) Thrust: 750000000 mN ## Kronos — Pangea Aerospace [propulsion] https://newspacemarket.com/products/pangea-kronos/ Propellant: LOX / Methane (methalox) ## Hall Effect Thrusters (HT-100/HT-400/HT-5k) — SITAEL S.p.A. [propulsion] https://newspacemarket.com/products/sitael-hall-effect-thrusters/ Flight heritage: ESA SMART-1 lunar mission and other programmes ## Cluster of IFM Nano Thruster for Smallsats — ENPULSION GmbH [propulsion] https://newspacemarket.com/products/cluster-of-ifm-nano-thruster-for-smallsats/ Lead time: 12 ## IFM Nano Thruster for CubeSats — ENPULSION GmbH [propulsion] https://newspacemarket.com/products/ifm-nano-thruster-for-cubesats/ Lead time: 16 ## BET-MAX Electrospray Thruster System — Busek Co. [propulsion] https://newspacemarket.com/products/busek-bet-max-electrospray-thruster-system/ Envelope (L×W×H): 3U ## BIT-3 RF Ion Thruster — Busek Co. [propulsion] https://newspacemarket.com/products/busek-bit-3-rf-ion-thruster/ Power consumption: 56-75 W Propellant: Iodine (also compatible with xenon) Flight heritage: NASA SLS deep-space CubeSat missions (2021) ## Astra Satellite Engine (ASE) — Astra Space [propulsion] https://newspacemarket.com/products/astra-satellite-engine-ase/ Propellant: Xenon (Xe) or Krypton (Kr) Total impulse: 300000 N·s Total impulse: 300000 N·s @ (variant 2) Flight heritage: Yes — 110+ engines shipped and on-orbit ## Starling Ardent — Benchmark Space Systems [propulsion] https://newspacemarket.com/products/starling-cold-gas-propulsion-system/ Thrust: 10 mN Min impulse bit: 0.05 mN·s (max) Total impulse: 2000 N·s Propellant: Non-toxic inert gas (ODPS™) Power consumption: 10-15 W Power consumption: 15-50 W @ (variant 2) ## Peregrine Bipropellant Thruster System — Benchmark Space Systems [propulsion] https://newspacemarket.com/products/peregrine-bipropellant-thruster-system/ Propellant: HTP (High-Test Peroxide) + Alcohol Specific impulse: 270 (min) Min impulse bit: 0.5 mN·s (max) Mass: 4000 g Power consumption: 5 W Thrust: 100 mN ## Spacecraft Propulsion Products — IHI Aerospace [propulsion] https://newspacemarket.com/products/ihi-satellite-propellant-tanks/ Propellant: Launch: cancelled; Orbit: Lunar orbit; Propellant load: N2H4 143 kg, NTO 49 kg; Thrusters: 500N main engine, 20N x6, 1N x4 Propellant: Launch: 1994; Orbit: GEO; Propellant load: N2H4 910 kg, NTO 825 kg; Thrusters: 1700N main engine, 50N x4 @ (variant 2) Propellant: Launch: 1996; Orbit: Launcher; Propellant load: N2H4 126 kg, NTO 120 kg; Thrusters: 3600N main engine @ (variant 3) Propellant: Launch: 1998; Orbit: GEO; Propellant load: N2H4 1030 kg, MON3 840 kg; Thrusters: 1700N main engine, 50N x4, 1N x16 @ (variant 4) Propellant: Launch: 2002; Orbit: GEO; Propellant load: N2H4 973 kg, MON3 641 kg; Thrusters: 500N LAE, 20N x8, 1N x16 @ (variant 5) Propellant: Launch: 2006; Orbit: GEO; Propellant load: MMH 1120 kg, MON3 1849 kg; Thrusters: 500N LAE, 22N x12 @ (variant 6) Propellant: Launch: 2007; Orbit: Lunar orbit; Propellant load: N2H4 960 kg, MON3 355 kg; Thrusters: 500N LAE, 20N x12, 1N x8 @ (variant 7) Propellant: Launch: 2007; Orbit: GEO; Propellant load: N2H4 1460 kg, MON3 1067 kg; Thrusters: 500N LAE, 20N x8, 4N x16 @ (variant 8) Propellant: Launch: 2009~2020; Orbit: ISS orbit; Propellant load: MMH 918 kg, MON3 1514 kg; Thrusters: 500N main engine x4, 120N x28 @ (variant 9) Propellant: Launch: 2025- (TBD); Orbit: ISS orbit; Propellant load: MMH 981 kg, MON3 1619 kg; Thrusters: 120N x24 @ (variant 10) Propellant: Launch: 2026 (TBD); Orbit: Martian moon; Propellant load: N2H4 916 kg, MON3 858 kg; Thrusters: 450N x4 @ (variant 11) Propellant: Launch: 2026 (TBD); Orbit: Martian moon; Propellant load: N2H4 607 kg, MON3 531 kg; Thrusters: 450N x2, 22N x20 @ (variant 12) Propellant: Launch: 1981; Propellant load: 64 kg; Thruster: 18N x2 @ (variant 13) Propellant: Launch: 1982; Propellant load: 18 kg; Thruster: 1N x12 @ (variant 14) Propellant: Launch: 1987; Propellant load: 18 kg; Thruster: 1N x14 @ (variant 15) Propellant: Launch: 1987; Propellant load: 113 kg; Thruster: 20N x2, 1N x16 @ (variant 16) Propellant: Launch: 1988; Propellant load: 118 kg; Thruster: 20N x4 @ (variant 17) Propellant: Launch: 1990; Propellant load: 14 kg; Thruster: 1N x14 @ (variant 18) Propellant: Launch: 1992; Propellant load: 115 kg; Thruster: 1N x22 @ (variant 19) Propellant: Launch: 1994; Propellant load: 115 kg; Thruster: 1N x16 @ (variant 20) Propellant: Launch: 1996-; Propellant load: 170 kg; Thruster: 20N x4, 1N x16 @ (variant 21) Propellant: Launch: 1997; Propellant load: 440 kg; Thruster: 20N x28, 1N x12 @ (variant 22) Propellant: Launch: 2002; Propellant load: 24 kg; Thruster: 1N x4 @ (variant 23) Propellant: Launch: 2005; Propellant load: 40 kg; Thruster: 1N x8 @ (variant 24) Propellant: Launch: 2006; Propellant load: 170 kg; Thruster: 4N x4, 1N x16 @ (variant 25) Propellant: Launch: 2008; Propellant load: 115 kg; Thruster: 20N x4, 1N x8 @ (variant 26) Propellant: Launch: 2012-; Propellant load: 260 kg; Thruster: 4N x12 @ (variant 27) Propellant: Launch: 2014-; Propellant load: 40 kg; Thruster: 4N x4 @ (variant 28) Propellant: Launch: 2024-; Propellant load: -; Thruster: 4N x8 @ (variant 29) Propellant: Propellant: Hydrazine/NTO; Thrust: 450 N; Isp: 326s; Inlet pressure: F >1.69 MPa, O >1.62 MPa; Demonstrated life: 32850s; Throughput: -; Status: Flight proven @ (variant 30) Propellant: Propellant: Hydrazine/NTO; Thrust: 21.5 N; Isp: 295s; Inlet pressure: 1.69 MPa; Demonstrated life: -; Throughput: 583 kg; Status: Flight proven @ (variant 31) Propellant: Propellant: MMH/MON3; Thrust: 478 N; Isp: 316s; Inlet pressure: 1.72 MPa; Demonstrated life: 15000s; Throughput: -; Status: Flight proven @ (variant 32) Propellant: Propellant: MMH/MON3; Thrust: 124.4 N; Isp: 274.9s; Inlet pressure: 2.05 MPa; Demonstrated life: 40000s; Throughput: 446 kg; Status: Flight proven @ (variant 33) Propellant: Thrust: 0.29-1.13N; Isp: 208-215s; Number of pulses: >850,000; Throughput: >100 kg; Status: Flight proven @ (variant 34) Propellant: Thrust: 1.80-5.01N; Isp: 212-225s; Number of pulses: >850,000; Throughput: >190 kg; Status: Flight proven @ (variant 35) Propellant: Thrust: 6.9-19.6N; Isp: 210-226s; Number of pulses: >261,914; Throughput: >115 kg; Status: Flight proven @ (variant 36) Propellant: Thrust: 24.5 N; Isp: >211s; Number of pulses: >7500; Throughput: >15 kg; Status: Qualified @ (variant 37) Propellant: Thrust: 23-50N; Isp: 215-225s; Number of pulses: >14,800; Throughput: >120 kg; Status: Flight proven @ (variant 38) Propellant: Thrust: 50 N; Isp: 225s; Number of pulses: >14,000; Throughput: >107 kg; Status: Flight proven @ (variant 39) Propellant: Size: 182 ID Sphere; Internal device: Diaphragm; Mount type: Boss; Status: Flight proven @ (variant 40) Propellant: Size: 420 ID Sphere; Internal device: Diaphragm; Mount type: 3 Tabs (Lugs); Status: Flight proven @ (variant 41) Propellant: Size: 420 ID Sphere; Internal device: Diaphragm; Mount type: Pedestal; Status: Flight proven @ (variant 42) Propellant: Size: 420 ID x750 length; Internal device: Diaphragm; Mount type: Pedestal; Status: Flight proven @ (variant 43) Propellant: Size: 420 ID x754 length; Internal device: Diaphragm; Mount type: 4 Tabs (Lugs); Status: Flight proven @ (variant 44) Propellant: Size: 570 ID x500 length; Internal device: Diaphragm; Mount type: 4 Tabs (Lugs); Status: Qualified @ (variant 45) Propellant: Size: 650 ID Sphere; Internal device: Diaphragm; Mount type: 3 Tabs (Lugs); Status: Flight proven @ (variant 46) Propellant: Size: 650 ID x750 length; Internal device: Diaphragm; Mount type: 3 Tabs (Lugs); Status: Qualified @ (variant 47) Propellant: Size: 820 ID x1087 length; Internal device: Channel mesh; Mount type: 4 Tabs (Lugs); Status: Flight proven @ (variant 48) Propellant: Size: 1020 ID Sphere; Internal device: Channel mesh; Mount type: 4 Tabs (Lugs); Status: Flight proven @ (variant 49) Propellant: Size: 1020 ID x1316 length; Internal device: Channel mesh; Mount type: 4 Tabs (Lugs); Status: Qualified @ (variant 50) Propellant: Diaphragm (SiO2-free diaphragm under development); Surface tension channel mesh @ (variant 51) ## Micro-A Thrusters — Micro Aerospace Solutions [propulsion] https://newspacemarket.com/products/mas-m100-micro-thruster/ Thrust: 5 mN Thrust: 100 mN @ (variant 2) Thrust: 500 mN @ (variant 3) Thrust: 1000 mN @ (variant 4) Thrust: 5 mN @ (variant 5) Thrust: 50 mN @ (variant 6) Thrust: 500 mN @ (variant 7) Thrust: 1000 mN @ (variant 8) Specific impulse: 100 Feed/tank pressure: 350000 bar Min impulse bit: 1.2 mN·s Power consumption: 0.5 W Specific impulse: 110 @ (variant 2) Feed/tank pressure: 350000 bar @ (variant 2) Min impulse bit: 9 mN·s @ (variant 2) Power consumption: 0.5 W @ (variant 2) Specific impulse: 120 @ (variant 3) Feed/tank pressure: 350000 bar @ (variant 3) Min impulse bit: 4 mN·s @ (variant 3) Power consumption: 1 W @ (variant 3) Specific impulse: 120 @ (variant 4) Feed/tank pressure: 350000 bar @ (variant 4) Min impulse bit: 8.5 mN·s @ (variant 4) Power consumption: 2 W @ (variant 4) Specific impulse: 150 @ (variant 5) Feed/tank pressure: 350000 bar @ (variant 5) Min impulse bit: 1.7 mN·s @ (variant 5) Power consumption: 0.5 W @ (variant 5) Specific impulse: 160 @ (variant 6) Feed/tank pressure: 350000 bar @ (variant 6) Min impulse bit: 6 mN·s @ (variant 6) Power consumption: 0.5 W @ (variant 6) Specific impulse: 170 @ (variant 7) Feed/tank pressure: 350000 bar @ (variant 7) Min impulse bit: 3 mN·s @ (variant 7) Power consumption: 1 W @ (variant 7) Specific impulse: 200 @ (variant 8) Feed/tank pressure: 350000 bar @ (variant 8) Min impulse bit: 3 mN·s @ (variant 8) ## 100 mN HPGP Thruster — Bradford Space [propulsion] https://newspacemarket.com/products/bradford-100mn-hpgp-thruster/ Thrust: 100 mN Specific impulse: 190 (min) Mass: 40 g Feed/tank pressure: 2.3-4.5 bar Power consumption: 6.3-8 W Propellant: LMP-103S (ADN-based, non-toxic) ## 1 N HPGP Thruster — Bradford Space [propulsion] https://newspacemarket.com/products/bradford-1n-hpgp-thruster/ Specific impulse: 204-231 Mass: 390 g Feed/tank pressure: 5.5-22 bar Power consumption: 12 W Propellant: LMP-103S (ADN-based, non-toxic) Thrust: 250-1000 mN ## 5 N HPGP Thruster — Bradford Space [propulsion] https://newspacemarket.com/products/bradford-5n-hpgp-thruster/ Thrust: 1400-5500 mN Specific impulse: 220-245 Mass: 450 g Feed/tank pressure: 5.5-24 bar Power consumption: 25-30 W Propellant: LMP-103S (ADN-based, non-toxic) ## 22 N HPGP Thruster — Bradford Space [propulsion] https://newspacemarket.com/products/bradford-22n-hpgp-thruster/ Specific impulse: 235-250 Mass: 1000 g Feed/tank pressure: 5.5-24 bar Power consumption: 36-50 W Propellant: LMP-103S (ADN-based, non-toxic) Thrust: 5500-22000 mN ## 200 N HPGP Thruster — Bradford Space [propulsion] https://newspacemarket.com/products/bradford-200n-hpgp-thruster/ Thrust: 50000-200000 mN Specific impulse: 206-234 Mass: 5700 g Feed/tank pressure: 5.5-24 bar Power consumption: 150-250 W Propellant: LMP-103S (ADN-based, non-toxic) ## 200 N HPGP RCS Thruster — Bradford Space [propulsion] https://newspacemarket.com/products/bradford-200n-hpgp-rcs-thruster/ Specific impulse: 206-234 Mass: 5700 g Feed/tank pressure: 5.5-24 bar Power consumption: 150-250 W Propellant: LMP-103S (ADN-based, non-toxic) Thrust: 50000-200000 mN ## 1 N GP Thruster — Bradford Space [propulsion] https://newspacemarket.com/products/bradford-1n-gp-thruster/ Thrust: 250-1000 mN Propellant: LMP-103S (ADN-based, non-toxic) ## Spacecraft Propulsion Systems — IHI Aerospace [propulsion] https://newspacemarket.com/products/ihi-mt-6-50n-thruster/ Propellant: Launch: cancelled; Orbit: Lunar orbit; Propellant Load: N2H4 143 kg, NTO 49 kg; Thrusters: 500N main engine, 20N x 6, 1N x 4 Propellant: Launch: 1994; Orbit: GEO; Propellant Load: N2H4 910 kg, NTO 825 kg; Thrusters: 1700N main engine, 50N x 4 @ (variant 2) Propellant: Launch: 1996; Orbit: Launcher; Propellant Load: N2H4 126 kg, NTO 120 kg; Thrusters: 3600N main engine @ (variant 3) Propellant: Launch: 1998; Orbit: GEO; Propellant Load: N2H4 1030 kg, MON3 840 kg; Thrusters: 1700N main engine, 50N x 4, 1N x 16 @ (variant 4) Propellant: Launch: 2002; Orbit: GEO; Propellant Load: N2H4 973 kg, MON3 641 kg; Thrusters: 500N LAE, 20N x 8, 1N x 16 @ (variant 5) Propellant: Launch: 2006; Orbit: GEO; Propellant Load: MMH 1120 kg, MON3 1849 kg; Thrusters: 500N LAE, 22N x 12 @ (variant 6) Propellant: Launch: 2007; Orbit: Lunar orbit; Propellant Load: N2H4 960 kg, MON3 355 kg; Thrusters: 500N LAE, 20N x 12, 1N x 8 @ (variant 7) Propellant: Launch: 2007; Orbit: GEO; Propellant Load: N2H4 1460 kg, MON3 1067 kg; Thrusters: 500N LAE, 20N x 8, 4N x 16 @ (variant 8) Propellant: Launch: 2009~2020; Orbit: ISS orbit; Propellant Load: MMH 918 kg, MON3 1514 kg; Thrusters: 500N main engine x 4, 120N x 28 @ (variant 9) Propellant: Launch: 2025- (TBD); Orbit: ISS orbit; Propellant Load: MMH 981 kg, MON3 1619 kg; Thrusters: 120N x 24 @ (variant 10) Propellant: Launch: 2026 (TBD); Orbit: Martian moon; Propellant Load: N2H4 916 kg, MON3 858 kg; Thrusters: 450N x 4 @ (variant 11) Propellant: Launch: 2026 (TBD); Orbit: Martian moon; Propellant Load: N2H4 607 kg, MON3 531 kg; Thrusters: 450N x 2, 22N x 20 @ (variant 12) Propellant: Launch: 1981; Propellant Load: 64 kg; Thruster: 18N x 2 @ (variant 13) Propellant: Launch: 1982; Propellant Load: 18 kg; Thruster: 1N x 12 @ (variant 14) Propellant: Launch: 1987; Propellant Load: 18 kg; Thruster: 1N x 14 @ (variant 15) Propellant: Launch: 1987; Propellant Load: 113 kg; Thruster: 20N x 2, 1N x 16 @ (variant 16) Propellant: Launch: 1988; Propellant Load: 118 kg; Thruster: 20N x 4 @ (variant 17) Propellant: Launch: 1990; Propellant Load: 14 kg; Thruster: 1N x 14 @ (variant 18) Propellant: Launch: 1992; Propellant Load: 115 kg; Thruster: 1N x 22 @ (variant 19) Propellant: Launch: 1994; Propellant Load: 115 kg; Thruster: 1N x 16 @ (variant 20) Propellant: Launch: 1996-; Propellant Load: 170 kg; Thruster: 20N x 4, 1N x 16 @ (variant 21) Propellant: Launch: 1997; Propellant Load: 440 kg; Thruster: 20N x 28, 1N x 12 @ (variant 22) Propellant: Launch: 2002; Propellant Load: 24 kg; Thruster: 1N x 4 @ (variant 23) Propellant: Launch: 2005; Propellant Load: 40 kg; Thruster: 1N x 8 @ (variant 24) Propellant: Launch: 2006; Propellant Load: 170 kg; Thruster: 4N x 4, 1N x 16 @ (variant 25) Propellant: Launch: 2008; Propellant Load: 115 kg; Thruster: 20N x 4, 1N x 8 @ (variant 26) Propellant: Launch: 2012-; Propellant Load: 260 kg; Thruster: 4N x 12 @ (variant 27) Propellant: Launch: 2014-; Propellant Load: 40 kg; Thruster: 4N x 4 @ (variant 28) Propellant: Launch: 2024-; Propellant Load: -; Thruster: 4N x 8 @ (variant 29) Propellant: Propellant: Hydrazine/NTO; Thrust: 450 N; Isp: 326s; Inlet pressure: F >1.69 MPa, O >1.62 MPa; Demonstrated life: 32850s; Throughput: -; Status: Flight proven @ (variant 30) Propellant: Propellant: Hydrazine/NTO; Thrust: 21.5 N; Isp: 295s; Inlet pressure: 1.69 MPa; Demonstrated life: -; Throughput: 583 kg; Status: Flight proven @ (variant 31) Propellant: Propellant: MMH/MON3; Thrust: 478 N; Isp: 316s; Inlet pressure: 1.72 MPa; Demonstrated life: 15000s; Throughput: -; Status: Flight proven @ (variant 32) Propellant: Propellant: MMH/MON3; Thrust: 124.4 N; Isp: 274.9s; Inlet pressure: 2.05 MPa; Demonstrated life: 40000s; Throughput: 446 kg; Status: Flight proven @ (variant 33) Propellant: Thrust: 0.29-1.13N; Isp: 208-215s; Number of pulses: >850,000; Throughput: >100 kg; Status: Flight proven @ (variant 34) Propellant: Thrust: 1.80-5.01N; Isp: 212-225s; Number of pulses: >850,000; Throughput: >190 kg; Status: Flight proven @ (variant 35) Propellant: Thrust: 6.9-19.6N; Isp: 210-226s; Number of pulses: >261,914; Throughput: >115 kg; Status: Flight proven @ (variant 36) Propellant: Thrust: 24.5 N; Isp: >211s; Number of pulses: >7500; Throughput: >15 kg; Status: Qualified @ (variant 37) Propellant: Thrust: 23-50N; Isp: 215-225s; Number of pulses: >14,800; Throughput: >120 kg; Status: Flight proven @ (variant 38) Propellant: Thrust: 50 N; Isp: 225s; Number of pulses: >14,000; Throughput: >107 kg; Status: Flight proven @ (variant 39) Propellant: Size: 182 ID Sphere; Internal device: Diaphragm; Mount type: Boss; Status: Flight proven @ (variant 40) Propellant: Size: 420 ID Sphere; Internal device: Diaphragm; Mount type: 3 Tabs (Lugs); Status: Flight proven @ (variant 41) Propellant: Size: 420 ID Sphere; Internal device: Diaphragm; Mount type: Pedestal; Status: Flight proven @ (variant 42) Propellant: Size: 420 ID x 750 length; Internal device: Diaphragm; Mount type: Pedestal; Status: Flight proven @ (variant 43) Propellant: Size: 420 ID x 754 length; Internal device: Diaphragm; Mount type: 4 Tabs (Lugs); Status: Flight proven @ (variant 44) Propellant: Size: 570 ID x 500 length; Internal device: Diaphragm; Mount type: 4 Tabs (Lugs); Status: Qualified @ (variant 45) Propellant: Size: 650 ID Sphere; Internal device: Diaphragm; Mount type: 3 Tabs (Lugs); Status: Flight proven @ (variant 46) Propellant: Size: 650 ID x 750 length; Internal device: Diaphragm; Mount type: 3 Tabs (Lugs); Status: Qualified @ (variant 47) Propellant: Size: 820 ID x 1087 length; Internal device: Channel mesh; Mount type: 4 Tabs (Lugs); Status: Flight proven @ (variant 48) Propellant: Size: 1020 ID Sphere; Internal device: Channel mesh; Mount type: 4 Tabs (Lugs); Status: Flight proven @ (variant 49) Propellant: Size: 1020 ID x 1316 length; Internal device: Channel mesh; Mount type: 4 Tabs (Lugs); Status: Qualified @ (variant 50) Propellant: Diaphragm (SiO2-free diaphragm under development); Surface tension channel mesh @ (variant 51) ## IHI Aerospace Spacecraft Propulsion Products — IHI Aerospace [propulsion] https://newspacemarket.com/products/ihi-mt-6a-50n-thruster/ Propellant: Launch Year: cancelled; Orbit: Lunar orbit; Propellant Load: N2H4 143 kg, NTO 49 kg; Thruster Configuration: 500N main engine, 20N x6, 1N x4 Propellant: Launch Year: 1994; Orbit: GEO; Propellant Load: N2H4 910 kg, NTO 825 kg; Thruster Configuration: 1700N main engine, 50N x4 @ (variant 2) Propellant: Launch Year: 1996; Orbit: Launcher; Propellant Load: N2H4 126 kg, NTO 120 kg; Thruster Configuration: 3600N main engine @ (variant 3) Propellant: Launch Year: 1998; Orbit: GEO; Propellant Load: N2H4 1030 kg, MON3 840 kg; Thruster Configuration: 1700N main engine, 50N x4, 1N x16 @ (variant 4) Propellant: Launch Year: 2002; Orbit: GEO; Propellant Load: N2H4 973 kg, MON3 641 kg; Thruster Configuration: 500N LAE, 20N x8, 1N x16 @ (variant 5) Propellant: Launch Year: 2006; Orbit: GEO; Propellant Load: MMH 1120 kg, MON3 1849 kg; Thruster Configuration: 500N LAE, 22N x12 @ (variant 6) Propellant: Launch Year: 2007; Orbit: Lunar orbit; Propellant Load: N2H4 960 kg, MON3 355 kg; Thruster Configuration: 500N LAE, 20N x12, 1N x8 @ (variant 7) Propellant: Launch Year: 2007; Orbit: GEO; Propellant Load: N2H4 1460 kg, MON3 1067 kg; Thruster Configuration: 500N LAE, 20N x8, 4N x16 @ (variant 8) Propellant: Launch Year: 2009-2020; Orbit: ISS orbit; Propellant Load: MMH 918 kg, MON3 1514 kg; Thruster Configuration: 500N main engine x4, 120N x28 @ (variant 9) Propellant: Launch Year: 2025- (TBD); Orbit: ISS orbit; Propellant Load: MMH 981 kg, MON3 1619 kg; Thruster Configuration: 120N x24 @ (variant 10) Propellant: Launch Year: 2026 (TBD); Orbit: Martian moon; Propellant Load: N2H4 916 kg, MON3 858 kg; Thruster Configuration: 450N x4 @ (variant 11) Propellant: Launch Year: 2026 (TBD); Orbit: Martian moon; Propellant Load: N2H4 607 kg, MON3 531 kg; Thruster Configuration: 450N x2, 22N x20 @ (variant 12) Propellant: Launch Year: 1981; Propellant Load: 64 kg; Thruster: 18N x2 @ (variant 13) Propellant: Launch Year: 1982; Propellant Load: 18 kg; Thruster: 1N x12 @ (variant 14) Propellant: Launch Year: 1987; Propellant Load: 18 kg; Thruster: 1N x14 @ (variant 15) Propellant: Launch Year: 1987; Propellant Load: 113 kg; Thruster: 20N x2, 1N x16 @ (variant 16) Propellant: Launch Year: 1988; Propellant Load: 118 kg; Thruster: 20N x4 @ (variant 17) Propellant: Launch Year: 1990; Propellant Load: 14 kg; Thruster: 1N x14 @ (variant 18) Propellant: Launch Year: 1992; Propellant Load: 115 kg; Thruster: 1N x22 @ (variant 19) Propellant: Launch Year: 1994; Propellant Load: 115 kg; Thruster: 1N x16 @ (variant 20) Propellant: Launch Year: 1996-; Propellant Load: 170 kg; Thruster: 20N x4, 1N x16 @ (variant 21) Propellant: Launch Year: 1997; Propellant Load: 440 kg; Thruster: 20N x28, 1N x12 @ (variant 22) Propellant: Launch Year: 2002; Propellant Load: 24 kg; Thruster: 1N x4 @ (variant 23) Propellant: Launch Year: 2005; Propellant Load: 40 kg; Thruster: 1N x8 @ (variant 24) Propellant: Launch Year: 2006; Propellant Load: 170 kg; Thruster: 4N x4, 1N x16 @ (variant 25) Propellant: Launch Year: 2008; Propellant Load: 115 kg; Thruster: 20N x4, 1N x8 @ (variant 26) Propellant: Launch Year: 2012-; Propellant Load: 260 kg; Thruster: 4N x12 @ (variant 27) Propellant: Launch Year: 2014-; Propellant Load: 40 kg; Thruster: 4N x4 @ (variant 28) Propellant: Launch Year: 2024-; Propellant Load: -; Thruster: 4N x8 @ (variant 29) Propellant: Propellant: Hydrazine/NTO; Thrust: 450 N; Isp: 326s; Inlet pressure: F >1.69 MPa, O >1.62 MPa; Demonstrated life: 32850s; Status: Flight proven @ (variant 30) Propellant: Propellant: Hydrazine/NTO; Thrust: 21.5 N; Isp: 295s; Inlet pressure: 1.69 MPa; Throughput: 583 kg; Status: Flight proven @ (variant 31) Propellant: Propellant: MMH/MON3; Thrust: 478 N; Isp: 316s; Inlet pressure: 1.72 MPa; Demonstrated life: 15000s; Status: Flight proven @ (variant 32) Propellant: Propellant: MMH/MON3; Thrust: 124.4 N; Isp: 274.9s; Inlet pressure: 2.05 MPa; Demonstrated life: 40000s; Throughput: 446 kg; Status: Flight proven @ (variant 33) Propellant: Thrust: 0.29-1.13N; Isp: 208-215s; Number of pulses: >850,000; Throughput: >100 kg; Status: Flight proven @ (variant 34) Propellant: Thrust: 1.80-5.01N; Isp: 212-225s; Number of pulses: >850,000; Throughput: >190 kg; Status: Flight proven @ (variant 35) Propellant: Thrust: 6.9-19.6N; Isp: 210-226s; Number of pulses: >261,914; Throughput: >115 kg; Status: Flight proven @ (variant 36) Propellant: Thrust: 24.5 N; Isp: >211s; Number of pulses: >7500; Throughput: >15 kg; Status: Qualified @ (variant 37) Propellant: Thrust: 23-50N; Isp: 215-225s; Number of pulses: >14,800; Throughput: >120 kg; Status: Flight proven @ (variant 38) Propellant: Thrust: 50 N; Isp: 225s; Number of pulses: >14,000; Throughput: >107 kg; Status: Flight proven @ (variant 39) Propellant: Volume: 3L; Size: 182 ID Sphere; Internal device: Diaphragm; Mount type: Boss; Status: Flight proven @ (variant 40) Propellant: Volume: 37L; Size: 420 ID Sphere; Internal device: Diaphragm; Mount type: 3 Tabs (Lugs); Status: Flight proven @ (variant 41) Propellant: Volume: 37L; Size: 420 ID Sphere; Internal device: Diaphragm; Mount type: Pedestal; Status: Flight proven @ (variant 42) Propellant: Volume: 67L; Size: 420 ID x 750 length mm; Internal device: Diaphragm; Mount type: Pedestal; Status: Flight proven @ (variant 43) Propellant: Volume: 74L; Size: 420 ID x 754 length mm; Internal device: Diaphragm; Mount type: 4 Tabs (Lugs); Status: Flight proven @ (variant 44) Propellant: Volume: 74L; Size: 570 ID x 500 length mm; Internal device: Diaphragm; Mount type: 4 Tabs (Lugs); Status: Qualified @ (variant 45) Propellant: Volume: 141L; Size: 650 ID Sphere; Internal device: Diaphragm; Mount type: 3 Tabs (Lugs); Status: Flight proven @ (variant 46) Propellant: Volume: 169L; Size: 650 ID x 750 length mm; Internal device: Diaphragm; Mount type: 3 Tabs (Lugs); Status: Qualified @ (variant 47) Propellant: Volume: 427L; Size: 820 ID x 1087 length mm; Internal device: Channel mesh; Mount type: 4 Tabs (Lugs); Status: Flight proven @ (variant 48) Propellant: Volume: 552L; Size: 1020 ID Sphere; Internal device: Channel mesh; Mount type: 4 Tabs (Lugs); Status: Flight proven @ (variant 49) Propellant: Volume: 726L; Size: 1020 ID x 1316 length mm; Internal device: Channel mesh; Mount type: 4 Tabs (Lugs); Status: Qualified @ (variant 50) ## Propulsion Products and Services — Northrop Grumman Space Systems [propulsion] https://newspacemarket.com/products/ngc-mre-thruster-family/ Propellant: Hydrazine ## Astrobrake — Gama Space [propulsion] https://newspacemarket.com/products/gama-astrobrake/ Mass: 900 g Envelope (L×W×H): 0.75 U Design lifetime: 10 years ## MICRO Dragsail — Frond Space Systems [propulsion] https://newspacemarket.com/products/frond-micro-dragsail/ Mass: 2000 g (max) Mass: 50000-200000 g Operating temperature: -30 °C Supply voltage: 8-12 ## Genergo Propellant-Free Electromagnetic Propulsion System — Genergo [propulsion] https://newspacemarket.com/products/genergo-propellant-free-propulsion/ Propellant: None — propellantless electromagnetic system TRL: 7-8 ## DXP Electrospray Thruster — DeltaX Propulsion [propulsion] https://newspacemarket.com/products/dxp-electrospray-thruster/ Propellant: Ionic liquid ## PBI Water Ion Thruster — Pale Blue [propulsion] https://newspacemarket.com/products/pale-blue-pbi-water-ion-thruster/ Power consumption: 60 W (max) Total impulse: 7000 N·s (min) Mass: 1600 g (max) Envelope (L×W×H): 1U+ Propellant: Water (no high-pressure storage required) Thrust: 0.35 mN (min) ## PBR-10 — Pale Blue [propulsion] https://newspacemarket.com/products/pale-blue-pbr-10/ Power consumption: 6 W Total impulse: 55 N·s (min) Mass: 575 g (max) Envelope (L×W×H): 0.5U Thrust: 1 mN ## PBR-20 — Pale Blue [propulsion] https://newspacemarket.com/products/pale-blue-pbr-20/ Power consumption: 20 W Total impulse: 220 N·s (min) Mass: 1500 g (max) Envelope (L×W×H): 1U Thrust: 1 mN ## PBR-30 — Pale Blue [propulsion] https://newspacemarket.com/products/pale-blue-pbr-30/ Power consumption: 10-35 W Total impulse: 400 N·s (min) Mass: 2100 g (max) Envelope (L×W×H): 2U Thrust: 3-12 mN ## PBR-50 — Pale Blue [propulsion] https://newspacemarket.com/products/pale-blue-pbr-50/ Power consumption: 50 W Total impulse: 4400 N·s Mass: 13400 g Envelope (L×W×H): Φ250 x 300 mm Thrust: 10 mN ## PBH-100 Hall Effect Thruster — Pale Blue [propulsion] https://newspacemarket.com/products/pale-blue-pbh-100/ Power consumption: 110-180 W Total impulse: 50000 N·s (min) Mass: 10000 g (max) Envelope (L×W×H): 300 × 300 × 150 mm Propellant: Water (no high-pressure storage required) Thrust: 5-8 mN ## Water Hall-effect Thruster — Pale Blue [propulsion] https://newspacemarket.com/products/pale-blue-water-hall-thruster/ Power consumption: 600 W Total impulse: 180000 N·s Mass: 45000 g (max) Envelope (L×W×H): 350 × 350 × 600 mm Propellant: Water (no high-pressure storage required) Thrust: 10 mN ## H2O2/HTPB Hybrid Upper Stage — Parabilis Space Technologies [propulsion] https://newspacemarket.com/products/parabilis-h2o2-htpb-hybrid-upper-stage/ Propellant: H2O2 (hydrogen peroxide) / HTPB ## LOx/Methane RCS Thruster — Parabilis Space Technologies [propulsion] https://newspacemarket.com/products/parabilis-lox-methane-rcs-thruster/ Propellant: LOx (liquid oxygen) / CH4 (methane) ## Aurora Hall-effect Propulsion System — Orbion Space Technology [propulsion] https://newspacemarket.com/products/orbion-aurora-hall-effect-propulsion-system/ Specific impulse: 1400 Propellant: Xenon or Krypton Envelope (L×W×H): 26.8 × 19.6 × 9.7 cm, 5.8 kg Envelope (L×W×H): 16.0 × 8.8 × 1.6 cm, 700 g @ (variant 2) Thrust: 60 mN (min) ## STAR-Water-nano — Water Resistojet for Nanosatellites — OhmSpace [propulsion] https://newspacemarket.com/products/ohmspace-star-water-nano-resistojet/ Specific impulse: 200 (min) Propellant: Water Propellant: From 250 g @ (variant 2) Radiation tolerance (TID): 5 krad ## STAR-Water-micro — Water Resistojet for Microsatellites — OhmSpace [propulsion] https://newspacemarket.com/products/ohmspace-star-water-micro-resistojet/ Specific impulse: 240 Propellant: Water (deionized/demineralized) Thrust: 75-150 mN ## STAR-X — Xenon Resistojet for GEO Reaction Control — OhmSpace [propulsion] https://newspacemarket.com/products/ohmspace-star-x-xenon-resistojet-geo/ Specific impulse: 80-100 Propellant: Xenon (Krypton as alternative) Thrust: 1000-2000 mN ## ALEXIUS Water-Electrolysis Propulsion System — MIPRONS [propulsion] https://newspacemarket.com/products/miprons-alexius-propulsion/ Feed/tank pressure: 30 bar Specific impulse: 300-320 TRL: 7 ## GP-LAM Liquid Apogee Module — Manastu Space [propulsion] https://newspacemarket.com/products/manastu-gp-lam-liquid-apogee-module/ Specific impulse: 250 Total impulse: 150000 N·s Supply voltage: 24 Propellant: MS289 (hydrogen peroxide-alcohol) Mass: 1100 g Operating temperature: -50 °C Thrust: 300000 mN ## I-Booster Green Propulsion System — Manastu Space [propulsion] https://newspacemarket.com/products/manastu-i-booster-propulsion/ Mass: 100000-500000 g Total impulse: 20000 N·s Supply voltage: 28 Propellant: MS289 (hydrogen peroxide based) Mass: 11000 g Envelope (L×W×H): 350 x 450 mm Operating temperature: -10 °C Thrust: 500 mN ## GP-LAM — Manastu Space [propulsion] https://newspacemarket.com/products/manastu-sharanga-micropropulsion/ Propulsion type: 300 Propellant: non-toxic MS289 green propellant Total impulse: 80000 N·s Thrust: 300000 mN Thrust: 300000 mN @ (variant 2) ## I-Booster — Manastu Space [propulsion] https://newspacemarket.com/products/manastu-vyom-2u-propulsion/ Total impulse: 20000 N·s Mass: 100000-500000 g ## L.Garde Solar Sails — L.Garde Inc [propulsion] https://newspacemarket.com/products/lgarde-solar-sails/ Envelope (L×W×H): 83 sq m and 318 sq m ## BOOSTER — Liftero [propulsion] https://newspacemarket.com/products/liftero-booster-propulsion/ Propellant: N₂O + C₂H6 (self-pressurizing, green chemical propellant) Flight heritage: RED5 mission, launched on SpaceX Transporter-13, March 2025 — first Polish propulsion system in orbit ## DARUMA Micro Hybrid Propulsion Unit — Letara [propulsion] https://newspacemarket.com/products/letara-daruma-micro-propulsion/ Mass: 30000 g Propellant: HDPE (high-density polyethylene) ## Air-Breathing Electric Propulsion (ABEP) Thruster — Kreios Space [propulsion] https://newspacemarket.com/products/kreios-abep-thruster/ Design lifetime: 7 years (min) Propellant: None required — ingests atmospheric gas ## GITA | Green Impulse Transmitter — Inspecity Space Laboratories [propulsion] https://newspacemarket.com/products/inspecity-rama-robotic-arm/ Propellant: Refuellable, easy to source ## Pulsed Plasma Rocket (PPR) — Howe Industries [propulsion] https://newspacemarket.com/products/howe-pulsed-plasma-rocket/ Specific impulse: 5000 Power consumption: 282 W Mass: 80000000 g Thrust: 100000000 mN ## GATE Jetpack S — GATE Space [propulsion] https://newspacemarket.com/products/gatespace-jetpack-propulsion/ Total impulse: 36000 N·s Lead time: 9 Propellant: C2H6 and N2O Specific impulse: 270 Mass: 36000 g Envelope (L×W×H): 525 × 525 × 380 mm Mass: 100000 g @ (variant 2) Envelope (L×W×H): 600 × 600 × 600 mm @ (variant 2) ## ATOM Monopropellant Thruster — DREAM Aerospace [propulsion] https://newspacemarket.com/products/dreamaerospace-atom-thruster/ Propellant: Eco-friendly, nontoxic monopropellant ## MPUC Monopropellant Propulsion Unit for CubeSats — CU Aerospace [propulsion] https://newspacemarket.com/products/cuaerospace-mpuc-propulsion/ Propellant: CMP-X (ethanol/hydrogen peroxide) Total impulse: 2000 N·s (min) ## CHIPS CubeSat High Impulse Propulsion System — CU Aerospace [propulsion] https://newspacemarket.com/products/cuaerospace-chips-propulsion/ Propellant: R236fa and R134a (range-safety approved) Envelope (L×W×H): 0.54U Total impulse: 180 N·s Envelope (L×W×H): As small as 0.3U @ (variant 2) ## FPPT Fiber-Fed Pulsed Plasma Thruster — CU Aerospace [propulsion] https://newspacemarket.com/products/cuaerospace-fppt-plasma-thruster/ Specific impulse: 3500 (min) Total impulse: 25000 N·s (min) Envelope (L×W×H): 0.7L to 53L Total impulse: 1000-600000 N·s Propellant: PTFE (Teflon) fiber ## GO-2 Electric Propulsion System — Morpheus Space [propulsion] https://newspacemarket.com/products/morpheus-go2-feep-propulsion/ Total impulse: 12400 N·s Power consumption: 7 W Envelope (L×W×H): Approximately 1U modular unit Propellant: Solid metallic propellant; zero leakage, no moving parts, chemicals or pressurization Flight heritage: Core technology in orbit since 2018; commercial customer missions since 2023 ## Maxwell Block 3 RF Plasma Thruster — Phase Four [propulsion] https://newspacemarket.com/products/phasefour-maxwell-block3-thruster/ Mass: 5900 g Mass: 8400 g @ (variant 2) Envelope (L×W×H): 19 × 13.5 × 19 cm Power at thrust: 300-500 W Supply voltage: 22-34 Specific impulse: 600-1300 Propellant: Xe, Kr, ASCENT, Hydrazine Power consumption: 300-500 W Thrust: 8-18 mN ## ThrustMe In-Space Propulsion Solutions — ThrustMe [propulsion] https://newspacemarket.com/products/thrustme-jpt150-hall-thruster/ Flight heritage: World’s first in-orbit demonstration of iodine-fuelled electric propulsion systems in 2019 and 2020; successfully tested the first iodine-fuelled electric propulsion system in space aboard the Beihangkongshi-1 satellite in January 2021. ## Passive Gas Thruster System (PGTS) — ThrustMe [propulsion] https://newspacemarket.com/products/thrustme-pgts-cold-gas-system/ Propellant: R134a (tetrafluoroethane) ## Aurora ARM Thruster System — Aurora Propulsion Technologies [propulsion] https://newspacemarket.com/products/aurora-mepe-pulsed-plasma-thruster/ Flight heritage: 4 Years Envelope (L×W×H): Smallest CubeSats up to 300 kg small sats Propellant: Unpressurised water (no hazmat logistics) ## Propulsion systems for maneuvers in space — Aurora Propulsion Technologies [propulsion] https://newspacemarket.com/products/aurora-wr10-water-resistojet/ Flight heritage: 4 Years ## FPPT — Fiber-Fed Pulsed Plasma Thruster — CU Aerospace [propulsion] https://newspacemarket.com/products/cua-fppt/ Specific impulse: 3500 (min) Total impulse: 25000 N·s (min) Envelope (L×W×H): 0.7 L to 53 L (1U to ESPA-class) Propellant: PTFE (Teflon®) fiber; solid, inert, no pressure vessel required ## ATOM — DREAM Aerospace [propulsion] https://newspacemarket.com/products/dream-aerospace-atom-thruster/ Propellant: Green monopropellant (nontoxic) Thrust: 1000 mN ## Iris Propulsion Module / Propulsion Kit — ExoTerra Resource [propulsion] https://newspacemarket.com/products/exoterra-iris-propulsion-module/ Radiation tolerance (TID): 30 krad Propellant: Xenon or Krypton ## REGULUS Electric Propulsion — T4i – Technology for Propulsion and Innovation [propulsion] https://newspacemarket.com/products/t4i-regulus-electric-propulsion/ Propellant: Iodine (I2) Envelope (L×W×H): 93.8 x 95.0 x 151.0-200.0 mm (REGULUS-50-I2 variants); 120.0 x 120.0 x 270.0-343.5 mm (REGULUS-150-I2) ## IANUS & PERSEUS Cold Gas Propulsion Systems — T4i – Technology for Propulsion and Innovation [propulsion] https://newspacemarket.com/products/t4i-ianus-perseus-cold-gas/ Propellant: R134a Mass: 2500 g Supply voltage: 12 Specific impulse: 40 (min) Total impulse: 450 N·s Min impulse bit: 0.5 mN·s (max) TRL: 9 Propellant: R134a @ (variant 2) Specific impulse: 40 (min) @ (variant 2) Total impulse: 38 N·s @ (variant 2) Min impulse bit: 0.5 mN·s (max) @ (variant 2) TRL: 8 @ (variant 2) ## ALPHARD Monopropellant Family — T4i – Technology for Propulsion and Innovation [propulsion] https://newspacemarket.com/products/t4i-alphard-monopropellant/ Propellant: HTP 90 w% (customizable up to 95 w%) Feed/tank pressure: 10-28 bar Feed/tank pressure: 10-50 bar @ (variant 2) Feed/tank pressure: 10-28 bar @ (variant 3) Feed/tank pressure: 10-50 bar @ (variant 4) Feed/tank pressure: 10-27 bar @ (variant 5) Feed/tank pressure: 28 bar Feed/tank pressure: 50 bar @ (variant 2) Feed/tank pressure: 28 bar @ (variant 3) Feed/tank pressure: 50 bar @ (variant 4) Feed/tank pressure: 27 bar @ (variant 5) Specific impulse: 160 Specific impulse: 160 @ (variant 2) Specific impulse: 160 @ (variant 3) Specific impulse: 160 @ (variant 4) Specific impulse: 160 @ (variant 5) Min impulse bit: 0.1-0.22 mN·s Min impulse bit: 0.1-0.33 mN·s @ (variant 2) Min impulse bit: 0.15-0.34 mN·s @ (variant 3) Min impulse bit: 0.15-0.51 mN·s @ (variant 4) Min impulse bit: 6.8-25 mN·s @ (variant 5) Total impulse: 56505 N·s Total impulse: 56505 N·s @ (variant 2) Total impulse: 113011 N·s @ (variant 3) Total impulse: 113011 N·s @ (variant 4) Total impulse: 100000 N·s @ (variant 5) Propellant: HTP 90 w% (customizable up to 95 w%) @ (variant 2) Feed/tank pressure: 10-28 bar @ (variant 6) Feed/tank pressure: 28 bar @ (variant 6) Specific impulse: 160 @ (variant 6) Min impulse bit: 0.1-0.22 mN·s @ (variant 6) Mass: 332 g Total impulse: 56505.6 N·s @ (variant 6) Propellant: HTP 90 w% (customizable up to 95 w%) @ (variant 3) Thrust: 5300-12700 mN Thrust: 5300-19700 mN @ (variant 2) Thrust: 10000-22600 mN @ (variant 3) Thrust: 10000-34000 mN @ (variant 4) Thrust: 100000-230000 mN @ (variant 5) Thrust: 10000 mN Thrust: 5300-12700 mN @ (variant 6) Thrust: 10000 mN @ (variant 2) ## GATE Jetpack M — GATE Space [propulsion] https://newspacemarket.com/products/gate-space-jetpack-m/ Total impulse: 80000 N·s Lead time: 9 Propellant: C2H6 and N2O Specific impulse: 270 Mass: 80000 g Envelope (L×W×H): 800 × 800 × 400 mm Mass: 100000 g @ (variant 2) Envelope (L×W×H): 690 × 690 × 690 mm @ (variant 2) ## GATE Jetpack L — GATE Space [propulsion] https://newspacemarket.com/products/gate-space-jetpack-l/ Total impulse: 140000 N·s Lead time: 9 Propellant: C2H6 and N2O Specific impulse: 270 Mass: 105000 g Envelope (L×W×H): 900 × 900 × 400 mm Mass: 200000 g @ (variant 2) Envelope (L×W×H): 990 × 990 × 990 mm @ (variant 2) ## GATE Thruster S — GATE Space [propulsion] https://newspacemarket.com/products/gate-space-thruster-s/ Lead time: 9-12 Min impulse bit: 200 mN·s Propellant: C2H6 and N2O Specific impulse: 270 Feed/tank pressure: 15 bar Operating temperature: -20 °C Thrust: 2000-20000 mN ## GATE Jetpack — GATE Space [propulsion] https://newspacemarket.com/products/gate-space-thruster-m/ Total impulse: 36000 N·s Lead time: 9 Propellant: C2H6 and N2O Specific impulse: 270 Mass: 36000 g Envelope (L×W×H): 525 × 525 × 380 mm Mass: 100000 g @ (variant 2) Envelope (L×W×H): 600 × 600 × 600 mm @ (variant 2) Envelope (L×W×H): 15 inch @ (variant 3) Total impulse: 80000 N·s @ (variant 2) Lead time: 9 @ (variant 2) Propellant: C2H6 and N2O @ (variant 2) Specific impulse: 270 @ (variant 2) Mass: 80000 g @ (variant 3) Envelope (L×W×H): 800 × 800 × 400 mm @ (variant 4) Mass: 100000 g @ (variant 4) Envelope (L×W×H): 690 × 690 × 690 mm @ (variant 5) Envelope (L×W×H): 15 or 24 inch @ (variant 6) Total impulse: 140000 N·s @ (variant 3) Lead time: 9 @ (variant 3) Propellant: C2H6 and N2O @ (variant 3) Specific impulse: 270 @ (variant 3) Mass: 105000 g @ (variant 5) Envelope (L×W×H): 900 × 900 × 400 mm @ (variant 7) Mass: 200000 g @ (variant 6) Envelope (L×W×H): 990 × 990 × 990 mm @ (variant 8) Envelope (L×W×H): 24 inch @ (variant 9) ## GATE Thruster L — GATE Space [propulsion] https://newspacemarket.com/products/gate-space-thruster-l/ Lead time: 9-12 Min impulse bit: 2000 mN·s Propellant: C2H6 and N2O Specific impulse: 270 Feed/tank pressure: 15 bar Operating temperature: -20 °C Thrust: 20000-200000 mN ## Jinwu Electric Propulsion System — Hongqing Technology (鸿擎科技) [propulsion] https://newspacemarket.com/products/hongqing-jinwu-electric-propulsion-system/ Propellant: Argon (Ar) Feed/tank pressure: 300 bar (min) Feed/tank pressure: 30 bar (max) Mass: 500 g ## ThermaSat — Howe Industries [propulsion] https://newspacemarket.com/products/howe-thermasat/ Propellant: Water (H2O) Power consumption: 8 W Propellant: Solid or liquid (ambient pressure) @ (variant 2) ## SEPTIR — Howe Industries [propulsion] https://newspacemarket.com/products/howe-septir/ Specific impulse: 3048 Power consumption: 3 W Mass: 10000 g Thrust: 0.295 mN ## SPRINTR — Howe Industries [propulsion] https://newspacemarket.com/products/howe-sprintr/ Specific impulse: 843 Power consumption: 40 W Mass: 2730000 g Propellant: Liquid hydrogen Thrust: 9930000 mN ## IVO Quantum Drive — IVO Limited [propulsion] https://newspacemarket.com/products/ivo-quantum-drive/ Power consumption: 1 W Propellant: None (zero fuel) Operating temperature: -100 °C Thrust: 45-52 mN ## HyNOx 4U CubeSat Propulsion Module — ISPTech [propulsion] https://newspacemarket.com/products/isptech-hynox-200-thruster/ Envelope (L×W×H): 4U (209.3×209.3×110.0 mm³) Envelope (L×W×H): Z-length adjustable. @ (variant 2) Lead time: 6 ## HyNOx Propulsion Systems — ISPTech [propulsion] https://newspacemarket.com/products/isptech-cold-gas-propulsion-module-1u/ Propellant: Liquid or gaseous, depending on mission requirements. ## HIP_11 Propulsion System — ISPTech [propulsion] https://newspacemarket.com/products/isptech-hip-11-propulsion-system/ Propellant: H2O2 (hydrogen peroxide) + ionic liquid fuel Propellant: Up to 1,440 kg/m3 @ (variant 2) Propellant: Up to 1,100 kg/m3 @ (variant 3) Thrust: 20000 mN ## Deorbit Drag Device (D3) — Orbotic Systems [propulsion] https://newspacemarket.com/products/d3-deorbit-drag-device/ Envelope (L×W×H): 10 cm x 10 cm x 5.9 cm (under 1U cubic form factor) Flight heritage: Successfully deployed in September 2022 from the International Space Station ## Autonomous Deorbit Device (E.T.PACK-F) — PERSEI Space [propulsion] https://newspacemarket.com/products/persei-space-deorbit-device/ Mass: 20000 g ## Green Mobility Module (GMM) — PERSEI Space [propulsion] https://newspacemarket.com/products/persei-space-green-mobility-module/ Mass: 5000 g ## H2/O2 Aerospike Thruster — SecondStar [propulsion] https://newspacemarket.com/products/secondstar-h2o2-aerospike-thruster/ Propellant: H2/O2 (from water electrolysis) ## Space Nuclear Power (RTG and Nuclear Electric) — CNNC Space (China National Nuclear Corp Space) [propulsion] https://newspacemarket.com/products/cnnc-space-nuclear-power/ Flight heritage: RHU units on Chang'e-4 and Chang'e-5 lunar missions ## Herik Labs HL-1 Green Hydrogen Rocket Engine — Herik Labs [propulsion] https://newspacemarket.com/products/herik-labs-space-tech-development/ Propellant: Green hydrogen ## ND-50 Neumann Drive — Pulsed Cathodic Arc Thruster — Neumann Space [propulsion] https://newspacemarket.com/products/neumann-space-electric-propulsion-thruster/ Power consumption: 50 W Mass: 1400 g Envelope (L×W×H): 100 × 96 × 96 mm Propellant: Solid metal rod — molybdenum (flight-standard); also Mg, Ti, V, Al, C Propellant: No gas tanks, no pressure vessels, long shelf life; can use orbital debris as propellant @ (variant 2) Flight heritage: SpIRIT (2023), EDISON/ESA Pioneer (2025), SSTL CarbSAR (2025) ## Orbital Arc Thruster and PPU — Orbital Arc [propulsion] https://newspacemarket.com/products/orbital-arc-mission-software/ Power consumption: 2 W Power consumption: 3250 W @ (variant 2) ## Sunbird — Nuclear Fusion Propulsion System — Pulsar Fusion [propulsion] https://newspacemarket.com/products/pulsar-fusion-nuclear-propulsion-engine/ Propellant: Deuterium + Helium-3 (DDFD — Dual Direct Fusion Drive) Specific impulse: 10000-15000 Envelope (L×W×H): ~9.8 × 3.5 × 3.5 m ## GEM (Green Electric Monopropellant) — Digital Solid State Propulsion [propulsion] https://newspacemarket.com/products/dssp-gem-green-electric-monopropellant-2/ Feed/tank pressure: 5-24 bar ## BE-4 Engine — Blue Origin [propulsion] https://newspacemarket.com/products/blueorigin-be-4-engine/ Propellant: LOX / LNG (liquefied natural gas) ## BE-7 Engine — Blue Origin [propulsion] https://newspacemarket.com/products/blueorigin-be-7-engine/ Specific impulse: 460 Propellant: Liquid hydrogen / Liquid oxygen (LH₂/LOX) Thrust: 44000000 mN ## Aquila Engine — Isar Aerospace [propulsion] https://newspacemarket.com/products/isar-aerospace-aquila/ Propellant: LOX/Propane (LPG) Propellant: Turbopump-fed @ (variant 2) ## SpaceVan Electric Propulsion Transfer System — Exotrail [propulsion] https://newspacemarket.com/products/exotrail-spacevan/ Power consumption: 300 W (max) ## Prometheus Reusable Rocket Engine — arianegroup [propulsion] https://newspacemarket.com/products/arianegroup-prometheus/ Propellant: LOX/Liquid Methane (LCH4) ## Maxwell RF Ion Thruster — Phase Four [propulsion] https://newspacemarket.com/products/phase-four-maxwell/ Propellant: Xenon or Krypton (inert gas) Specific impulse: 700-1500 Power consumption: 20-200 W Thrust: 1-10 mN ## NanoTILE CubeSat Propulsion Module — Accion Systems [propulsion] https://newspacemarket.com/products/accion-systems-nanotile/ Specific impulse: 800-1500 Power consumption: 0.5-3 W Propellant: Solid ionic liquid chip (no pressurized gas) Thrust: 0.01-0.1 mN ## Navier LOX/Methane Engine — Latitude [propulsion] https://newspacemarket.com/products/latitude-navier/ Propellant: LOX/Liquid Methane Flight heritage: Same cycle as Russian RD-180/RD-170 (adapted for methane) ## nμpro Electrospray Thruster — Morpheus Space [propulsion] https://newspacemarket.com/products/morpheus-space-nupro/ Specific impulse: 1500-3000 ## Prometheus-1 Small Liquid Rocket Engine — Promin Aerospace [propulsion] https://newspacemarket.com/products/promin-prometheus-1/ Propellant: LOX/Kerosene or Earth-storable bipropellants Flight heritage: Ukrainian rocket propulsion engineering (SDO Yuzhnoye, Yuzhmash lineage) ## Apollo Constellation Engine (ACE) Ion Thruster — Apollo Fusion (Astra) [propulsion] https://newspacemarket.com/products/apollo-fusion-ace-thruster/ Power consumption: 200 W Propellant: Xenon ## Bradford ECAPS HPGP Thruster — Bradford Space [propulsion] https://newspacemarket.com/products/bradford-space-hpgp-thruster/ Propellant: LMP-103S (HPGP, green propellant) Flight heritage: PRISMA (2010), ORBCOMM, numerous commercial smallsats ## Nuclear Thermal Propulsion and RTG Research — CNNC Space (China National Nuclear Corp Space) [propulsion] https://newspacemarket.com/products/cnnc-nuclear-thermal-propulsion/ Flight heritage: Chang'e lunar RHU (heating units); Soviet/US NTP flight test base ## Hydra Space Water-Based Propulsion System — Hydra Space [propulsion] https://newspacemarket.com/products/hydra-space-water-propulsion/ Propellant: Water (H₂O) Propellant: Green / non-toxic / non-pressurized @ (variant 2) ## Vacuum Arc Thruster (VAT) Electric Propulsion System — Hypernova Space Technologies [propulsion] https://newspacemarket.com/products/hypernova-space-propulsion/ Propellant: Solid metal (aluminium or steel) Propellant: Solid (no pressurization required) @ (variant 2) Propellant: Non-toxic, non-hazardous for launch @ (variant 3) Flight heritage: EnduroSat Platform-2 SharedSat, SpaceX Transporter-6, January 2023 Propellant: 2 solid metal types @ (variant 4) Propellant: In-orbit metal replenishment from asteroid/debris sources @ (variant 5) ## RD840 — Yuzhnoye Design Bureau [propulsion] https://newspacemarket.com/products/yuzhnoye-rd840/ Propellant: NT + UDMH Specific impulse: 315 Feed/tank pressure: 10 bar Mass: 4300 g ## RD843 — Yuzhnoye Design Bureau [propulsion] https://newspacemarket.com/products/yuzhnoye-rd843/ Propellant: NT + UDMH Specific impulse: 315.5 Mass: 16500 g TRL: 9 Thrust: 2451662.5 mN ## RD861K — Yuzhnoye Design Bureau [propulsion] https://newspacemarket.com/products/yuzhnoye-rd861k/ Propellant: NT + UDMH Specific impulse: 330 Mass: 214000 g TRL: 8 Thrust: 77629441.4 mN ## DU802 — Yuzhnoye Design Bureau [propulsion] https://newspacemarket.com/products/yuzhnoye-du802/ Propellant: NT + UDMH Specific impulse: 322.5 Mass: 165400 g TRL: 7 Thrust: 4412992.5 mN ## RD805 — Yuzhnoye Design Bureau [propulsion] https://newspacemarket.com/products/yuzhnoye-rd805/ Propellant: O2 + kerosene Specific impulse: 345 Mass: 80000 g TRL: 4 Thrust: 21084297.5 mN ## RD809M — Yuzhnoye Design Bureau [propulsion] https://newspacemarket.com/products/yuzhnoye-rd809m/ Propellant: O2 + kerosene Specific impulse: 345 Mass: 325000 g TRL: 6 Thrust: 88259850 mN ## RD809K — Yuzhnoye Design Bureau [propulsion] https://newspacemarket.com/products/yuzhnoye-rd809k/ Propellant: O2 + kerosene Specific impulse: 352 Mass: 330000 g TRL: 6 Thrust: 98066500 mN ## RD835 / RD835T — Yuzhnoye Design Bureau [propulsion] https://newspacemarket.com/products/yuzhnoye-rd835-rd835t/ Propellant: O2 + kerosene Specific impulse: 355 Mass: 830000 g Mass: 808000 g @ (variant 2) TRL: 3 Thrust: 490332500 mN ## RD870 — Yuzhnoye Design Bureau [propulsion] https://newspacemarket.com/products/yuzhnoye-rd870/ Propellant: O2 + kerosene Specific impulse: 301.5 Specific impulse: 340 @ (variant 2) Mass: 1420000 g TRL: 6 Thrust: 777667345 mN Thrust: 876714510 mN @ (variant 2) ## RD872 — Yuzhnoye Design Bureau [propulsion] https://newspacemarket.com/products/yuzhnoye-rd872/ Propellant: O2 + kerosene Specific impulse: 350.5 Mass: 1530000 g TRL: 6 Thrust: 912018450 mN ## RD874 — Yuzhnoye Design Bureau [propulsion] https://newspacemarket.com/products/yuzhnoye-rd874/ Propellant: Liquid oxygen + kerosene Specific impulse: 303.2 Specific impulse: 338.7 @ (variant 2) Mass: 6070000 g TRL: 6 Thrust: 3130282680 mN Thrust: 3495090060 mN @ (variant 2) ## RD815 — Yuzhnoye Design Bureau [propulsion] https://newspacemarket.com/products/yuzhnoye-rd815/ Propellant: O2 + kerosene Specific impulse: 306.7 Specific impulse: 335 @ (variant 2) Mass: 3200000 g TRL: 4 Thrust: 2464411145 mN Thrust: 2691925425 mN @ (variant 2) ## RD860 — Yuzhnoye Design Bureau [propulsion] https://newspacemarket.com/products/yuzhnoye-rd860/ Propellant: NT + UDMH Specific impulse: 322.5 Mass: 34000 g TRL: 6 Thrust: 4903325 mN Thrust: 2451662.5 mN @ (variant 2) ## RD860L — Yuzhnoye Design Bureau [propulsion] https://newspacemarket.com/products/yuzhnoye-rd860l/ Propellant: NT + UDMH Specific impulse: 322.5 Mass: 106000 g TRL: 6 Thrust: 9806650 mN Thrust: 2451662.5 mN @ (variant 2) ## RD860M — Yuzhnoye Design Bureau [propulsion] https://newspacemarket.com/products/yuzhnoye-rd860m/ Propellant: NT + UDMH Specific impulse: 322.5 Mass: 112000 g TRL: 6 Thrust: 4903325 mN Thrust: 2451662.5 mN @ (variant 2) ## Solid Rocket Motors for Space Launch Vehicles — Yuzhnoye Design Bureau [propulsion] https://newspacemarket.com/products/yuzhnoye-solid-rocket-motors-for-space-launch-vehicles/ Propellant: Composite, high-energy ## Liquid-Propellant Low-Thrust Thrusters — Yuzhnoye Design Bureau [propulsion] https://newspacemarket.com/products/yuzhnoye-liquid-propellant-low-thrust-thrusters/ Propellant: Nitrogen Tetroxide + UDMH Specific impulse: 2000 Specific impulse: 2600 @ (variant 2) Supply voltage: 28 Thrust: 30000-100000 mN ## Gas-Jet Propulsion System (GJPS) — Yuzhnoye Design Bureau [propulsion] https://newspacemarket.com/products/yuzhnoye-gas-jet-propulsion-system-gjps/ Feed/tank pressure: 230 bar Feed/tank pressure: 3 bar @ (variant 2) Specific impulse: 710 Thrust: 250000-7000000 mN ## Hall-Engine Electric Jet Propulsion System (EJPS) — Yuzhnoye Design Bureau [propulsion] https://newspacemarket.com/products/yuzhnoye-hall-engine-electric-jet-propulsion-system-ejps/ Feed/tank pressure: 130 bar Specific impulse: 2200-22000 Thrust: 50000000-1000000000 mN Thrust: 1-66 mN @ (variant 2) ## Green Monopropellant Propulsion System — Yuzhnoye Design Bureau [propulsion] https://newspacemarket.com/products/yuzhnoye-green-monopropellant-propulsion-system/ Propellant: 0.15 kg Mass: 1100 g Envelope (L×W×H): 100 x 100 x 135 mm Thrust: 320000 mN Thrust: 153 mN @ (variant 2) Propellant mass: 150 g ## Ablation Jet Engine — Yuzhnoye Design Bureau [propulsion] https://newspacemarket.com/products/yuzhnoye-ablation-jet-engine/ Specific impulse: 20000 Total impulse: 200 N·s Power consumption: 20 W Envelope (L×W×H): 90 x 21 x 32 mm Envelope (L×W×H): 100 x 100 x 30 mm @ (variant 2) Propellant: No pressurized gases required Thrust: 0.1 mN ## Ammonia Jet Propulsion System (APS) — Yuzhnoye Design Bureau [propulsion] https://newspacemarket.com/products/yuzhnoye-ammonia-jet-propulsion-system-aps/ Propellant: Ammonia Supply voltage: 24-34 Power consumption: 375 W Mass: 24000 g Thrust: 49 mN Thrust: 7000000 mN @ (variant 2) Thrust: 2500000 mN @ (variant 3) ## Lunar Booster Stage (LBS) — Yuzhnoye Design Bureau [propulsion] https://newspacemarket.com/products/yuzhnoye-lunar-booster-stage-lbs/ Propellant: LOX + kerosene ## Circumlunar Booster Tug (LBT) — Yuzhnoye Design Bureau [propulsion] https://newspacemarket.com/products/yuzhnoye-circumlunar-booster-tug-lbt/ Propellant: NT + UDMH ## RL-10 Upper Stage Engine Family — Aerojet Rocketdyne (L3Harris) [propulsion] https://newspacemarket.com/products/aerojet-rl-10-upper-stage-engine/ Propellant: Fuel: liquid hydrogen; Oxidizer: liquid oxygen ## Supernova — Rapidly Maneuverable Multi-Orbit Spacecraft — Portal Space Systems [propulsion] https://newspacemarket.com/products/portal-space-supernova-spacecraft/ Propellant: Ammonia (storable, non-cryogenic) ## ND-25TC Neumann Drive — Low-Power Nanosatellite Thruster — Neumann Space [propulsion] https://newspacemarket.com/products/neumann-nd-25tc-thruster/ Total impulse: 880 N·s (min) Specific impulse: 1800-2000 Propellant: Solid metal rod (molybdenum standard; also Mg, Ti, V, Al, C) ## LeoBear — 500 W Hall-Effect Thruster — Pulsar Fusion [propulsion] https://newspacemarket.com/products/pulsar-fusion-leobear-het/ Specific impulse: 1199-2149 Specific impulse: 2058-2300 @ (variant 2) Propellant: Krypton (primary), Xenon Envelope (L×W×H): 130 × 130 × 150 mm Thrust: 13-36 mN ## MoonRanger — 5 kW Hall-Effect Thruster — Pulsar Fusion [propulsion] https://newspacemarket.com/products/pulsar-fusion-moonranger-5kw/ Power consumption: 5-7 W Propellant: Krypton, Xenon Thrust: 280 mN (min) Thrust: 350 mN (min) @ (variant 2) ## MarsRanger — 10 kW Hall-Effect Thruster — Pulsar Fusion [propulsion] https://newspacemarket.com/products/pulsar-fusion-marsranger-10kw/ Power consumption: 10 W Supply voltage: 300-500 Propellant: Krypton (primary) ## spaceware™ Hall Effect Thruster — Exotrail [propulsion] https://newspacemarket.com/products/spaceware-hall-effect-thruster-3252/ Power consumption: 60 W Power consumption: 150 W @ (variant 2) Power consumption: 300-600 W Thrust: 2.5 mN Thrust: 7 mN @ (variant 2) Thrust: 12-32 mN ## R-4D-15 HiPAT 445 N High Performance Rocket Engine — Aerojet Rocketdyne (L3Harris) [propulsion] https://newspacemarket.com/products/aerojet-r-4d-15-hipat-445n-engine/ Propellant: Hydrazine or MMH fuel with NTO oxidizer Thrust: 445000 mN ## R-4D-11 490 N Bipropellant Rocket Engine — Aerojet Rocketdyne (L3Harris) [propulsion] https://newspacemarket.com/products/aerojet-r-4d-11-490n-bipropellant-engine/ Propellant: Hydrazine or MMH fuel with NTO oxidizer Thrust: 490000 mN ## R-1E 110 N Bipropellant Rocket Engine — Aerojet Rocketdyne (L3Harris) [propulsion] https://newspacemarket.com/products/aerojet-r-1e-110n-bipropellant-engine/ Propellant: Hydrazine or MMH fuel with NTO oxidizer Thrust: 110000 mN ## R-6F 22 N Bipropellant Rocket Engine — Aerojet Rocketdyne (L3Harris) [propulsion] https://newspacemarket.com/products/aerojet-r-6f-22n-bipropellant-engine/ Propellant: Hydrazine or MMH fuel with NTO oxidizer Thrust: 22000 mN ## R-42 890 N Bipropellant Rocket Engine — Aerojet Rocketdyne (L3Harris) [propulsion] https://newspacemarket.com/products/aerojet-r-42-890n-bipropellant-engine/ Propellant: Hydrazine or MMH fuel with NTO oxidizer Thrust: 890000 mN ## R-42DM 890 N Dual Mode High Performance Rocket Engine — Aerojet Rocketdyne (L3Harris) [propulsion] https://newspacemarket.com/products/aerojet-r-42dm-890n-dual-mode-engine/ Propellant: Hydrazine or MMH fuel with NTO oxidizer Thrust: 890000 mN ## AMBR 556 N Dual Mode High Performance Rocket Engine — Aerojet Rocketdyne (L3Harris) [propulsion] https://newspacemarket.com/products/aerojet-ambr-556n-dual-mode-engine/ Propellant: Hydrazine or MMH fuel with NTO oxidizer Thrust: 556000 mN ## Hydrazine Monopropellant Rocket Engines — Aerojet Rocketdyne (L3Harris) [propulsion] https://newspacemarket.com/products/aerojet-monopropellant-rocket-engines/ Propellant: Hydrazine (catalytic decomposition) ## AEPS Advanced Electric Propulsion System — Aerojet Rocketdyne (L3Harris) [propulsion] https://newspacemarket.com/products/aerojet-aeps-advanced-electric-propulsion-system/ Power consumption: 12 W ## NEXT-C Ion Propulsion System — Aerojet Rocketdyne (L3Harris) [propulsion] https://newspacemarket.com/products/aerojet-next-c-ion-propulsion-system/ Power consumption: 7 W Flight heritage: NASA DART mission, launched 2021 (technology demonstration) ## Green Propulsion Systems (AF-M315E) — Aerojet Rocketdyne (L3Harris) [propulsion] https://newspacemarket.com/products/aerojet-green-propulsion-af-m315e/ Propellant: AF-M315E green propellant (hydrazine alternative) Envelope (L×W×H): 1U to 8U ## MESSE Magnetically Enhanced Small Satellite Engine — aliena [propulsion] https://newspacemarket.com/products/aliena-messe-hall-thruster/ Power consumption: 350 W Total impulse: 200000 N·s (min) Propellant: Kr / Xe Thrust: 13.5 mN ## MUSIC Hollow Cathode — aliena [propulsion] https://newspacemarket.com/products/aliena-music-hollow-cathode/ Power consumption: 50 W (max) Time to thrust: 270 s Envelope (L×W×H): 50 g / 3 cm x 4.5 cm ## Hybrid Propulsion Systems — HyImpulse Technologies [propulsion] https://newspacemarket.com/products/hybrid-propulsion-systems/ Propellant: Nitrous oxide hybrid Thrust: 90000000 mN Thrust: 75000000 mN @ (variant 2) Thrust: 10000000 mN @ (variant 3) ## Satellite Engine — Astra Space [propulsion] https://newspacemarket.com/products/satellite-engine/ Propellant: Xenon (Xe) or Krypton (Kr) ## MUSIC Flight-ready | 2nd gen qualified 2026 — aliena [propulsion] https://newspacemarket.com/products/music-flight-ready-2nd-gen-qualified-2026/ Mass: 6000 g Power consumption: 100 W Propellant: Xe ## TH-11 — Space Pioneer (Tianbing Technology) [propulsion] https://newspacemarket.com/products/th-11/ Propellant: Liquid Oxygen + Kerosene Specific impulse: 345 ## TH-12 — Space Pioneer (Tianbing Technology) [propulsion] https://newspacemarket.com/products/th-12/ Propellant: Liquid Oxygen + Kerosene Specific impulse: 285 ## TH-12V — Space Pioneer (Tianbing Technology) [propulsion] https://newspacemarket.com/products/th-12v/ Propellant: Liquid Oxygen + Kerosene Specific impulse: 346 ## TH-31 — Space Pioneer (Tianbing Technology) [propulsion] https://newspacemarket.com/products/th-31/ Propellant: Dinitrogen tetroxide/Monomethylhydrazine (NTO/MMH) Specific impulse: 310 Thrust: 3000000 mN ## High-Test Peroxide Systems – Halcyon — Benchmark Space Systems [propulsion] https://newspacemarket.com/products/high-test-peroxide-systems-halcyon/ Propellant: 1 - 10 N Specific impulse: 155-160 Propellant: 20 N @ (variant 2) Specific impulse: 270-280 @ (variant 2) Thrust: 1000-10000 mN Thrust: 20000 mN ## RF Ion Thrusters — Busek Co. [propulsion] https://newspacemarket.com/products/rf-ion-thrusters/ Power consumption: 56-80 W ## BGT-X5 Green Monopropellant Thruster — Busek Co. [propulsion] https://newspacemarket.com/products/bgt-x5-green-monopropellant-thruster/ Power consumption: 20 W Propellant: ASCENT Specific impulse: 220-225 Total impulse: 565 N·s Thrust: 500 mN ## BHT-100 — Busek Co. [propulsion] https://newspacemarket.com/products/bht-100/ Power consumption: 100 W Specific impulse: 1000 Total impulse: 250000 N·s (min) Thrust: 7 mN ## Electrospray Thrusters — Busek Co. [propulsion] https://newspacemarket.com/products/electrospray-thrusters/ Propellant: Ionic Liquid Thrust: 0.0002 mN (max) ## CHIPS (0.5U) — CU Aerospace [propulsion] https://newspacemarket.com/products/chips-0-5u/ Total impulse: 176 N·s Specific impulse: 67 Mass: 1079 g TRL: 6 Thrust: 15 mN ## Filament pulsed plasma thruster (FPPT) — CU Aerospace [propulsion] https://newspacemarket.com/products/filament-pulsed-plasma-thruster-fppt/ Specific impulse: 3500 Total impulse: 1000-600000 N·s Total impulse: 1.7 N·s Envelope (L×W×H): 1.7 liters ## Monofilament Vaporization Propulsion (MVP) — CU Aerospace [propulsion] https://newspacemarket.com/products/monofilament-vaporization-propulsion-mvp/ Specific impulse: 66 Total impulse: 265 N·s ## Mira — Impulse Space [propulsion] https://newspacemarket.com/products/mira/ Propellant: Nitrous oxide and ethane ## Helios — Impulse Space [propulsion] https://newspacemarket.com/products/helios/ Specific impulse: 380 Propellant: Liquid oxygen and liquid methane ## EVTC-09G1D103-05 — Emhiser Research [radios] https://newspacemarket.com/products/g-band-transmitters-evtc-series/ Modulation: 8 MHz Pk-Pk Modulation: 75 Ohms, Shunted by 30pF Maximum @ (variant 2) Modulation: 300 KHz Pk-Pk @ (variant 3) Operating temperature: -20 °C Survival temperature: -54 °C TX power: 10 W @ Minimum Power consumption: 56 W @ TX (calculated from 28V * 2.0A) Data interface: other @ Frequency Selection via MDM-15P Connector Connector: SMA FEMALE @ RF OUT Connector: SMA FEMALE @ VIDEO IN Connector: #PT02H-8-4P @ Power Input Envelope (L×W×H): 3.50" L x 3.20" W x 1.00" H Mass: 12 g @ Maximum ## Telemetry Transmitters (ETT Series) — Emhiser Research [radios] https://newspacemarket.com/products/telemetry-transmitters-ett-series/ Envelope (L×W×H): 3.40" x 1.865" x 0.30" Frequency: 1435.5 MHz (min) Frequency: 2399.5 MHz (max) TX power: 0.15 W @ minimum TX power: 0.5 W @ minimum (variant 2) TX power: 1 W @ minimum (variant 3) TX power: 2 W @ minimum (variant 4) Supply voltage: 12 (min) Supply voltage: 4 (max) Power consumption: 0.2 W @ 150mW output Power consumption: 0.4 W @ 500mW output Power consumption: 0.65 W @ 1W output Power consumption: 1 W @ 2W output Operating temperature: -20 °C (min) Operating temperature: 70 °C (max) Mass: 2 g @ maximum ## Digital Receivers (EDR Series) — Emhiser Research [radios] https://newspacemarket.com/products/digital-receivers-edr-series/ Operating temperature: -20 °C Survival temperature: -54 °C RX sensitivity: -90 @ RF Input Sensitivity (minimum signal for 0.5V, >0.3 VDC nominal at threshold sensitivity) RX sensitivity: -90 @ RF Input Sensitivity (minimum signal for 0.5V, >0.3 VDC nominal at threshold sensitivity) (varia Data rate: 0.1 kbps (min) @ Digital Output Data Rate Data rate: 15000 kbps (max) @ Digital Output Data Rate Data interface: RS-422 @ Digital Output Interface Data rate: 0.1 kbps (min) @ Digital Output Data Rate (variant 2) Data rate: 2000 kbps (max) @ Digital Output Data Rate (variant 2) Data interface: RS-422 @ Digital Output Interface (variant 2) Data rate: 0.1 kbps (min) @ Digital Output Data Rate (variant 3) Data rate: 15000 kbps (max) @ Digital Output Data Rate (variant 3) Data interface: RS-422 @ Digital Output Interface (variant 3) Data rate: 0.1 kbps (min) @ Digital Output Data Rate (variant 4) Data rate: 2000 kbps (max) @ Digital Output Data Rate (variant 4) Data interface: RS-422 @ Digital Output Interface (variant 4) Power consumption: 8.4 W (max) @ Reverse Polarity Protected Power consumption: 8.4 W (max) @ Reverse Polarity Protected (variant 2) Power consumption: 8.4 W (max) @ Reverse Polarity Protected (variant 3) Power consumption: 8.4 W (max) @ Reverse Polarity Protected (variant 4) Envelope (L×W×H): 3.50" x 3.20" x 2.20" @ approximate Envelope (L×W×H): 3.50" x 3.20" x 2.20" @ approximate (variant 2) Envelope (L×W×H): 3.50" x 3.20" x 2.20" @ approximate (variant 3) Envelope (L×W×H): 3.50" x 3.20" x 2.20" @ approximate (variant 4) ## FSK Receivers (EFR Series) — Emhiser Research [radios] https://newspacemarket.com/products/fsk-receivers-efr-series/ Envelope (L×W×H): 3.50 x 2.20 x 1.31 inches Frequency: 1439.5-1538.5 MHz @ RF Input Frequency: 2300.2-2399.2 MHz @ RF Input (variant 2) Frequency: 12-13 MHz @ IF RX sensitivity: -100 @ Minimum, without damage RX sensitivity: -93 @ at Threshold Sensitivity Data rate: 57.6 kbps @ MIL-STD-1553, or RS422 Compatible Supply voltage: 28 @ Nominal Power consumption: 0.55 W @ Maximum Operating temperature: -20-70 °C Survival temperature: -55-115 °C ## N-XONOS – X-Band Transmitter – High Data Rate — Syrlinks [radios] https://newspacemarket.com/products/syrlinks-n-xonos-x-band-transmitter/ Flight heritage: Yes Flight heritage: Yes @ (variant 2) Design lifetime: 2-5 years @ LEO missions Data rate: 400000 kbps @ Input Power consumption: 15 W @ at 2W RF ## S-band Transceiver — EnduroSat [radios] https://newspacemarket.com/products/endurosat-s-band-transceiver/ Frequency: 8000-8400 MHz ## UHF Transceiver — EnduroSat [radios] https://newspacemarket.com/products/endurosat-uhf-transceiver/ Data rate: 19.6 kbps TX power: 8 W Supply voltage: 5 TX power: 27 W @ (variant 2) ## SatCOM UHF Digital Radio Transceiver — NanoAvionics [radios] https://newspacemarket.com/products/nanoavionics-uhf-transceiver/ Flight heritage: 60+ satellites launched, 300+ in production (per nanoavionics.com) ## SXC-UHF-02 UHF Transceiver — SPUTNIX [radios] https://newspacemarket.com/products/sputnix-sxc-uhf-02-transceiver/ Envelope (L×W×H): 87 × 93 × 13 mm Modulation: GMSK RX sensitivity: -119 ## SX-GND-03 Laboratory UHF Transceiver — SPUTNIX [radios] https://newspacemarket.com/products/sputnix-sx-gnd-03-lab-uhf-transceiver/ TX power: 0.01 W Envelope (L×W×H): 149 × 64 × 49 ## Radio Complex set RK-SM — Glavkosmos [radios] https://newspacemarket.com/products/radio-complex-set-rk-sm/ Design lifetime: 10 years Lead time: 6 Frequency: 402-406 MHz Mass: 5000 g ## High-speed X-band Downlink Transmitter — Glavkosmos [radios] https://newspacemarket.com/products/high-speed-x-band-downlink-transmitter/ Design lifetime: 7 years Lead time: 12 Mass: 1800 g Power consumption: 70 W Frequency: 8050-8500 MHz TX power: 8 W Modulation: QPSK, 8PSK, 16APSK Radiation tolerance (TID): 6 krad (min) ## Nanosatellite Transceiver — Glavkosmos [radios] https://newspacemarket.com/products/nanosatellite-transceiver/ Design lifetime: 1 years Lead time: 6 Connector: SMA ## UHF Transceiver — Glavkosmos [radios] https://newspacemarket.com/products/uhf-transceiver/ Design lifetime: 1 years Lead time: 2 Flight heritage: SiriusSat-1/2, launched 15 August 2018 Envelope (L×W×H): 87 × 93 × 13 mm Mass: 43 g Supply voltage: 5-14 Power consumption: 0.2 W Power consumption: 3.5 W @ (variant 2) RX sensitivity: -119 TX power: 1 W ## X-band Transmitter Designed for Lunar Spacecraft — Glavkosmos [radios] https://newspacemarket.com/products/x-band-transmitter-designed-for-lunar-spacecraft/ Design lifetime: 1 years Lead time: 12 Mass: 2900 g Power consumption: 70 W Frequency band: 8450-8500 TX power: 8 W Modulation: QPSK, 8PSK Radiation tolerance (TID): 6 krad (min) ## X-band Transmitter for Cubesat — Glavkosmos [radios] https://newspacemarket.com/products/x-band-transmitter-for-cubesat/ Design lifetime: 3 years Lead time: 12 Mass: 380 g Power consumption: 22 W Frequency: 8100-8500 MHz TX power: 2.5 W Modulation: QPSK, 8PSK, 16APSK ## Emergency Locator Transmitter — Glavkosmos [radios] https://newspacemarket.com/products/emergency-locator-transmitter/ Mass: 530 g Envelope (L×W×H): 55 × 79 × 175 mm Lead time: 6 ## Personal Radio Beacon — Glavkosmos [radios] https://newspacemarket.com/products/personal-radio-beacon/ Lead time: 6 Mass: 530 g Envelope (L×W×H): 55 × 79 × 175 mm ## K/Ka-Band SATCOM Transceiver Module KKa-TR-DL-1929 — Arralis [radios] https://newspacemarket.com/products/arralis-kka-tr-dl-1929-satcom-transceiver/ Frequency: 17000-21000 MHz Frequency: 27000-30000 MHz @ (variant 2) Frequency: 1000-5000 MHz @ (variant 3) Frequency: 1000-4000 MHz @ (variant 4) TX power: 0.1 W Supply voltage: 12 Power consumption: 6 W (max) Envelope (L×W×H): 96 x 91 x 33 mm Operating temperature: -40 °C Connector: SMPM (RF), SMA (IF/reference) ## X-Band SATCOM Transceiver X-TR-DL-78 — Arralis [radios] https://newspacemarket.com/products/arralis-x-tr-dl-78-x-band-satcom-transceiver/ Frequency: 8000-8500 MHz Frequency: 7000-7500 MHz @ (variant 2) Frequency: 200-700 MHz @ (variant 3) Frequency: 200-700 MHz @ (variant 4) TX power: 1 W TX power: 2 W @ (variant 2) Supply voltage: 12-36 Supply voltage: 6-42 @ (variant 2) Envelope (L×W×H): 96 x 91 x 33 mm Mass: 1000 g (max) Operating temperature: -40 °C Connector: SMA (TX/RX), SMPM edge-mount (IF) ## Xen-Hub — Xenesis [radios] https://newspacemarket.com/products/xenesis-xen-hub/ Data rate: 10000000 kbps (min) Design lifetime: 5 years ## X-Band LNA for Earth Observation & Lunar Communications — TTI Norte [radios] https://newspacemarket.com/products/tti-norte-x-band-lna/ Frequency: 7900-8500 MHz Frequency: 8000-8500 MHz @ (variant 2) Frequency: 8400-8500 MHz @ (variant 3) ## TA4010 — Triad RF Systems [radios] https://newspacemarket.com/products/triad-rf-ta4010/ Frequency: 4400 MHz Frequency: 5000 MHz @ (variant 2) Envelope (L×W×H): 5.3 x 3.25 x 0.6 in ## CENTAURI — Transcelestial [radios] https://newspacemarket.com/products/transcelestial-centauri/ Power consumption: 25-32 W ## CENTAURI+ — Transcelestial [radios] https://newspacemarket.com/products/transcelestial-centauri-plus/ Envelope (L×W×H): > 70% smaller than traditional RF antennas ## GAMALINK Inter-Satellite Link Radio — TEKEVER [radios] https://newspacemarket.com/products/tekever-gamalink-isl-radio/ Flight heritage: ESA Hera mission (asteroid proximity operations) ## EWC27 X-Band Transmitter — Syrlinks [radios] https://newspacemarket.com/products/syrlinks-ewc27-xband-transmitter/ Data rate: 140000 kbps Flight heritage: 120+ flight models, 100% reliability; OPS-SAT, HawkEye 360 ## LaserCube Laser Communication Terminal — Stellar Project [radios] https://newspacemarket.com/products/stellar-project-lasercube/ Mass: 2000 g Flight heritage: Maiden flight June 30, 2021 on SpaceX Transporter-2 (D-Orbit ION Satellite Carrier) ## Passive Nanosatellite Tracking and Telemetry RF Tag — Stellar Exploration, Inc. [radios] https://newspacemarket.com/products/passive-nanosatellite-tracking-and-telemetry-rf-tag/ Modulation: Backscatter modulation from space radars Lead time: 3 Flight heritage: NASA PACE-1 and PACE-2 satellites Envelope (L×W×H): 5 cm x 5 cm x 1 cm ## NANOcomm-2 — SkyLabs d.o.o. [radios] https://newspacemarket.com/products/skylabs-nanocomm-2/ TRL: 9 ## BusCORE Satellite RF Terminal — SkyFox Labs s.r.o. [radios] https://newspacemarket.com/products/skyfox-labs-buscore-satellite-rf-terminal/ Connector: PC/104+ stack connector, 2x MCX-Female antenna ports Envelope (L×W×H): 95.9 x 90.8 x 18 mm Mass: 140 g Operating temperature: -40-85 °C Flight heritage: TRL9, SSO 530 km, 5+ years of operations ## NANOlink(-S)-boost-dp — SkyLabs d.o.o. [radios] https://newspacemarket.com/products/skylabs-nanolink-s-boost-dp/ TRL: 9 ## NANOlink(-S)-boost — SkyLabs d.o.o. [radios] https://newspacemarket.com/products/skylabs-nanolink-s-boost/ TRL: 9 ## NANOlink(-S)-base — SkyLabs d.o.o. [radios] https://newspacemarket.com/products/skylabs-nanolink-s-base/ TRL: 9 ## NANOcast — SkyLabs d.o.o. [radios] https://newspacemarket.com/products/skylabs-nanocast/ TRL: 5 ## Satlab VTRX — Satlab A/S [radios] https://newspacemarket.com/products/satlab-vtrx/ Supply voltage: 11 Envelope (L×W×H): 93.0 mm × 87.2 mm × 39.7 mm Mass: 420 g Flight heritage: since 2023 TRL: 9 ## RGUC-A Low Power — RevGo [radios] https://newspacemarket.com/products/revgo-rguc-a-low-power-10w-20w/ Power consumption: 10 W Frequency: 950-1950 MHz Envelope (L×W×H): 5.5*3.94*2.95 inches ## RGUC-Aa160-ACREN-A0 — RevGo [radios] https://newspacemarket.com/products/revgo-rguc-aa160-acren-a0-160w/ Power consumption: 160 W Envelope (L×W×H): 13.7*8.66*7.87 inches Frequency: 950-1950 MHz ## RGUC-D Mid Power — RevGo [radios] https://newspacemarket.com/products/revgo-rguc-d-mid-power-20w-40w/ Power consumption: 20 W Frequency: 16350 MHz TX power: 20 W Power consumption: 20 W @ (variant 2) Envelope (L×W×H): 8.11*5.35*3.47 inches ## RGUC-U Low Power (IFL) — RevGo [radios] https://newspacemarket.com/products/revgo-rguc-u-low-power-ifl-6w-8w/ Power consumption: 6 W Power consumption: 6 W @ (variant 2) Envelope (L×W×H): 6.8*4.0*2.0 inches TX power: 6 W ## UHF TM/TC radio link — SPUTNIX [radios] https://newspacemarket.com/products/uhf-tm-tc-radio-link/ Envelope (L×W×H): 115 x 66 x 19 (without fasteners) mm Mass: 135 g Frequency: 435-438 MHz TX power: 5 W ## S-band TM/TC radio link — SPUTNIX [radios] https://newspacemarket.com/products/s-band-tm-tc-radio-link/ Envelope (L×W×H): 117 x 111 x 48 (without fasteners and diplexer) Frequency: 2025-2110 MHz Frequency: 2200-2290 MHz @ (variant 2) TX power: 5 W Modulation: BPSK, QPSK, 8-PSK ## UHF transceiver — SPUTNIX [radios] https://newspacemarket.com/products/uhf-transceiver-2/ Envelope (L×W×H): 84 x 94 x 19 mm Mass: 43 g Power consumption: 0.4 W Power consumption: 5 W @ (variant 2) Frequency: 433-438 MHz Frequency: 400.1-402 MHz @ (variant 2) Frequency: 144-146 MHz @ (variant 3) Modulation: GMSK ## X-band High Data Rate Transmitter — SPUTNIX [radios] https://newspacemarket.com/products/x-band-high-data-rate-transmitter/ Mass: 15000 g Envelope (L×W×H): 315 x 315 x 120 mm Frequency: 8220 MHz Power consumption: 200 W Power consumption: 20 W @ (variant 2) ## Bracer Tactical SATCOM Radio — QinetiQ Space [radios] https://newspacemarket.com/products/qinetiq-bracer-satcom/ Mass: 450 g Data rate: 2.4 kbps ## Satellite Transponder Systems — Saab Space [radios] https://newspacemarket.com/products/saab-satellite-transponders/ Flight heritage: ESA missions, European commercial satellites ## Laser Communication Terminal — AstroGate Labs [radios] https://newspacemarket.com/products/astrogate-laser-comm/ Flight heritage: Validated with Indian Navy, ISRO, DRDO ## Stensat radio beacon — StenSat Group LLC [radios] https://newspacemarket.com/products/stensat-radio-beacon/ Frequency band: 2 TX power: 0-3 W Supply voltage: 5-12 Envelope (L×W×H): 1.75" x 3.1" x 1 " ## CANSAT Transmitter Module — StenSat Group LLC [radios] https://newspacemarket.com/products/stensat-cansat-transmitter-module/ Supply voltage: 5-12 ## μKaTX-300™ Ka-Band Transmitter — Voyager Technologies [radios] https://newspacemarket.com/products/spacemicro-ukatx-300-ka-band-transmitter/ Data rate: 4000000 kbps Modulation: 32QAM Flight heritage: NASA TESS — over 5 years continuous operation ## S-Band Transmitter for Pico and Nanosatellites — IQ Spacecom [radios] https://newspacemarket.com/products/s-band-transmitter-for-pico-and-nanosatellites/ Lead time: 4 ## EyeStar-S3 Satellite Simplex Communications System — NearSpace Launch [radios] https://newspacemarket.com/products/eyestar-s3-satellite-simplex-communications-system/ TRL: 9 ## NSL EyeStar S4 — NearSpace Launch [radios] https://newspacemarket.com/products/nsl-eyestar-s4/ Flight heritage: since 2015 Envelope (L×W×H): 60x30x21 mm Mass: 29 g TX power: 1 W Power consumption: 0.25 W TX power: 1.4 W @ (variant 2) Frequency: 1622 MHz TRL: 9 Flight heritage: over 180 successfully deployed in orbit @ (variant 2) ## S-Band Transceiver SRS-3 — NanoAvionics [radios] https://newspacemarket.com/products/nanoavionics-sband-transceiver-srs3/ Frequency: 2200-2290 MHz Frequency: 2025-2110 MHz @ (variant 2) Supply voltage: 5-40 Mass: 190 g ## S-Band Transceiver SRS-4 — NanoAvionics [radios] https://newspacemarket.com/products/nanoavionics-sband-transceiver-srs4/ Frequency: 2200-2290 MHz Frequency: 2025-2110 MHz @ (variant 2) Modulation: BPSK, QPSK, 8PSK Modulation: BPSK, QPSK (up to 5 MBd) @ (variant 2) Supply voltage: 5.1-28.8 Mass: 253 g ## AstroLink Laser Communication Terminal — AstroGate Labs [radios] https://newspacemarket.com/products/astrolink-laser-communication-terminal/ Envelope (L×W×H): 95 × 95 × 80 mm TRL: 7 Flight heritage: Flight heritage 2021 (3U nanosatellite) ## C-Band Transponder — IMT (Ingegneria Marketing Technologies) [radios] https://newspacemarket.com/products/imt-c-band-transponder/ Design lifetime: 3 years Frequency band: 5091 Envelope (L×W×H): 90 x 96 x 40 mm Mass: 400 g Connector: RADIALL SMPM R201.423.110 Connector: SAMTEC SEAF-20-06-0-S-04-1-A-K @ (variant 2) Frequency band: 500 (min) Connector: RADIALL SMPM R201.423.110 @ (variant 3) Frequency: 390 MHz Frequency band: 18 @ (variant 2) Connector: RADIALL SMPM R201.423.110 @ (variant 4) Frequency: 460 MHz @ (variant 2) ## IMT X-Band Transponder — IMT (Ingegneria Marketing Technologies) [radios] https://newspacemarket.com/products/imt-x-band-transponder/ TX power: 15 W Modulation: PCM/PSK/PM Power consumption: 7.4 W Power consumption: 12.8 W @ (variant 2) Power consumption: 94.4 W @ (variant 3) Mass: 1200 g Operating temperature: -20-50 °C Design lifetime: 3 years ## Akash Satellite Radio — Akash Systems [radios] https://newspacemarket.com/products/akash-cubesat-radio/ Modulation: Flexible modulation and coding scheme Envelope (L×W×H): 50% smaller ## LBR-2195A L-Band Satellite Beacon Receiver — AVCOM of Virginia [radios] https://newspacemarket.com/products/avcom-lbr-2195a/ Frequency: 950-2150 MHz Frequency band: 10-750 Frequency band: 10-150 @ (variant 2) Power consumption: 3 W (max) Operating temperature: -30-60 °C ## SBS2-2150E Embedded Satellite Beacon Receiver Board — AVCOM of Virginia [radios] https://newspacemarket.com/products/avcom-sbs2-2150e/ Frequency: 950-2150 MHz Frequency band: 10-750 Frequency band: 10-150 @ (variant 2) Power consumption: 7 W Envelope (L×W×H): 3.75 x 5.75 x 1.1 in Operating temperature: -40-70 °C ## A88 Series S-Band Telemetry Transmitter (STX) — ADDNICS Corporation [radios] https://newspacemarket.com/products/addnics-a88-stx/ Frequency: 2250-2300 MHz TX power: 0.5 W Modulation: BPSK Envelope (L×W×H): 80 x 80 x 15 mm Mass: 120 g Flight heritage: RISING-2 (2014), HODOYOSHI series, DIWATA-1 (2016), DIWATA-2 (2018) ## A74 Series S-Band Telemetry Transmitter (STX) — ADDNICS Corporation [radios] https://newspacemarket.com/products/addnics-a74-stx/ TX power: 0.1 W Modulation: QPSK/OQPSK (Intelsat IESS-308) Envelope (L×W×H): 95 x 50 x 20 mm Mass: 140 g Flight heritage: SPRITE-SAT / RISING (2009) ## A88 Series X-Band Telemetry Transmitter (XTX) — ADDNICS Corporation [radios] https://newspacemarket.com/products/addnics-a88-xtx/ Flight heritage: Procyon deep-space (2014), DIWATA-1 (2016), DIWATA-2 (2018) ## UHF-Band Telemetry Transmitter (UHF Com) — ADDNICS Corporation [radios] https://newspacemarket.com/products/addnics-uhf-com-transmitter/ TX power: 0.8 W Modulation: GMSK, AFSK Data rate: 9.6 kbps Data rate: 1.2 kbps @ (variant 2) Envelope (L×W×H): 70 x 40 x 14 mm ## ODALCOM — Emxys [radios] https://newspacemarket.com/products/emxys-odalcom/ Mass: 1500 g (max) Power consumption: 0.2 W Power consumption: 1 W @ (variant 2) Modulation: Unipolar NRZ Envelope (L×W×H): 109K logic elements Power consumption: 2.6 W @ (variant 3) Envelope (L×W×H): 87 mm x 87 mm x 15 mm @ (variant 2) Mass: 60 g ## Intellian MIL-SPEC VSAT — Intellian Technologies [radios] https://newspacemarket.com/products/intellian-mil-spec-vsat/ Frequency band: 29 Frequency band: 30 @ (variant 2) ## K Band Transmitter — Paradigma Technologies [radios] https://newspacemarket.com/products/paradigma-k-band-transmitter/ Frequency: 17800-20200 MHz Frequency: 900-3500 MHz @ (variant 2) Modulation: ASK, PSK up to 2 Mbps; OQPSK, MSK, FSK, GFSK, 4-FSK up to 350 kbps Power consumption: 13 W Power consumption: 0.1 W (max) Supply voltage: 4-18 Mass: 475 g Envelope (L×W×H): 94 × 94 × 25 mm Operating temperature: -40 °C ## Ka Band Receiver with UHF Transceiver — Paradigma Technologies [radios] https://newspacemarket.com/products/paradigma-ka-band-receiver-uhf-transceiver/ Frequency band: 26.5-30 Frequency band: 2.5 (max) Frequency band: 900-930 @ (variant 2) TX power: 1 W Power consumption: 4 W Power consumption: 6 W @ (variant 2) Supply voltage: 3-18 Mass: 250 g Envelope (L×W×H): 94 × 94 × 20 mm Operating temperature: -40 °C ## Ka Band Transponder — Paradigma Technologies [radios] https://newspacemarket.com/products/paradigma-ka-band-transponder/ Frequency: 17300-21200 MHz Frequency: 27000-31000 MHz @ (variant 2) Power consumption: 19 W Supply voltage: 11-32 Mass: 1600 g Envelope (L×W×H): 2U Operating temperature: -30 °C Flight heritage: Q2 2024 ## Q Band Transmitter — Paradigma Technologies [radios] https://newspacemarket.com/products/paradigma-q-band-transmitter/ Frequency: 37500-42500 MHz Modulation: ASK/OOK up to 2 Mbps; n-FSK up to 1 Mbps Power consumption: 10 W Supply voltage: 6.5-30 Mass: 700 g Envelope (L×W×H): 1.5U Operating temperature: -30 °C Flight heritage: Q2 2023 ## TeraBIX Silicon Photonic Transceiver — Mbryonics [radios] https://newspacemarket.com/products/mbryonics-terabix-photonic-transceiver/ Power consumption: 0.005 W (max) ## LE016-R5 QO-100 Full-Duplex Transverter System — Leijenaar Electronics [radios] https://newspacemarket.com/products/leijenaar-le016-r5-transverter/ Power consumption: 5 W TX power: 4 W Frequency: 144.5 MHz Frequency: 1580 MHz @ (variant 2) Mass: 650 g ## SPOT X Two-Way Satellite Messenger — Globalstar (C-3 next-gen) [radios] https://newspacemarket.com/products/globalstar-spot-x-messenger/ Envelope (L×W×H): 16.61 x 7.37 x 2.39 cm Operating temperature: -20 °C ## SmartOne Solar Industrial Asset Tracker — Globalstar (C-3 next-gen) [radios] https://newspacemarket.com/products/globalstar-smartone-solar-tracker/ Envelope (L×W×H): 8.26 x 17.78 x 2.86 cm Operating temperature: -40 °C Supply voltage: 10-48 ## IDRS i100 Inter-Satellite Data Relay Terminal — Addvalue Technologies [radios] https://newspacemarket.com/products/addvalue-idrs-i100-relay-terminal/ Envelope (L×W×H): 125 × 96 × 70 mm Mass: 1000 g Power consumption: 8 W Operating temperature: -25 °C ## ESTI-T2E1-SR Transmitter — Emhiser Research [radios] https://newspacemarket.com/products/multimode-transmitters-esti-series/ Frequency: 2200-2300 MHz Power consumption: 2 W ## EVT-01 Series Transmitters — Emhiser Research [radios] https://newspacemarket.com/products/video-transmitters-evt-series/ Frequency: 1710-1850 MHz Frequency: 2200-2400 MHz @ (variant 2) Power consumption: 0.15 W Power consumption: 0.5 W @ (variant 2) Power consumption: 1 W @ (variant 3) Power consumption: 2 W @ (variant 4) ## FSK Transmitters (EFT Series) — Emhiser Research [radios] https://newspacemarket.com/products/fsk-transmitters-eft-series/ Modulation: FSK Modulation: 2.5 Max @ (variant 2) Data rate: 0-5000 kbps Frequency: 1435.5-1539.5 MHz Frequency: 1710-1850 MHz @ (variant 2) Frequency: 2300.5-2399.5 MHz @ Single Frequency TX power: 2 W TX power: 5 W @ (variant 2) TX power: 10 W @ (variant 3) TX power: 20 W @ (variant 4) Supply voltage: 28-4 @ supply Power consumption: 1.2 W @ 2 Watts Power consumption: 2.2 W @ 5 Watts Power consumption: 3.6 W @ 10 Watts Power consumption: 6 W @ 20 Watts Envelope (L×W×H): 9 Cubic Inches Mass: 12 g Operating temperature: -20-70 °C Survival temperature: -54-125 °C Frequency: 1435.5-1539.5 MHz @ (variant 3) Frequency: 1710-1850 MHz @ (variant 4) Frequency: 2300.5-2399.5 MHz @ Single Frequency (variant 2) TX power: 2 W @ (variant 5) TX power: 5 W @ (variant 6) TX power: 10 W @ (variant 7) TX power: 20 W @ (variant 8) Supply voltage: 28-4 @ supply (variant 2) Power consumption: 1.2 W @ 2 Watts (variant 2) Power consumption: 2.2 W @ 5 Watts (variant 2) Power consumption: 3.6 W @ 10 Watts (variant 2) Power consumption: 6 W @ 20 Watts (variant 2) Envelope (L×W×H): 11 Cubic Inches @ (variant 2) Mass: 14 g @ (variant 2) Operating temperature: -20-70 °C @ (variant 2) Survival temperature: -54-125 °C @ (variant 2) Frequency: 1435.5-1539.5 MHz @ (variant 5) Frequency: 1710-1850 MHz @ (variant 6) Frequency: 2300.5-2399.5 MHz @ Single Frequency (variant 3) TX power: 40 W @ (variant 9) Supply voltage: 28-4 @ supply (variant 3) Power consumption: 7.5 W @ 30 Watts Power consumption: 9.5 W @ 40 Watts Envelope (L×W×H): 36 Cubic Inches @ (variant 3) Mass: 28 g @ (variant 3) Operating temperature: -20-70 °C @ (variant 3) Survival temperature: -54-125 °C @ (variant 3) Frequency: 1435.5-1539.5 MHz @ (variant 7) Frequency: 1710-1850 MHz @ (variant 8) Frequency: 2300.5-2399.5 MHz @ Channlized TX power: 2 W @ (variant 10) TX power: 5 W @ (variant 11) TX power: 10 W @ (variant 12) TX power: 20 W @ (variant 13) Supply voltage: 28-4 @ supply (variant 4) Power consumption: 1.2 W @ 2 Watts (variant 3) Power consumption: 2.2 W @ 5 Watts (variant 3) Power consumption: 3.6 W @ 10 Watts (variant 3) Power consumption: 6 W @ 20 Watts (variant 3) Envelope (L×W×H): 9 Cubic Inches @ (variant 4) Mass: 12 g @ (variant 4) Operating temperature: -20-70 °C @ (variant 4) Survival temperature: -54-125 °C @ (variant 4) ## Telemetry Receivers (ETR Series) — Emhiser Research [radios] https://newspacemarket.com/products/telemetry-receivers-etr-series/ Supply voltage: 28 Operating temperature: -20 °C Survival temperature: -54 °C ## Video Receivers (EVR Series) — Emhiser Research [radios] https://newspacemarket.com/products/video-receivers-evr-series/ Supply voltage: 28 Frequency band: 30 Operating temperature: -20 °C Survival temperature: -54 °C ## GM1001 — Geespace [radios] https://newspacemarket.com/products/gm1001-f-geesatcom-satellite-communication-module/ Operating temperature: -40 °C Power consumption: 0.3 W Power consumption: 10 W (max) Envelope (L×W×H): 30 mm×35 mm×3.5 mm ## GM1003 — Geespace [radios] https://newspacemarket.com/products/gm1003-geesatcom-in-vehicle-satellite-communication-module/ Operating temperature: -40-85 °C Power consumption: 0.35 W Power consumption: 1.3 W (max) Envelope (L×W×H): 34 mm×48 mm×3.6 mm, stamp-hole package ## Geesatcom DTU — Geespace [radios] https://newspacemarket.com/products/geesatcom-dtu-gt1001-d/ Envelope (L×W×H): Φ=280 mm, H=239 mm ## Geesatcom Solar (GT1002) — Geespace [radios] https://newspacemarket.com/products/geesatcom-solar-gt1002/ Envelope (L×W×H): <=230 mm x 140 mm x 46.7 mm (L x W x H) ## Geesatcom Compact (GT1003) — Geespace [radios] https://newspacemarket.com/products/geesatcom-compact-gt1003/ Envelope (L×W×H): 157.7 mm x 147 mm x 47.5 mm ## Geesatcom Pad — Geespace [radios] https://newspacemarket.com/products/geesatcom-pad-gt1006/ Envelope (L×W×H): 256.5 mm x 170 mm x 8.1 mm ## Geesatcom Handset (GH1001) — Geespace [radios] https://newspacemarket.com/products/geesatcom-handset-gh1001/ Envelope (L×W×H): 112 mm x 82 mm x 31 mm ## ReliaSat Satellite Communications RF Systems and Subsystems — ReliaSat [radios] https://newspacemarket.com/products/reliasat-leolink100/ Frequency: 27500-30000 MHz Frequency: 17700-20200 MHz @ (variant 2) ## NAVRAIL S-Band Locomotive Tracking Terminal — Saankhya Labs [radios] https://newspacemarket.com/products/saankhya-labs-navrail-s-band-locomotive-tracking-terminal/ Frequency: 2560-2590 MHz Frequency: 2670-2690 MHz @ (variant 2) ## GYANDOOT L-Band Satellite Receive-Only Terminal — Saankhya Labs [radios] https://newspacemarket.com/products/saankhya-labs-gyandoot-l-band-satellite-receive-only-terminal/ Frequency band: 950-2150 Envelope (L×W×H): 105 x 70 x 25 mm Mass: 150 g ## Lehar S-band Broadcast Receiver — Saankhya Labs [radios] https://newspacemarket.com/products/saankhya-labs-lehar-s-band-broadcast-receiver/ Frequency band: 2560-2590 Envelope (L×W×H): 105 mm x 74 mm Mass: 95 g ## SAMRAT S-Band Satphone — Saankhya Labs [radios] https://newspacemarket.com/products/saankhya-labs-samrat-s-band-satphone/ Frequency: 2560-2590 MHz Frequency: 2670-2690 MHz @ (variant 2) Data rate: 2.7 kbps ## Broadcast Radio Head (BRH) — Saankhya Labs [radios] https://newspacemarket.com/products/saankhya-labs-broadcast-radio-head/ TX power: 5-40 W ## LinkStar-STX3-PC104 — sci_Zone / QuickSAT [radios] https://newspacemarket.com/products/scizone-linkstar-stx3-pc104/ TX power: 3-5 W ## Chascii Single Optical Terminal (SOT) — Chascii [radios] https://newspacemarket.com/products/chascii-space-tech-services/ Power consumption: 15 W ## IoT System Dedicated Communication Module — Guodian Gaoke (Tianqi Satellite) [radios] https://newspacemarket.com/products/guodian-tianqi-400-gm10-module/ RX sensitivity: -125 Envelope (L×W×H): 30 mm*20 mm*3.5 mm Data rate: 268 kbps Operating temperature: -40 °C Supply voltage: 3.3 Data rate: 115.2 kbps @ (variant 2) Mass: 3 g ## Satellite IoT Dedicated Communication Module — Guodian Gaoke (Tianqi Satellite) [radios] https://newspacemarket.com/products/guodian-tianqi-400-gm12-module/ Data rate: 268 kbps TX power: 30.8 W RX sensitivity: -125 RX sensitivity: -156 @ (variant 2) Operating temperature: -40 °C Envelope (L×W×H): 35*25*3.5 mm Mass: 5 g ## Satellite IoT Communication Module — Guodian Gaoke (Tianqi Satellite) [radios] https://newspacemarket.com/products/guodian-tianqi-400-gm20-module/ RX sensitivity: -125 Envelope (L×W×H): 17.7 mm*15.8 mm*2.4 mm Data rate: 268 kbps RX sensitivity: -125 @ (variant 2) Operating temperature: -40 °C Mass: 1 g ## 240-GM13 Communication Module — Guodian Gaoke (Tianqi Satellite) [radios] https://newspacemarket.com/products/guodian-tianqi-240-gm13-module/ Frequency band: 318-320 RX sensitivity: -125 Envelope (L×W×H): 35*25*3.5 mm Envelope (L×W×H): GB/T 1804 class C tolerance @ (variant 2) ## Tianqi Communication Gateway — Guodian Gaoke (Tianqi Satellite) [radios] https://newspacemarket.com/products/guodian-tianqi-tqzd-08-terminal/ TX power: 1 W (min) RX sensitivity: -132 Survival temperature: -40 °C Connector: DTM06~12 Envelope (L×W×H): 135 mm*117 mm*35 mm Mass: 500 g ## Satellite IoT Communication Terminal — Guodian Gaoke (Tianqi Satellite) [radios] https://newspacemarket.com/products/guodian-tianqi-tqzd-10-terminal/ TX power: 1 W (min) RX sensitivity: -125 Supply voltage: 8-38 Survival temperature: -40 °C Connector: Waterproof M12 Envelope (L×W×H): 80 × 21 ±0.5 mm (diameter × height) Mass: 200 g (max) ## Tianqi Satellite Emergency Distress Terminal — Guodian Gaoke (Tianqi Satellite) [radios] https://newspacemarket.com/products/guodian-tianqi-alarm-01-emergency/ TX power: 1 W (min) Envelope (L×W×H): 125*50*30 mm Mass: 200 g ## Emergency Distress Terminal — Guodian Gaoke (Tianqi Satellite) [radios] https://newspacemarket.com/products/guodian-tianqi-alarm-02-ais-emergency/ TX power: 1 W (min) Envelope (L×W×H): 125*50*30 mm Mass: 200 g ## Tianqi AIS Emergency Rescue Terminal Alarm-03 — Guodian Gaoke (Tianqi Satellite) [radios] https://newspacemarket.com/products/guodian-tianqi-alarm-03-ais-emergency/ Envelope (L×W×H): 125*50*30 mm Mass: 200 g ## Tianqi Bio Mini Wildlife Tracking Terminal — Guodian Gaoke (Tianqi Satellite) [radios] https://newspacemarket.com/products/guodian-tianqi-bio-mini-terminal/ Envelope (L×W×H): 20.6*20.6*11.5 mm ## LSC-F03 — Guodian Gaoke (Tianqi Satellite) [radios] https://newspacemarket.com/products/guodian-tianqi-vehicle-terminal/ Envelope (L×W×H): φ100mmx42.9 mm[H] Frequency: 400 MHz Data rate: 268 kbps TX power: 32 W ## Tianqi Cold-Chain Container Monitoring Terminal — Guodian Gaoke (Tianqi Satellite) [radios] https://newspacemarket.com/products/guodian-tianqi-container-terminal/ Operating temperature: -20 °C Design lifetime: 5 years (min) Envelope (L×W×H): 182 mm(L)×80 mm(W)×37 mm(H) ## ATZC-10-100 C-Band VSAT Transmitter SSPA — ATCi [radios] https://newspacemarket.com/products/atci-atzc-10-100-cband-sspa/ Warranty: 1 ## EWC27 + OPT27-SRX – X/S Transceiver — Syrlinks [radios] https://newspacemarket.com/products/syrlinks-ewc27-xs-transceiver/ Flight heritage: Yes ## EWC28 – X-Band Transmitter — Syrlinks [radios] https://newspacemarket.com/products/syrlinks-ewc28-x-band-transmitter/ Flight heritage: Yes Flight heritage: Yes @ (variant 2) ## XONOS – X-Band High-Data-Rate Transmitter — Syrlinks [radios] https://newspacemarket.com/products/syrlinks-xonos-x-band-transmitter/ Design lifetime: 7 years ## Communication Payload for Satellites — Thorium Space Technology [radios] https://newspacemarket.com/products/thorium-communication-payload/ Frequency: 17700-21200 MHz Frequency: 27500-31000 MHz @ (variant 2) ## Tianqi IoT Gateway Terminal TQZD-08 — Guodian Gaoke (Tianqi Satellite) [radios] https://newspacemarket.com/products/guodian-tianqi-tqzd-08-terminal-2/ Envelope (L×W×H): Max 120 bytes per message TX power: 1 W (min) RX sensitivity: -132 RX sensitivity: -147 @ (variant 2) RX sensitivity: -162 @ (variant 3) TX power: 9.6 W (max) Power consumption: 0.04 W (max) Operating temperature: -20 °C Data rate: 115.2 kbps Envelope (L×W×H): 135×117×35 mm @ (variant 2) Mass: 500 g Design lifetime: 5 years (min) ## UHF/VHF Transceiver — Pyxis Space [radios] https://newspacemarket.com/products/pyxis-uhf-vhf-transceiver/ Envelope (L×W×H): 6 × 30 × 62 mm³ ## DR068-M1 Digitising Receiver — Teledyne Defence & Space [radios] https://newspacemarket.com/products/teledyne-dr068-digitising-receiver/ Frequency: 2000-18000 MHz ## ExseedSat-1 Amateur Radio CubeSat (VO-96) — Satellize [radios] https://newspacemarket.com/products/satellize-exseedsat-1-vo96/ Frequency: 145.9 MHz ## A88 Series S-Band Receiver (A88 SRX) — ADDNICS Corporation [radios] https://newspacemarket.com/products/addnics-a88-srx-sband-receiver/ Modulation: PCM-PSK-PM Operating temperature: -20-60 °C Envelope (L×W×H): 80 x 80 x 16 mm Connector: SMA or SMPM (RF), MDM-15 pin (power/data) ## X-Band TT&C Transponder (X-TRP) — ADDNICS Corporation [radios] https://newspacemarket.com/products/addnics-x-trp-xband-transponder/ Modulation: PCM-PSK-PM Envelope (L×W×H): 80 x 80 mm (height configuration-dependent) ## XTX-DVBS2 — ADDNICS Corporation [radios] https://newspacemarket.com/products/addnics-xtx-dvbs2-xband-transmitter/ Envelope (L×W×H): 80mmx80mmx49.5 mm Modulation: QPSK,16-PSK ## R6 VDES Space Payload — Saab Space [radios] https://newspacemarket.com/products/saab-r6-vdes-payload/ Flight heritage: Saab TransponderTech AIS family: R3, R4, R4A MkII, R5, R5 SUPREME ## CONDOR Mk3.1 — Mynaric [radios] https://newspacemarket.com/products/condor-mk3-1-3282/ TX power: 4 W Data rate: 313000-2500000 kbps Envelope (L×W×H): 280 x 270 x 371 Envelope (L×W×H): 205 x 170 x 157 @ (variant 2) Envelope (L×W×H): 230 x 190 x 128 @ (variant 3) Supply voltage: 22 ## CONDOR Mk3 — Mynaric [radios] https://newspacemarket.com/products/condor-mk3-3282/ Data rate: 313000-2500000 kbps TX power: 4 W Envelope (L×W×H): 370 mm x 270 mm x 270 mm Envelope (L×W×H): 128 mm x 190 mm x 230 mm @ (variant 2) Envelope (L×W×H): 158 mm x170 mm x 205 mm @ (variant 3) Supply voltage: 22 Design lifetime: 5 years ## GaN C SSPA/BUC 800W Outdoor — TTI Norte [radios] https://newspacemarket.com/products/gan-c-sspa-buc-800w-outdoor/ Power consumption: 800 W Supply voltage: 90-264 Power consumption: 3000 W @ (variant 2) Envelope (L×W×H): 442 x 424 x 302 mm Mass: 45000 g Frequency: 950-1525 MHz Frequency: 5850-6425 MHz @ (variant 2) Frequency: 4900 MHz TX power: 794.328 W TX power: 630.957 W @ (variant 2) ## GaN C SSPA/BUC 800W 2:1 REDUNDANCY SYSTEM – Outdoor — TTI Norte [radios] https://newspacemarket.com/products/gan-c-sspa-buc-800w-21-redundancy-system-outdoor/ Power consumption: 800 W Envelope (L×W×H): 19” ## GaN C SSPA/BUC 800W 1:1 REDUNDANCY SYSTEM – Outdoor — TTI Norte [radios] https://newspacemarket.com/products/gan-c-sspa-buc-800w-11-redundancy-system-outdoor/ Power consumption: 800 W Envelope (L×W×H): 19” ## GaN C SSPA/BUC 800W 2:1 Redundancy System Indoor — TTI Norte [radios] https://newspacemarket.com/products/gan-c-sspa-buc-800w-21-redundancy-system-indoor/ Envelope (L×W×H): 19” Rack 42 U (H) x 1 m (D) ## GaN C SSPA/BUC 800W 1:1 Redundancy System Indoor — TTI Norte [radios] https://newspacemarket.com/products/gan-c-sspa-buc-800w-11-redundancy-system-indoor/ Envelope (L×W×H): 19” Rack 42 U (H) x 1 m (D) ## Dual GaN Ka SSPA/BUC 40W Outdoor — TTI Norte [radios] https://newspacemarket.com/products/dual-gan-ka-sspa-buc-40w-outdoor/ Supply voltage: 90-264 Power consumption: 350 W Envelope (L×W×H): 340 x 210 x 170 mm Mass: 15000 g (max) Frequency: 1000-2000 MHz ## GaN X SSPA 300W Indoor — TTI Norte [radios] https://newspacemarket.com/products/gan-x-sspa-300w-indoor/ TX power: 316.228 W TX power: 158.489 W @ (variant 2) Supply voltage: 90-264 Power consumption: 800 W Envelope (L×W×H): 483 x 266 x 560 mm - 6RU panel height Envelope (L×W×H): 343 x 120 x 508 mm - 343 x 120 x 684 mm with pipes @ (variant 2) Mass: 23000 g (max) Frequency: 7900-8400 MHz ## Q SSPA/BUC — TTI Norte [radios] https://newspacemarket.com/products/q-sspa-buc/ Supply voltage: 90-264 Power consumption: 800 W Envelope (L×W×H): 483 x 266 x 560 mm - 6RU panel height Envelope (L×W×H): 343 x 120 x 508 mm - 343 x 120 x 684 mm with pipes @ (variant 2) Mass: 23000 g (max) Frequency: 7900-8400 MHz TX power: 316.228 W TX power: 158.489 W @ (variant 2) ## Q SSPA 25W Outdoor — TTI Norte [radios] https://newspacemarket.com/products/q-sspa-25w-outdoor/ Supply voltage: 90-264 Power consumption: 495 W Envelope (L×W×H): 340 x 210 x 170 mm Mass: 12600 g ## Q BUC 25W Outdoor — TTI Norte [radios] https://newspacemarket.com/products/q-buc-25w-outdoor/ Supply voltage: 264 Power consumption: 495 W Envelope (L×W×H): 340 x 210 x 170 mm Mass: 12300 g Frequency: 950-1450 MHz Frequency: 43000-43500 MHz @ (variant 2) TX power: 25.119 W ## PW LDMOS S SSPA 350W Indoor — TTI Norte [radios] https://newspacemarket.com/products/pw-ldmos-s-sspa-350w-indoor/ Power consumption: 1200 W (max) Envelope (L×W×H): 483 x 88 x 322 mm / 19” Standard, 2U height Mass: 11000 g Operating temperature: 10 °C Frequency: 3000 MHz TX power: 349.945 W ## CW/PW LDMOS UHF SSPA 1.25kW Indoor — TTI Norte [radios] https://newspacemarket.com/products/cw-pw-ldmos-uhf-sspa-1-25kw-indoor/ Power consumption: 1200 W (max) Envelope (L×W×H): 483 x 88 x 322 mm Mass: 11000 g Operating temperature: 10 °C Frequency: 3000 MHz TX power: 349.945 W ## CW LDMOS UHF SSPA 500W Indoor — TTI Norte [radios] https://newspacemarket.com/products/cw-ldmos-uhf-sspa-500w-indoor/ Power consumption: 2500 W (max) Envelope (L×W×H): 483 x 176 x 557 mm Mass: 25000 g Operating temperature: 10 °C Frequency: 200 MHz ## GaN C SSPA/BUC 800W STANDALONE – Indoor — TTI Norte [radios] https://newspacemarket.com/products/gan-c-sspa-buc-800w-standalone-indoor/ TX power: 800 W TX power: 630.957 W @ (variant 2) Supply voltage: 90-264 Power consumption: 3000 W (max) Frequency: 950-1525 MHz Frequency: 5850-6425 MHz @ (variant 2) Frequency: 4900 MHz Envelope (L×W×H): 483 x 266 x 518 mm (RF unit 6RU panel height) Mass: 35000 g ## Triad THPR1060 Range Enhanced Silvus StreamCaster Radio System — Triad RF Systems [radios] https://newspacemarket.com/products/triad-thpr1060-range-enhanced-silvus-streamcaster-radio-system/ Frequency: 2200-2500 MHz Power consumption: 50 W Power consumption: 10 W @ (variant 2) Operating temperature: -40-55 °C Envelope (L×W×H): 9.21 x 5.77 x 5.35 in (233.93 x 146.55 x 135.89 mm) Connector: TNC-F Connector: 801-011-07M10-2PA @ (variant 2) Connector: 801-011-07M13-37PA @ (variant 3) ## VILSA XDL X-Band Downlink Transmitter — Anywaves [radios] https://newspacemarket.com/products/vilsa-xdl-x-band-downlink-transmitter/ Envelope (L×W×H): ≈ 1,375 g / 88 × 55 × 210 mm Envelope (L×W×H): ≈ 400 g / 180 × 32 × 120 mm @ (variant 2) ## RIGEL — Cassiopeia Space Systems [radios] https://newspacemarket.com/products/rigel/ Envelope (L×W×H): 45 cm Power consumption: 280 W Operating temperature: -40 °C Frequency band: X @ TX Frequency: 7900-8400 MHz @ TX Frequency band: X @ RX Frequency: 7250-7750 MHz @ RX Frequency band: Ku @ TX (variant 2) Frequency: 13750-14500 MHz @ TX (variant 2) Frequency band: Ku @ RX (variant 2) Frequency: 10700-12750 MHz @ RX (variant 2) Frequency band: Ka @ TX (variant 3) Frequency: 29000-31000 MHz @ TX (variant 3) Frequency band: Ka @ RX (variant 3) Frequency: 19200-21200 MHz @ RX (variant 3) Mass: 55000 g Operating temperature: -40-60 °C ## S-BAND TRANSCEIVER — Alén Space [radios] https://newspacemarket.com/products/s-band-transceiver/ Modulation: BPSK Data rate: 2000 kbps ## piAIS/FM (Flight Model) — SkyFox Labs s.r.o. [radios] https://newspacemarket.com/products/piais-fm-flight-model/ Envelope (L×W×H): 76x53x12 mm Mass: 55 g ## piADSB-NG/FM (Flight Model) — SkyFox Labs s.r.o. [radios] https://newspacemarket.com/products/piadsb-ng-fm-flight-model/ TRL: 9 Envelope (L×W×H): 98x82.6x12.5 mm Connector: PicoBlade™ 1.25 6P Mass: 124 g ## X/S-Band High-Speed LEO Radio — Akash Systems [radios] https://newspacemarket.com/products/x-s-band-high-speed-leo-radio/ Data rate: 650000 kbps Frequency band: 120 Frequency: 8000-8400 MHz Frequency: 2000-2100 MHz @ (variant 2) TX power: 2-5 W ## SKIF-D — ISS Reshetnev [radios] https://newspacemarket.com/products/skif-d/ Power consumption: 170 W Mass: 148000 g Design lifetime: 3 years ## Angosat-2 — ISS Reshetnev [radios] https://newspacemarket.com/products/angosat-2/ Power consumption: 4400 W Mass: 1875000 g Design lifetime: 15 years ## Express-AMU7 — ISS Reshetnev [radios] https://newspacemarket.com/products/express-amu7/ Power consumption: 6300 W Mass: 1976000 g Design lifetime: 15 years ## Express-80 — ISS Reshetnev [radios] https://newspacemarket.com/products/express-80/ Power consumption: 6300 W Mass: 2101000 g Design lifetime: 15 years ## Express-103 — ISS Reshetnev [radios] https://newspacemarket.com/products/express-103/ Power consumption: 6300 W Mass: 2267000 g Design lifetime: 15 years ## Express-AM8 — ISS Reshetnev [radios] https://newspacemarket.com/products/express-am8/ Power consumption: 5880 W Mass: 2100000 g Design lifetime: 15 years ## Yamal-401 — ISS Reshetnev [radios] https://newspacemarket.com/products/yamal-401-2/ Power consumption: 16800 W Mass: 2976000 g Design lifetime: 14 years ## Express-AM6 — ISS Reshetnev [radios] https://newspacemarket.com/products/express-am6/ Power consumption: 16200 W Mass: 3360000 g Design lifetime: 15 years ## KazSat-3 — ISS Reshetnev [radios] https://newspacemarket.com/products/kazsat-3/ Power consumption: 9320 W Mass: 1740000 g Design lifetime: 15 years ## Express- AT1 — ISS Reshetnev [radios] https://newspacemarket.com/products/express-at1/ Power consumption: 7600 W Mass: 1680000 g Design lifetime: 15 years ## Express- AT2 — ISS Reshetnev [radios] https://newspacemarket.com/products/express-at2/ Power consumption: 5200 W Mass: 1420000 g Design lifetime: 15 years ## Yamal-300K — ISS Reshetnev [radios] https://newspacemarket.com/products/yamal-300k/ Power consumption: 7600 W Mass: 1870000 g Design lifetime: 14 years ## AMOS-5 — ISS Reshetnev [radios] https://newspacemarket.com/products/amos-5/ Power consumption: 7600 W Mass: 1970000 g Design lifetime: 14 years ## Meridian — ISS Reshetnev [radios] https://newspacemarket.com/products/meridian/ Power consumption: 3200 W Mass: 2100000 g Design lifetime: 7 years ## Express-AM — ISS Reshetnev [radios] https://newspacemarket.com/products/express-am/ Power consumption: 6350 W Mass: 2579000 g Design lifetime: 12 years ## Molniya-3K — ISS Reshetnev [radios] https://newspacemarket.com/products/molniya-3k/ Power consumption: 1470 W Mass: 1700000 g Design lifetime: 5 years ## SESAT — ISS Reshetnev [radios] https://newspacemarket.com/products/sesat/ Power consumption: 5300 W Mass: 2572000 g Design lifetime: 10 years ## Express-A — ISS Reshetnev [radios] https://newspacemarket.com/products/express-a/ Power consumption: 2540 W Mass: 2600000 g Design lifetime: 7 years ## Gonets-D1 — ISS Reshetnev [radios] https://newspacemarket.com/products/gonets-d1/ Power consumption: 100 W Mass: 225000 g Design lifetime: 1.5 years ## Express — ISS Reshetnev [radios] https://newspacemarket.com/products/express/ Power consumption: 2400 W Mass: 2500000 g Design lifetime: 5 years ## Gals — ISS Reshetnev [radios] https://newspacemarket.com/products/gals/ Power consumption: 2400 W Mass: 2500000 g Design lifetime: 5 years ## Gonets-D — ISS Reshetnev [radios] https://newspacemarket.com/products/gonets-d/ Power consumption: 100 W Mass: 225000 g Design lifetime: 1.5 years ## Raduga-1 — ISS Reshetnev [radios] https://newspacemarket.com/products/raduga-1/ Power consumption: 1600 W Mass: 2320000 g Design lifetime: 3 years ## Ekran-M — ISS Reshetnev [radios] https://newspacemarket.com/products/ekran-m/ Power consumption: 1800 W Mass: 2100000 g Design lifetime: 3 years ## ATLAS-X-MINI — Astrolight [radios] https://newspacemarket.com/products/atlas-x-mini/ Power consumption: 3.5 W (min) ## ATLAS-2 — Astrolight [radios] https://newspacemarket.com/products/atlas-2/ TX power: 2 W (max) Data rate: 2500000 kbps Mass: 2300 g ## POLARIS — Astrolight [radios] https://newspacemarket.com/products/polaris/ Power consumption: 200 W Mass: 16000 g ## OGS-2.5 — Astrolight [radios] https://newspacemarket.com/products/ogs-2-5/ Envelope (L×W×H): 355 mm (14 ") Envelope (L×W×H): 508 mm (20 ") @ (variant 2) Modulation: OOK Data rate: 1.25 kbps Frequency band: 10 ## Satellite-mounted X-band transmitter (MTX-540X) — Meisei Electric [radios] https://newspacemarket.com/products/satellite-mounted-x-band-transmitter-mtx-540x/ Data rate: 538000 kbps ## BMCU21 – Ka-Band Upconverter — Bonn Hungary Electronics Ltd. [radios] https://newspacemarket.com/products/bmcu21-ka-band-upconverter/ Frequency: 70 MHz ## BPBC19 – X-band Outdoor 1:1 Redundant Solid State Power Amplifier — Bonn Hungary Electronics Ltd. [radios] https://newspacemarket.com/products/bpbc19-x-band-outdoor-11-redundant-solid-state-power-amplifier/ TX power: 100 W ## BMCD39-channel Ka-band Indoor Tracking Downconverter — Bonn Hungary Electronics Ltd. [radios] https://newspacemarket.com/products/bmcd39-channel-ka-band-indoor-tracking-downconverter/ Frequency: 2940 MHz ## Reaction Wheels RW0 / 4RW0 — NanoAvionics [reaction-wheels] https://newspacemarket.com/products/nanoavionics-reaction-wheels-4rw0/ Flight heritage: 60+ satellites launched, 300+ in production (per nanoavionics.com) ## TensorCMG-10m-S — Tensor Tech [reaction-wheels] https://newspacemarket.com/products/tensor-tech-cmg-10m-s/ Envelope (L×W×H): 54 x 49 x 56 mm3 Power consumption: 1.92 W Mass: 280 g Max torque: 1 mN·m ## TensorCMG-10m — Tensor Tech [reaction-wheels] https://newspacemarket.com/products/tensor-tech-cmg-10m-v/ Envelope (L×W×H): 54 x 49 x 56 mm3 Power consumption: 1.92 W Mass: 280 g Flight heritage: since 2022 ## CMG for SmallSats — Tensor Tech [reaction-wheels] https://newspacemarket.com/products/tensor-tech-cmg-4/ Angular momentum storage: 1 N·m·s Max torque: 3000 mN·m (min) Envelope (L×W×H): 100 x 100 x 120 mm3 Mass: 2500 g (max) ## SSW-110 — SSTL (Surrey Satellite Technology) [reaction-wheels] https://newspacemarket.com/products/sstl-geo-wheel/ Wheel speed: 0.4166 Design lifetime: 15.25 years Operating temperature: -30 °C Survival temperature: -35 °C Supply voltage: 48.5-52.5 Power consumption: 5 W (max) Power consumption: 180 W (max) @ (variant 2) Envelope (L×W×H): Diameter 240 x 95 mm Mass: 5600 g (max) ## RW Series Reaction Wheels — Blue Canyon Technologies [reaction-wheels] https://newspacemarket.com/products/bct-rw-series-reaction-wheels/ Flight heritage: Extensive — NASA MarCO, TROPICS, HaloSat, Starling, DoD missions ## RWP Series Reaction Wheels — Blue Canyon Technologies [reaction-wheels] https://newspacemarket.com/products/bct-rwp-series-reaction-wheels/ Flight heritage: BCT Saturn and Venus mission heritage ## Momentum Control Systems — Honeywell Aerospace [reaction-wheels] https://newspacemarket.com/products/honeywell-m50-control-moment-gyroscope/ Power consumption: 120 W ## Reaction Wheels — Gimbal Space [reaction-wheels] https://newspacemarket.com/products/gimbalspace-reaction-wheels/ Envelope (L×W×H): Multiple sizes ## TELDIX® Space Wheels — Collins Aerospace [reaction-wheels] https://newspacemarket.com/products/collins-rdr-68-3-momentum-reaction-wheel/ Mass: 7600 g Power consumption: 20 W Flight heritage: Part of TELDIX wheel family, 2,900+ cumulative in-orbit years ## 15 mNms Momentum Wheel — Shenzhen MagicCubeSat Technology (MCS) [reaction-wheels] https://newspacemarket.com/products/mcs-momentum-wheel-15-mnms/ Angular momentum storage: 0.015 N·m·s ## 50 mNms Momentum Wheel — Shenzhen MagicCubeSat Technology (MCS) [reaction-wheels] https://newspacemarket.com/products/mcs-momentum-wheel-50-mnms/ Angular momentum storage: 0.05 N·m·s ## 340 mNms Momentum Wheel — Shenzhen MagicCubeSat Technology (MCS) [reaction-wheels] https://newspacemarket.com/products/mcs-momentum-wheel-340-mnms/ Angular momentum storage: 0.34 N·m·s ## Solar Array Mechanical Device — Glavkosmos [sadm] https://newspacemarket.com/products/solar-array-mechanical-device/ Design lifetime: 15 years Lead time: 18 Mass: 700-900 g ## Solar Array Drive Mechanism. Type 1 — Glavkosmos [sadm] https://newspacemarket.com/products/solar-array-drive-mechanism-type-1/ Design lifetime: 15.25 years Lead time: 12 Flight heritage: Express-AM5, Express-AM6 Envelope (L×W×H): 210 × 230 × 275 mm Mass: 5300 g ## Solar Array Drive Mechanism. Type 2 — Glavkosmos [sadm] https://newspacemarket.com/products/solar-array-drive-mechanism-type-2/ Design lifetime: 13.5 years Lead time: 15 Envelope (L×W×H): 240 × 160 × 300 mm Design lifetime: 10 years @ (variant 2) ## Solar Array Drive Mechanism. Type 3 — Glavkosmos [sadm] https://newspacemarket.com/products/solar-array-drive-mechanism-type-3/ Design lifetime: 7 years Lead time: 12 Envelope (L×W×H): 941 × 355 × 460 mm Mass: 22700 g ## Solar Array Drive Mechanism. Type 4 — Glavkosmos [sadm] https://newspacemarket.com/products/solar-array-drive-mechanism-type-4/ Envelope (L×W×H): 156 × 260 × 223 mm Mass: 4300 g Design lifetime: 15.5 years Lead time: 12 ## Solar Array Drive Mechanism. Type 5 — Glavkosmos [sadm] https://newspacemarket.com/products/solar-array-drive-mechanism-type-5/ Design lifetime: 10 years Lead time: 12 Envelope (L×W×H): 270 × 156 × 281 mm Mass: 4500 g ## Solar Array Drive Mechanism. Type 6 — Glavkosmos [sadm] https://newspacemarket.com/products/solar-array-drive-mechanism-type-6/ Design lifetime: 10 years Lead time: 12 Envelope (L×W×H): 152 × 200 × 290 mm Mass: 4600 g ## NANOeps-AMPPT — SkyLabs d.o.o. [sadm] https://newspacemarket.com/products/skylabs-nanoeps-amppt/ TRL: 9 ## SpaceTech SADA 44/22 (Solar Array Drive Assembly) — SpaceTech GmbH [sadm] https://newspacemarket.com/products/spacetech-sada-44-22/ Supply voltage: 22 Connector: DSUB-37 pins ## IMT µSADA Miniaturized Solar Array Drive Assembly — IMT (Ingegneria Marketing Technologies) [sadm] https://newspacemarket.com/products/imt-microsada-solar-array-drive-assembly/ Power consumption: 118 W Supply voltage: 31-54 Power consumption: 0.5 W @ (variant 2) Mass: 250 g Envelope (L×W×H): 88 x 101 x 15 mm Mass: 1190 g @ (variant 2) Envelope (L×W×H): 710 x 324 x 11 mm @ (variant 2) ## VLCI Receipt/Transmit Center-LSN — Glavkosmos [sdr-modems] https://newspacemarket.com/products/vlci-receipt-transmit-center-lsn/ Design lifetime: 3 years Lead time: 8 Mass: 2 g Operating temperature: -40-85 °C ## NSR-SDR-S/S — Vulcan Wireless [sdr-modems] https://newspacemarket.com/products/vulcan-nsr-sdr-s-s/ Design lifetime: 5 years Protocols / waveforms: NASA NEN, TDRS-MA, USB, coherent turnaround/ranging, PROXIMITY-1, crosslink ## NSR-SDR-X/S HP — Vulcan Wireless [sdr-modems] https://newspacemarket.com/products/vulcan-nsr-sdr-x-s-hp/ Power consumption: 10 W (min) Design lifetime: 5 years Protocols / waveforms: DVB-S2 ## NSR-SDR-MUOS — Vulcan Wireless [sdr-modems] https://newspacemarket.com/products/vulcan-nsr-sdr-muos/ Design lifetime: 5 years Protocols / waveforms: Spread-spectrum anti-jam MUOS; legacy UHF SATCOM ## ThumbNet N3 SDR Receiver — ThumbSat [sdr-modems] https://newspacemarket.com/products/thumbsat-thumbnet-n3-sdr-receiver/ Envelope (L×W×H): 6 x 4 cm Connector: Mini-USB (host), F-type RF (antenna) ## ECHO Software Defined Radio (SDR) — TALOS GmbH [sdr-modems] https://newspacemarket.com/products/talos-echo-sdr/ Flight heritage: RAVEN microsatellite, TALOS-I constellation (ICARUS 2.0) ## Sx3099 SDR ASIC — MDA Space [sdr-modems] https://newspacemarket.com/products/sx3099-sdr-asic/ Protocols / waveforms: up to 8 (~1 Gsps aggregate) ## μSDR-C™ Software Defined Radio — Voyager Technologies [sdr-modems] https://newspacemarket.com/products/spacemicro-usdr-c-software-defined-radio/ Flight heritage: Space Micro (now Voyager Technologies) ## NanoCom™ Software Defined Radio — Voyager Technologies [sdr-modems] https://newspacemarket.com/products/spacemicro-nanocom-software-defined-radio/ Protocols / waveforms: Network protocols supported ## NanoCom-500™ Software Defined Radio — Voyager Technologies [sdr-modems] https://newspacemarket.com/products/spacemicro-nanocom-500-software-defined-radio/ Protocols / waveforms: Network protocols supported ## SDR-1001 — CesiumAstro [sdr-modems] https://newspacemarket.com/products/sdr-1001-software-defined-radio/ TRL: 9 ## VILSA Software Defined Radio — Anywaves [sdr-modems] https://newspacemarket.com/products/vilsa-software-defined-radio/ Radiation tolerance (TID): 18 krad Flight heritage: Based on previous-generation SDR with in-flight heritage (e.g., Juventas radar payload on ESA Hera mission) ## XLink SDR Transceiver — IQ Spacecom [sdr-modems] https://newspacemarket.com/products/iq-spacecom-xlink-sdr/ Protocols / waveforms: CCSDS, DVB-S2 ## XLink — IQ Spacecom [sdr-modems] https://newspacemarket.com/products/iq-spacecom-xlink-l/ Flight heritage: Flight proven design (TRL 9) Protocols / waveforms: CCSDS and DVB-S2 ## Comprehensive TT&C Baseband — Emposat Co., Ltd. [sdr-modems] https://newspacemarket.com/products/comprehensive-ttc-baseband/ Protocols / waveforms: TCP, UDP ## VILSA SDR — Software Defined Radio Payload — Anywaves [sdr-modems] https://newspacemarket.com/products/vilsa-sdr-software-defined-radio-payload/ Mass: 300 g (max) Power consumption: 10 W (max) ## STARLIGHT Optical Modem and Amplifier — Mbryonics [sdr-modems] https://newspacemarket.com/products/mbryonics-starlight-optical-modem/ Mass: 3500 g (max) Mass: 4000 g (max) @ (variant 2) Mass: 14000 g (max) @ (variant 3) ## BlackFish Airborne SIGINT System — Horizon Technologies [sdr-modems] https://newspacemarket.com/products/horizontech-blackfish-sigint/ Mass: 4400 g ## STX3 OEM Satellite Modem — Globalstar (C-3 next-gen) [sdr-modems] https://newspacemarket.com/products/globalstar-stx3-oem-modem/ Envelope (L×W×H): 28.70 x 20.57 mm ## Eagle-1 Optical Modem — CELESTIA Satellite Test & Simulation [sdr-modems] https://newspacemarket.com/products/celestiasts-eagle1-optical-modem/ Flight heritage: EAGLE-1 QKD satellite (validated) ## StarCom — Mbryonics [sdr-modems] https://newspacemarket.com/products/starcom/ Flight heritage: Selected by DARPA, ESA, SpeQtral, Airbus Defence and Space and European Defence Agency. ## StarLight Modem, Amplifiers and Antenna Control Unit — Mbryonics [sdr-modems] https://newspacemarket.com/products/starlight/ Mass: 3500 g (max) Mass: 4000 g (max) @ (variant 2) Mass: 14000 g (max) @ (variant 3) ## SL-400X Mobile TV Integrated Receiver — Saankhya Labs [sdr-modems] https://newspacemarket.com/products/saankhya-labs-sl-400x-mobile-tv-integrated-receiver/ Envelope (L×W×H): 2 K/4 K/8 K/16 K Operating temperature: 0-85 °C Envelope (L×W×H): 7 x 11 mm @ (variant 2) ## Q8 SDR Dock Daughterboard — Xiphos Technologies [sdr-modems] https://newspacemarket.com/products/xiphos-q8-sdr-dock/ Envelope (L×W×H): 80 x 80 x 34.7 mm (with Q8 installed) Supply voltage: 5 ## Q8J SDR Daughterboard — Xiphos Technologies [sdr-modems] https://newspacemarket.com/products/xiphos-q8j-sdr/ Envelope (L×W×H): 80 x 106 x 23.5 mm (with Q8J) Supply voltage: 6-8.4 ## Q8RF Gen 1 RFSoC Processor — Xiphos Technologies [sdr-modems] https://newspacemarket.com/products/xiphos-q8rf/ Envelope (L×W×H): 100 x 100 x 20 mm Mass: 200 g Power consumption: 20-30 W Supply voltage: 5-9 Operating temperature: -40-60 °C Radiation tolerance (TID): 30 krad ## HOCSAI Multi-Protocol Optical Modem — WARPSPACE Inc. [sdr-modems] https://newspacemarket.com/products/warpspace-hocsai-optical-modem/ Protocols / waveforms: Multi-standard (interoperable across different optical terminal vendors) ## SCR-104 S-Band Software-defined Compact Radio — Innoflight [sdr-modems] https://newspacemarket.com/products/innoflight-scr-104-s-band-radio/ TRL: 9 Flight heritage: Since 2019 ## SCR-106 / SCR-106HDR X-Band Software-defined Compact Radio — Innoflight [sdr-modems] https://newspacemarket.com/products/innoflight-scr-106-x-band-radio/ TRL: 9 Flight heritage: Since 2022 ## SCR-208 Medusa Ka-Band Software-defined Compact Radio — Innoflight [sdr-modems] https://newspacemarket.com/products/innoflight-scr-208-ka-band-radio/ Envelope (L×W×H): 197 x 150 x 82 mm Mass: 2720 g Power consumption: 80 W TRL: 5 ## AIS PAYLOAD — Alén Space [sdr-modems] https://newspacemarket.com/products/ais-payload/ TRL: 9 ## ADS-B PAYLOAD — Alén Space [sdr-modems] https://newspacemarket.com/products/ads-b-payload/ TRL: 9 ## Hasten — Remos Space Systems AB [sdr-modems] https://newspacemarket.com/products/hasten/ Protocols / waveforms: CCSDS CADU, DVB-S2(x) Envelope (L×W×H): 4U Mass: 16000 g Envelope (L×W×H): 177x482x555 mm @ (variant 2) Operating temperature: 10-40 °C ## EXOtube — Exolaunch [separation-systems] https://newspacemarket.com/products/exolaunch-exotube/ Mass: 1000000 g ## EXOport — Exolaunch [separation-systems] https://newspacemarket.com/products/exolaunch-exoport/ Flight heritage: 8 missions, 20 EXOports flown, since Jan 2021 Export status: ITAR-FREE ## EXObox — Exolaunch [separation-systems] https://newspacemarket.com/products/exolaunch-exobox/ Flight heritage: Since 2017, 7 missions, 132 smallsats ## Deep Space Deployer — ISISPACE Group [separation-systems] https://newspacemarket.com/products/isispace-deep-space-deployer/ Envelope (L×W×H): 6UXL Mass: 4900 g Envelope (L×W×H): 272 x 156.7 x 432.4 mm @ (variant 2) Envelope (L×W×H): 272 x 206.77 x 555.05 mm @ (variant 3) Flight heritage: ESA Hera mission ## Tulip — ISISPACE Group [separation-systems] https://newspacemarket.com/products/isispace-tulip/ Mass: 70100 g Envelope (L×W×H): ~2 m ## Pyrolock — Glavkosmos [separation-systems] https://newspacemarket.com/products/pyrolock/ Design lifetime: 6 years Operating temperature: -90-100 °C Mass: 370 g ## Release Device (electromechanical, shock-free). Type 1 — Glavkosmos [separation-systems] https://newspacemarket.com/products/release-device-electromechanical-shock-free-type-1/ Design lifetime: 8 years Lead time: 4 Operating temperature: -100-100 °C Envelope (L×W×H): 41 × 41, 5 × 41 mm Mass: 80 g ## Release Device (electromechanical, shock-free). Type 2 — Glavkosmos [separation-systems] https://newspacemarket.com/products/release-device-electromechanical-shock-free-type-2/ Design lifetime: 9 years Lead time: 4 Operating temperature: -100-100 °C Envelope (L×W×H): ø38 x41.7 mm Mass: 50 g ## Separation Device Clamp Band — Glavkosmos [separation-systems] https://newspacemarket.com/products/separation-device-clamp-band/ Design lifetime: 6 years Lead time: 4 Operating temperature: -100-100 °C Cycles / reuses: 10 Mass: 500 g ## Spacecraft Separation Device — Glavkosmos [separation-systems] https://newspacemarket.com/products/spacecraft-separation-device/ Design lifetime: 6 years Lead time: 12 Mass: 10500-15000 g Mass: 1600000-3400000 g @ (variant 2) ## Microsatellite Separation System (M3S) — ISISPACE Group [separation-systems] https://newspacemarket.com/products/isispace-microsatellite-separation-system/ Mass: 120000 g ## Docking Plate — Astroscale US [separation-systems] https://newspacemarket.com/products/astroscale-docking-plate/ Flight heritage: Validated on ELSA-d mission (2021) ## HDRM REACT – Hold Down & Release Mechanisms (5KN, 15KN, 35KN) — Arquimea [separation-systems] https://newspacemarket.com/products/arquimea-hdrm-react/ Operating temperature: -90 °C ## Hold-Down & Release Mechanisms (HDRM) — Astronika [separation-systems] https://newspacemarket.com/products/astronika-hdrm/ Flight heritage: NASA InSight (HP3 Mole), ESA Hera ## EBAD TiNi frangibolt — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/ebad-tini-frangibolt/ Lead time: 24 ## EBAD TiNi™ ejector — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/ebad-tini-ejector/ Envelope (L×W×H): 4-40 to 3/8”-24 ## EBAD TiNi™ Pin Puller — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/ebad-tini-pin-puller/ Envelope (L×W×H): Five Flight heritage: Mars Global Surveyor spacecraft (November 1996) and numerous other space applications ## Micro Release Nut (uD3RN) — Dcubed [separation-systems] https://newspacemarket.com/products/micro-release-nut-ud3rn/ TRL: 9 Cycles / reuses: 40-100 Lead time: 10-12 Preload / holding force: 4 kN Envelope (L×W×H): 25 x 25 x 25 mm Mass: 38 g ## Nano Pin Puller (nD3PP) — Dcubed [separation-systems] https://newspacemarket.com/products/nano-pin-puller-nd3pp/ TRL: 9 Lead time: 6-8 Envelope (L×W×H): 17 x 17 x 17 mm Mass: 12 g Mass: 25 g @ (variant 2) ## Nano Release Nut (nD3RN) — Dcubed [separation-systems] https://newspacemarket.com/products/nano-release-nut-nd3rn/ TRL: 9 Preload / holding force: 0.25-0.38 kN Envelope (L×W×H): 17 x 17 x 17 mm Mass: 12 g Mass: 25 g @ (variant 2) ## Nano SmartPack Release Nut (nD3SP) — Dcubed [separation-systems] https://newspacemarket.com/products/nano-smartpack-release-nut-nd3sp/ TRL: 9 Lead time: 8-10 Preload / holding force: 0.2 kN (min) Envelope (L×W×H): 74 x 35 x 4 mm Mass: 27 g ## Micro Pin Puller (uD3PP) — Dcubed [separation-systems] https://newspacemarket.com/products/micro-pin-puller-ud3pp/ Lead time: 10-12 Envelope (L×W×H): 25 x 50 x 41 mm Mass: 75-85 g ## REAC-353 V2 EX 35kN SMARQ Release Actuator — Arquimea [separation-systems] https://newspacemarket.com/products/reac-353-v2-ex-35kn-smarq-release-actuator/ Mass: 367 g Supply voltage: 25 Release shock: 1300 (max) Operating temperature: -90-125 °C ## REAC-153 V2 SX 15kN SMARQ Release Actuator — Arquimea [separation-systems] https://newspacemarket.com/products/reac-153-v2-sx-15kn-smarq-release-actuator/ Mass: 268 g Supply voltage: 25 Release shock: 1300 (max) Operating temperature: -90-125 °C ## REAC-053 V2 SX 5kN SMARQ Release Actuator — Arquimea [separation-systems] https://newspacemarket.com/products/reac-053-v2-sx-5kn-smarq-release-actuator/ Mass: 226-230 g Supply voltage: 25 Release shock: 1000 (max) Operating temperature: -90-125 °C ## REAC-053 V2 SX 5kN Nitinol Release Actuator — Arquimea [separation-systems] https://newspacemarket.com/products/reac-053-v2-sx-5kn-nitinol-release-actuator/ Mass: 226-230 g Operating temperature: -90-65 °C ## REAC-153 V2 SX 15kN Nitinol Release Actuator — Arquimea [separation-systems] https://newspacemarket.com/products/reac-153-v2-sx-15kn-nitinol-release-actuator/ Mass: 300 g Supply voltage: 20 Operating temperature: -90-65 °C ## REAC-353 V2 35kN Nitinol Release Actuator — Arquimea [separation-systems] https://newspacemarket.com/products/reac-353-v2-35kn-nitinol-release-actuator/ Release shock: 1300 (max) Operating temperature: -90-65 °C ## Hold Down Release Mechanism (HDRM) — Sierra Space [separation-systems] https://newspacemarket.com/products/sierra-hdrm-hold-down-release-mechanism/ Cycles / reuses: 1 (max) ## Redwire LoFF Rideshare Adapter — Redwire Corporation [separation-systems] https://newspacemarket.com/products/redwire-loff-rideshare-adapter/ Flight heritage: Spaceflight SSO-A ## Release Nuts — Dcubed [separation-systems] https://newspacemarket.com/products/dcubed-release-nut/ Envelope (L×W×H): 74x35x4 mm / 2.91x1.38x0.16 in TRL: 9 Envelope (L×W×H): 17x17x17 mm / 0.67x0.67x0.67 in @ (variant 2) TRL: 9 @ (variant 2) Envelope (L×W×H): 25x25x25 mm / 0.9x0.9x0.9 in @ (variant 3) TRL: 9 @ (variant 3) Envelope (L×W×H): 25x25x25 mm / 0.9x0.9x0.9 in @ (variant 4) TRL: 8 @ (variant 4) Envelope (L×W×H): Ø 56 x 55 mm / Ø 2.204 x 2.165 in @ (variant 5) TRL: 8 @ (variant 5) ## Pin Pullers — Dcubed [separation-systems] https://newspacemarket.com/products/dcubed-pin-puller/ Envelope (L×W×H): Ø28x52 mm / Ø1.1x20.27 in Mass: 85 g TRL: 9 Envelope (L×W×H): 17x17x17 mm / 0.67x0.67x0.67 in @ (variant 2) TRL: 9 @ (variant 2) ## TRIGGY — Shape Memory Alloy Breakable Fastener — Nimesis Technology [separation-systems] https://newspacemarket.com/products/nimesis-triggy-sma-breakable-fastener/ Envelope (L×W×H): M2 to M12 ## GRIPPER — SMA Hold-Down Release Actuator — Nimesis Technology [separation-systems] https://newspacemarket.com/products/nimesis-gripper-sma-hold-down-release-actuator/ Preload / holding force: 1.5 kN ## SATLATCH — Shock-Free Deployment and Latching Mechanism — Nimesis Technology [separation-systems] https://newspacemarket.com/products/nimesis-satlatch-deployment-mechanism/ TRL: 8 Operating temperature: -120 °C ## MURPHY — Re-entry Triggered Dismantling Fastener — Nimesis Technology [separation-systems] https://newspacemarket.com/products/nimesis-murphy-reentry-dismantling-fastener/ TRL: 7 ## LARA — SMA Release Nut for Launch Vehicle Stage Separation — Nimesis Technology [separation-systems] https://newspacemarket.com/products/nimesis-lara-sma-release-nut/ TRL: 4 Release time: 100 ms (max) Operating temperature: -120 °C ## HARPER — Ultra-Flat SMA Locking Actuator for Launchers — Nimesis Technology [separation-systems] https://newspacemarket.com/products/nimesis-harper-ultra-flat-locking-actuator/ TRL: 5 ## A-Deck Adapter System — Adaptive Launch Solutions [separation-systems] https://newspacemarket.com/products/als-adeck-adapter-system/ TRL: 8 ## Mark II Motorized Lightband (MLB) — Planetary Systems Corp (Rocket Lab) [separation-systems] https://newspacemarket.com/products/psc-rocket-lab-mark-ii-motorized-lightband/ Envelope (L×W×H): 12 to 60 fasteners depending on diameter Preload / holding force: 1200 kN Flight heritage: 100+ on-orbit separations, 100% mission success ## Advanced Lightband (ALB) — Planetary Systems Corp (Rocket Lab) [separation-systems] https://newspacemarket.com/products/psc-rocket-lab-advanced-lightband/ Envelope (L×W×H): 12 to 36 fasteners depending on diameter Flight heritage: 100% on-orbit separation success; thousands of qualification tests ## FuseBlox Small Satellite Docking Mechanism — SpaceWorks Enterprises [separation-systems] https://newspacemarket.com/products/spaceworks-fuseblox-docking/ TRL: 6 Flight heritage: DARPA and AFRL sponsored development ## NPSCuL (NPS CubeSat Launcher) — Naval Postgraduate School [separation-systems] https://newspacemarket.com/products/npscul-nps-cubesat-launcher-12353/ Flight heritage: OUTSat, GEMSat missions ## NEA Hold Down Release Mechanisms — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/ebad-nea-hold-down-release-mechanisms/ Flight heritage: 20+ years: A2100, Spacebus, Eurostar, LS-1300, JWST ## Spacecraft Dispensing Systems — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/ebad-spacecraft-dispensing-systems/ Flight heritage: 60+ years serving satellite and launch vehicle markets ## Payload Separation and Release Systems — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/ebad-payload-separation-release-systems/ Flight heritage: 50+ years, invention of the Linear Shaped Charge ## Deep Space Deployer (DSD) — Innovative Space Logistics [separation-systems] https://newspacemarket.com/products/deep-space-deployer-dsd-1478/ Mass: 4900 g Envelope (L×W×H): 272 x 156.7 x 432.4 mm Envelope (L×W×H): 272 x 206.77 x 555.05 mm @ (variant 2) Mass: 12500 g @ (variant 2) ## TiNi MINI Frangibolt FD04 Actuator — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/ebad-fd04/ Envelope (L×W×H): #4 Mass: 10 g Power consumption: 9 W Supply voltage: 6-8 Operating temperature: -50 °C ## TiNi Flat Pack FP50 Frangibolt Actuator — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/ebad-fp50/ Power consumption: 1.25 W Operating temperature: -65 °C ## TiNi ERM E250 Ejector Release Mechanism — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/ebad-e250/ Envelope (L×W×H): .138 in-32 ## TiNi ERM E500 Ejector Release Mechanism — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/ebad-e500/ Envelope (L×W×H): .164 in-32 ## TiNi ERM E1000 Ejector Release Mechanism — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/ebad-e1000/ Envelope (L×W×H): .190 in-32 ## TiNi ERM E2000 Ejector Release Mechanism — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/ebad-e2000/ Envelope (L×W×H): .250 in-28 ## TiNi ERM E4000 Ejector Release Mechanism — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/ebad-e4000/ Envelope (L×W×H): .375 in-24 ## TiNi Frangibolt Actuator FC2 — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/ebad-fc2/ Envelope (L×W×H): #8 Mass: 25 g Power consumption: 25 W Supply voltage: 22-36 ## TiNi Frangibolt Actuator FC3 — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/ebad-fc3/ Envelope (L×W×H): #10 Mass: 40 g Power consumption: 49 W Supply voltage: 22-36 ## TiNi Frangibolt Actuator FC4 — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/ebad-fc4/ Envelope (L×W×H): 1/4" Mass: 55 g Power consumption: 80 W Supply voltage: 22-36 ## TiNi Frangibolt Actuator FC6 — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/ebad-fc6/ Envelope (L×W×H): 3/8" Mass: 110 g Power consumption: 111 W Supply voltage: 95-105 ## TiNi Frangibolt Actuator FC8 — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/ebad-fc8/ Envelope (L×W×H): 1/2" Mass: 175 g Power consumption: 112 W Supply voltage: 22-36 ## TiNi Frangibolt Actuator FB12 — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/ebad-fb12/ Envelope (L×W×H): 1" Mass: 350 g Power consumption: 143 W Supply voltage: 95-105 ## NEA PRM 9103A Payload Release Module — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/ebad-prm-9103a/ Release shock: 500 (max) Release time: 50 ms (max) Operating temperature: -90 °C ## NEA PRM 9104A Payload Release Module — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/ebad-prm-9104a/ Release shock: 300 (max) Release time: 40 ms (max) Operating temperature: -90 °C ## NEA® 24″ Payload Release Ring (PRR-24) — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/ebad-prr-24/ Release shock: 300 (max) Release time: 40 ms (max) Operating temperature: -90 °C ## EBAD NEA1120-05 Pin Puller — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/ebad-nea1120-05/ Random vibration: 29.4 ## EBAD NEA® Model 2545 Pin Puller — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/ebad-2545/ Release time: 50 ms (max) Operating temperature: -101 °C Mass: 182 g ## NEA 1120-05 Pin Puller — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/ebad-1120-05/ Release shock: 1000 (max) Random vibration: 29.4 ## NEA Model 9040 Miniature Hold Down & Release Mechanism (HDRM) — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/nea-model-9040-miniature-hold-down-release-mechanism-hdrm/ Release time: 50 ms (max) Operating temperature: -60 °C Mass: 13.6 g (max) ## NEA Model 9100 Hold Down & Release Mechanism — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/nea-model-9100-hold-down-release-mechanism/ Release time: 50 ms (max) ## NEA® Model 9102G Hold Down & Release Mechanism (HDRM) — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/nea-model-9102g-hold-down-release-mechanism-hdrm/ Preload / holding force: 4000 kN Release time: 50 ms (max) Operating temperature: -135 °C Mass: 130 g Release shock: 4000 ## NEA® Model 9103 Hold Down & Release Mechanism (HDRM) — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/nea-model-9103-hold-down-release-mechanism-hdrm/ Release time: 50 ms (max) Operating temperature: -135 °C Mass: 200 g ## NEA® Model 9104 Hold Down & Release Mechanism (HDRM) — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/nea-model-9104-hold-down-release-mechanism-hdrm/ Release time: 50 ms (max) Operating temperature: -135 °C ## NEA Model 9106B Hold Down & Release Mechanism (HDRM) — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/nea-model-9106b-hold-down-release-mechanism-hdrm/ Release time: 50 ms (max) Operating temperature: -135 °C Mass: 700 g ## NEA® Model 9107 Hold Down & Release Mechanism (HDRM) — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/nea-model-9107-hold-down-release-mechanism-hdrm/ Release time: 50 ms (max) Operating temperature: -135 °C Mass: 2155 g ## NEA® Model 9108 Hold Down & Release Mechanism (HDRM) — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/nea-model-9108-hold-down-release-mechanism-hdrm/ Release time: 200 ms (max) Operating temperature: -135 °C Mass: 3855 g ## NEA® Payload Release Module PRM 9103A — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/nea-payload-release-module-prm-9103a/ Release shock: 500 (max) Release time: 50 ms (max) Operating temperature: -90 °C ## NEA® Payload Release Module PRM 9104A — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/nea-payload-release-module-prm-9104a/ Release shock: 300 (max) Release time: 40 ms (max) Operating temperature: -90 °C ## NEA® 8″ Payload Release Ring (PRR-8) — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/nea-8-payload-release-ring-prr-8/ Release shock: 300 (max) Release time: 40 ms Operating temperature: -90 °C ## NEA® 15″ Payload Release Ring (PRR-15) — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/nea-15-payload-release-ring-prr-15/ Release shock: 300 (max) Release time: 40 ms (max) Operating temperature: -40 °C ## NEA® Model 2545 Pin Puller — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/nea-model-2545-pin-puller/ Release time: 50 ms (max) Operating temperature: -101 °C ## TiNi Flat Pack FP50 Miniature Hold-Down Release Mechanism — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/tini-flat-pack-fp50-miniature-hold-down-release-mechanism/ Power consumption: 1.25 W Operating temperature: -65 °C ## Maverick NLAS Ruggedized 6U Dispenser — Maverick Space Systems [separation-systems] https://newspacemarket.com/products/maverick-nlas-dispenser-6u/ Flight heritage: NASA Ames NLAS ## ARTICA — NPC Spacemind [separation-systems] https://newspacemarket.com/products/artica/ Mass: 210 g Connector: Micro-DSUB 9 Power consumption: 6 W ## SpaceTech Deployable Solar Arrays — SpaceTech GmbH [solar-panels] https://newspacemarket.com/products/spacetech-solar-arrays/ Form factor: < 0.5 m² (XS) to > 6 m² (XL) per panel Deployable: Controlled, unsynchronized multi-hinge deployment using standardized C-spring hinges Random vibration: 148 Random vibration: 20 @ (variant 2) Mass: 3000 g (min) Mass: 4000 g (max) @ depending on the influence of the deployment mechanisms Output power (BOL): 5 W (max) Cell efficiency: 85 (max) Flight heritage: More than 300 solar arrays in orbit – 100 % success rate ## Solar Panels 1p Set (QTY 5) — Alba Orbital [solar-panels] https://newspacemarket.com/products/solar-panels-1p-set-qty-5-1479/ Lead time: 10-12 Output power (BOL): 0.368 W Supply voltage: 13.14 (nominal) Form factor: pocketqubesat panel ## 6U Deployable Solar Array — EnduroSat [solar-panels] https://newspacemarket.com/products/endurosat-6u-deployable-solar-array/ Cell efficiency: 29 ## 3U Solar Panel — EnduroSat [solar-panels] https://newspacemarket.com/products/endurosat-3u-solar-panel/ Cell efficiency: 30 Output power (BOL): 8.4 W Supply voltage: 17.5 Mass: 147 g ## SXC-SG-03 GaAs Solar Panels (Side / End) — SPUTNIX [solar-panels] https://newspacemarket.com/products/sputnix-sxc-sg-03-solar-panels/ Cell efficiency: 28 Envelope (L×W×H): 98 × 82.6 × 8.6 mm (1.7 mm thick without connector) Output power (BOL): 4.7 W ## GaAs Solar Panel with Coils (end edge) — Glavkosmos [solar-panels] https://newspacemarket.com/products/gaas-solar-panel-with-coils-end-edge/ Design lifetime: 1 years Lead time: 5 Envelope (L×W×H): 98 × 82.6 × 1.7 mm Mass: 32 g Supply voltage: 5.3 Output power (BOL): 4.7 W Output power (BOL): 480 W @ (variant 2) Cell efficiency: 28 ## GaAs Solar Panel with Coils (side) — Glavkosmos [solar-panels] https://newspacemarket.com/products/gaas-solar-panel-with-coils-side/ Design lifetime: 1 years Lead time: 5 Flight heritage: SiriusSat-1/2, launched 15 August 2018 Envelope (L×W×H): 98 × 82.6 × 1.7 mm Mass: 34 g Supply voltage: 5.4 Output power (BOL): 4.4 W Output power (BOL): 480 W @ (variant 2) Cell efficiency: 28 ## Nanosatellite Solar Panel — Glavkosmos [solar-panels] https://newspacemarket.com/products/nanosatellite-solar-panel/ Design lifetime: 1 years Lead time: 6 Output power (BOL): 2.1 W ## Si Solar panel with Coils (end edge) — Glavkosmos [solar-panels] https://newspacemarket.com/products/si-solar-panel-with-coils-end-edge/ Design lifetime: 1 years Lead time: 2 Envelope (L×W×H): 98 × 82.6 × 1.7 mm Mass: 32 g Supply voltage: 5.4 Output power (BOL): 4.4 W Output power (BOL): 260 W @ (variant 2) Cell efficiency: 18 ## Si Solar Panel with Coils (side) — Glavkosmos [solar-panels] https://newspacemarket.com/products/si-solar-panel-with-coils-side/ Design lifetime: 1 years Lead time: 2 Envelope (L×W×H): 98 × 82.6 × 1.7 mm Mass: 32 g Supply voltage: 5.4 Output power (BOL): 4.4 W Output power (BOL): 260 W @ (variant 2) Cell efficiency: 18 ## Solar Cell Battery — Glavkosmos [solar-panels] https://newspacemarket.com/products/solar-cell-battery/ Lead time: 2 Supply voltage: 4.5 ## Solar Element GaInP2 / GaAs / Ge — Glavkosmos [solar-panels] https://newspacemarket.com/products/solar-element-gainp2-gaas-ge/ Lead time: 1 Cell efficiency: 28.5 Output power (BOL): 2371 W Output power (BOL): 381 W @ (variant 2) Envelope (L×W×H): 80 × 40 mm ## Satellite Solar Panels — ISISPACE Group [solar-panels] https://newspacemarket.com/products/isispace-satellite-solar-panels/ Form factor: 50 g Mass: 100 g Form factor: 150 g @ (variant 2) Form factor: 300 g @ (variant 3) Mass: 400 g @ (variant 2) Operating temperature: -40-80 °C Cell efficiency: 30 Supply voltage: 2.7 Form factor: 1U, 2U, 3U(XL), 6U(XL), 8U, custom (including deployable) @ (variant 4) ## Titan Bare Module — Ascent Solar Technologies [solar-panels] https://newspacemarket.com/products/ascent-solar-titan-bare-module/ Form factor: 336 mm × 289 mm Form factor: 336 mm × 247 mm @ (variant 2) Cell efficiency: 15.7 Cell efficiency: 17.73 @ (variant 2) Supply voltage: 20 Lead time: 6-8 ## CubeSat HDK Solar Array — Ascent Solar Technologies [solar-panels] https://newspacemarket.com/products/ascent-solar-cubesat-hdk/ Form factor: 0.5U, 1U, 3U, 6U Supply voltage: 28 Flight heritage: TRL 9 (Momentus Vigoride-6, MISSE-10 ISS) Lead time: 6-8 ## Smallsat HDK Solar Array — Ascent Solar Technologies [solar-panels] https://newspacemarket.com/products/ascent-solar-smallsat-hdk/ Supply voltage: 28 Flight heritage: TRL 9 Lead time: 6-8 ## EP-500V HDK Solar Array — Ascent Solar Technologies [solar-panels] https://newspacemarket.com/products/ascent-solar-ep-500v-hdk/ Supply voltage: 500 Lead time: 6-8 ## Space Solar Panels — Spectrolab [solar-panels] https://newspacemarket.com/products/spectrolab-space-solar-panels/ Flight heritage: 500+ spacecraft powered by Spectrolab panels ## Space Solar Arrays — Spectrolab [solar-panels] https://newspacemarket.com/products/spectrolab-space-solar-arrays/ Flight heritage: 500+ spacecraft including GEO, LEO, scientific, and defense missions Flight heritage: 70+ years of Spectrolab space solar array manufacturing @ (variant 2) ## ROSA Roll-Out Solar Array (Redwire / DSS) — Deployable Space Systems (DSS) — now Redwire [solar-panels] https://newspacemarket.com/products/redwire-dss-rosa/ Flight heritage: ISS iROSA (6 wings), DART mission ## GaAs side solar panel with coils — SPUTNIX [solar-panels] https://newspacemarket.com/products/gaas-side-solar-panel-with-coils/ Envelope (L×W×H): 98 x 82.6 x 8.6 mm (1.8 mm thickness w/o connector) (±0.2 mm) Output power (BOL): 4.3 W Output power (BOL): 440-480 W Cell efficiency: 28 ## GaAs end edge solar panel with coils — SPUTNIX [solar-panels] https://newspacemarket.com/products/gaas-end-edge-solar-panel-with-coils/ Envelope (L×W×H): 98 x 98 x 10 mm (1.8 mm thickness w/o connector) (±0.2 mm) Output power (BOL): 4.3 W Output power (BOL): 440-480 W Cell efficiency: 28 ## CubeSat Kit Fixed Solar Panels — Pumpkin, Inc. [solar-panels] https://newspacemarket.com/products/pumpkin-cubesat-kit-fixed-solar-panels/ Form factor: 2 large-area triple-junction solar cells Form factor: 3 large-area triple-junction solar cells @ (variant 2) Form factor: 4 large-area triple-junction solar cells @ (variant 3) Form factor: 7 large-area triple-junction solar cells @ (variant 4) ## Custom PMDSAS Panel, Body-Mounted, per Cell — Pumpkin, Inc. [solar-panels] https://newspacemarket.com/products/pumpkin-pmdsas-body-mounted-per-cell/ Flight heritage: 600+ panels flown since 2008, 100% on-orbit success rate, LEO to GTO Cell efficiency: 32 (min) ## Custom PMDSAS Panel, Deployable, per Cell — Pumpkin, Inc. [solar-panels] https://newspacemarket.com/products/pumpkin-pmdsas-deployable-per-cell/ Flight heritage: 600+ panels flown since 2008, 100% on-orbit success rate, LEO to GTO Cell efficiency: 32 (min) ## 135W Dual Articulated Deployable Solar Array — Pumpkin, Inc. [solar-panels] https://newspacemarket.com/products/pumpkin-135w-dual-articulated-deployable-solar-array/ Form factor: ~198812 cm^3 Envelope (L×W×H): 227.3 cm x 36.5 cm x 23.9 cm Output power (BOL): 135 W Output power (BOL): 67 W @ (variant 2) ## Lunar Rover Solar Panel — Pumpkin, Inc. [solar-panels] https://newspacemarket.com/products/pumpkin-lunar-rover-solar-panel/ Flight heritage: PMDSAS solar panel/solar array technology: 100% success rate in LEO and GTO orbits ## Solar Panel for AntS antenna — Pumpkin, Inc. [solar-panels] https://newspacemarket.com/products/pumpkin-solar-panel-for-ants-antenna/ Flight heritage: over 600 PMDSAS panels flown, 100% on-orbit success rate, LEO to GTO ## Advanced Solar Power Systems — Astradyne [solar-panels] https://newspacemarket.com/products/solar-z-array/ Cell efficiency: 33 (min) Output power (BOL): 10-25 W ## DROP Deployable Solar Panels — 2NDSpace Srl [solar-panels] https://newspacemarket.com/products/drop-deployable-solar-panels/ Form factor: 1U to 16U ## Solar Modules — Source Energy [solar-panels] https://newspacemarket.com/products/source-energy-solar-modules/ Flight heritage: SpaceX Transporter-8 and Transporter-9 rideshare missions ## Large Deployable Solar Arrays — Source Energy [solar-panels] https://newspacemarket.com/products/source-energy-large-deployable-solar-arrays/ Deployable: Strain energy driven Design lifetime: 7 years ## CubeSat Solar panel DHV-CS-10 — DHV Technology [solar-panels] https://newspacemarket.com/products/cubesat-solar-panel-dhv-cs-10/ Lead time: 4-5 ## Origami Solar Array — Dcubed [solar-panels] https://newspacemarket.com/products/origami-solar-array/ Lead time: 12 Mass: 1200 g Supply voltage: 14-28 ## SP Body-Mounted Solar Panels — NPC Spacemind [solar-panels] https://newspacemarket.com/products/npc-spacemind-sp-body-mounted-solar-panels/ Connector: Parallel Picoblade power connectors (2 on small sizes, 4 on SP8X) ## D-SP Deployable Solar Panels — NPC Spacemind [solar-panels] https://newspacemarket.com/products/npc-spacemind-d-sp-deployable-solar-panels/ Connector: 2 parallel Picoblade power connectors ## SmallSat GaAs Deployable Solar Panels — NanoAvionics [solar-panels] https://newspacemarket.com/products/nanoavionics-smallsat-gaas-solar-panels/ Output power (BOL): 0.0369 W Operating temperature: -40 °C Deployable: 45 W Deployable: 75 W @ (variant 2) Deployable: 90 W @ (variant 3) Deployable: 150 W @ (variant 4) Deployable: 225 W @ (variant 5) ## Ra Solar Panels — Spacemanic s.r.o. [solar-panels] https://newspacemarket.com/products/spacemanic-ra-solar-panels-2/ Cell efficiency: 30 (min) Form factor: 1U to 8U configurations Operating temperature: -40 °C Lead time: 3-7 ## Rigid Panel Solar Array — Redwire Corporation [solar-panels] https://newspacemarket.com/products/redwire-rigid-panel-solar-array/ Deployable: Spring-actuated hinged panel stack Flight heritage: Multiple commercial, civil, and defense programs ## SP1X — NPC Spacemind [solar-panels] https://newspacemarket.com/products/npc-spacemind-sp1x-solar-panel/ Mass: 40 g Output power (BOL): 2.3-2.5 W Output power (BOL): 500-520 W @ (variant 2) Output power (BOL): 4.6-5 W @ (variant 3) Supply voltage: 5.2-5.5 ## SP1Z — NPC Spacemind [solar-panels] https://newspacemarket.com/products/npc-spacemind-sp1z-solar-panel/ Mass: 45 g Output power (BOL): 2.3-2.5 W Output power (BOL): 500-520 W @ (variant 2) Output power (BOL): 4.6-5 W @ (variant 3) Supply voltage: 5.2-5.5 ## SP2X — NPC Spacemind [solar-panels] https://newspacemarket.com/products/npc-spacemind-sp2x-solar-panel/ Mass: 87 g Output power (BOL): 4.6-5 W Output power (BOL): 500-520 W @ (variant 2) Output power (BOL): 9.2-10 W @ (variant 3) Supply voltage: 10.4-11 ## SP6X — NPC Spacemind [solar-panels] https://newspacemarket.com/products/npc-spacemind-sp6x-solar-panel/ Mass: 335 g Output power (BOL): 18.4-20 W Output power (BOL): 1-1.04 W @ (variant 2) Output power (BOL): 18.4-20 W @ (variant 3) Supply voltage: 20.8-22 ## SP8X — NPC Spacemind [solar-panels] https://newspacemarket.com/products/npc-spacemind-sp8x-solar-panel/ Mass: 450 g Output power (BOL): 23-25 W Output power (BOL): 1-1.04 W @ (variant 2) Output power (BOL): 23-25 W @ (variant 3) Supply voltage: 26-27.5 ## CubeSat GaAs End/Edge Solar Panel SXC-SGE-03 — SPUTNIX [solar-panels] https://newspacemarket.com/products/sputnix-sxc-sge-03-solar-panel/ Envelope (L×W×H): 98 × 98 × 10 mm Mass: 37 g Cell efficiency: 28 Supply voltage: 5-5.5 ## CubeSat GaAs Side Solar Panel SXC-SGS-03 — SPUTNIX [solar-panels] https://newspacemarket.com/products/sputnix-sxc-sgs-03-solar-panel/ Envelope (L×W×H): 98 × 82.6 × 8.6 mm Mass: 30 g Cell efficiency: 28 Supply voltage: 5-5.5 ## Solar Arrays — Blue Canyon Technologies [solar-panels] https://newspacemarket.com/products/bct-solar-array-6u-12u/ Form factor: 27 – 34 W Form factor: 14.9 VDC @ (variant 2) Form factor: 48 – 118 W @ (variant 3) Form factor: 17 or 34.1 VDC @ (variant 4) Output power (BOL): 222-444 W Supply voltage: 36.2 Output power (BOL): 588-1175 W @ (variant 2) Supply voltage: 38.4 @ (variant 2) Flight heritage: Proven ## SP3X — NPC Spacemind [solar-panels] https://newspacemarket.com/products/npc-spacemind-sp-body-mounted-solar-panel/ Mass: 137 g Output power (BOL): 8-8.8 W Output power (BOL): 500-520 W @ (variant 2) Output power (BOL): 16-17.5 W @ (variant 3) Supply voltage: 18.2-19.3 ## D-SP6X-L-1W — NPC Spacemind [solar-panels] https://newspacemarket.com/products/npc-spacemind-d-sp-deployable-solar-panel/ Deployable: XY side Output power (BOL): 18.4-20 W Output power (BOL): 1-1.04 W @ (variant 2) Output power (BOL): 18.4-20 W @ (variant 3) Supply voltage: 20.8-22 ## Redwire Rigid Panel Solar Array Systems — Redwire Corporation [solar-panels] https://newspacemarket.com/products/redwire-rigid-panel-solar-array-systems/ Mass: 20-150 g Envelope (L×W×H): ~1 m x 1 m and larger, scaled to power Flight heritage: IXPE (launched Dec 2021), LEO/MEO/GEO and deep-space missions ## HaWK High Watts per Kilogram Solar Arrays — MMA Design [solar-panels] https://newspacemarket.com/products/mma-hawk-solar-arrays/ Output power (BOL): 36 W Flight heritage: NASA MarCO interplanetary mission, defense and commercial missions ## Chiyu Solar Energy System — Hongqing Technology (鸿擎科技) [solar-panels] https://newspacemarket.com/products/hongqing-chiyu-solar-energy-system/ Output power (BOL): 1000 W Deployable: High (optimized for compact launch stowage) ## 1U Solar Panel — NBSpace [solar-panels] https://newspacemarket.com/products/nbspace-1u-solar-panel/ Form factor: 1U ## 3U Solar Panel — NBSpace [solar-panels] https://newspacemarket.com/products/nbspace-3u-solar-panel/ Form factor: 3U ## 6U Solar Panel — NBSpace [solar-panels] https://newspacemarket.com/products/nbspace-6u-solar-panel/ Form factor: 6U ## Space Solar Solutions — SolAero Technologies (Rocket Lab) [solar-panels] https://newspacemarket.com/products/solaero-ztj-plus-solar-cell/ Flight heritage: Over 25 years ## XTE-LILT Triple-Junction Solar Cell — Spectrolab [solar-panels] https://newspacemarket.com/products/spectrolab-xte-lilt-solar-cell/ Flight heritage: Juno, New Horizons, 1000+ spacecraft ## KSSP Solar Panels — Kairo Space [solar-panels] https://newspacemarket.com/products/kairo-space-kssp-solar-panels/ Form factor: 1U–8U CubeSat ## Flexible High-Efficiency Space Solar Arrays — Flexell [solar-panels] https://newspacemarket.com/products/flexell-flexible-solar-arrays/ Deployable: Roll-out or fold-out (very compact stowed volume) ## Lunar Solar Power Plant — Yuzhnoye Design Bureau [solar-panels] https://newspacemarket.com/products/yuzhnoye-lunar-solar-power-plant/ Output power (BOL): 10 W Output power (BOL): 1-2 W Mass: 4110000 g ## ROSA — Roll-Out Solar Array — Roccor (Redwire) [solar-panels] https://newspacemarket.com/products/redwire-rosa-roll-out-solar-array-2/ Deployable: Stored strain energy in composite boom (no motors required) Flight heritage: ISS iROSA (4 pairs delivered), NASA DART, Lunar Gateway PPE (contracted) ## 1U Solar Panels — CubeSat Aerospace [solar-panels] https://newspacemarket.com/products/1u-solar-panels-3654/ Connector: 10-pin FFC connector for each panel Envelope (L×W×H): Sized to fit standard 1U CubeSat side panels ## ELSA — Deployable Space Systems (DSS) — now Redwire [solar-panels] https://newspacemarket.com/products/elsa-3683/ Form factor: Configurable per mission requirements Output power (BOL): 500 W Output power (BOL): 100 W (min) ## Small Satellite Solar Panels — Innovative Space Logistics [solar-panels] https://newspacemarket.com/products/small-satellite-solar-panels-1478/ Mass: 50 g Mass: 100 g @ (variant 2) Mass: 150 g @ (variant 3) Mass: 300 g @ (variant 4) Mass: 400 g @ (variant 5) Operating temperature: -40-80 °C Output power (BOL): 1.23 W Supply voltage: 2.7 Cell efficiency: 30 ## Solar Panels — Ananth Technologies [solar-panels] https://newspacemarket.com/products/solar-panels-3467/ Operating temperature: -60 °C Form factor: Up to 1.5m × 2.5m Form factor: PCB @ (variant 2) Form factor: 2 cells in series @ (variant 3) Form factor: ~2 W @ (variant 4) Form factor: 83 × 103.2 mm @ (variant 5) Form factor: 206.5 × 321.3 mm @ (variant 6) Form factor: FR-4 @ (variant 7) Form factor: 5S × 3P @ (variant 8) Form factor: CFRP plate + FR-4 flex circuitry @ (variant 9) Form factor: 336 × 205 mm @ (variant 10) Envelope (L×W×H): up to 1.5 m × 2.5 m ## 8U Deployable Solar Array — EnduroSat [solar-panels] https://newspacemarket.com/products/8u-deployable-solar-array/ Cell efficiency: 30 Cell efficiency: 29 @ (variant 2) Output power (BOL): 48 W Mass: 930-1035 g Supply voltage: 49.8 ## 3U Deployable Solar Array — EnduroSat [solar-panels] https://newspacemarket.com/products/3u-deployable-solar-array/ Cell efficiency: 30 Cell efficiency: 29 @ (variant 2) ## 8U SOLAR PANEL — EnduroSat [solar-panels] https://newspacemarket.com/products/8u-solar-panel/ Cell efficiency: 30 Cell efficiency: 29 @ (variant 2) Output power (BOL): 24 W Mass: 545 g Supply voltage: 49.8 ## 6U Solar Panel — EnduroSat [solar-panels] https://newspacemarket.com/products/6u-solar-panel/ Cell efficiency: 30 Cell efficiency: 29 @ (variant 2) Output power (BOL): 19.2 W Mass: 392 g Supply voltage: 39.8 ## Triple-Junction GaAs Solar Array — Shenzhen MagicCubeSat Technology (MCS) [solar-panels] https://newspacemarket.com/products/mcs-gaas-solar-array/ Flight heritage: 20+ arrays in orbit ## Solar Panels for Small Satellites — DHV Technology [solar-panels] https://newspacemarket.com/products/solar-panels-for-small-satellites/ TRL: 9 ## Solar panels for CubeSats — DHV Technology [solar-panels] https://newspacemarket.com/products/solar-panels-for-cubesats/ Form factor: 2.4 W Form factor: 4.8 V @ (variant 2) Form factor: 0.5 A @ (variant 3) Form factor: < 50 g @ (variant 4) Mass: 100 g (max) Form factor: 8.4 W @ (variant 5) Form factor: 16.8 V @ (variant 6) Form factor: 0.5 A @ (variant 7) Form factor: < 160 g @ (variant 8) ## D-SP6X-V — NPC Spacemind [solar-panels] https://newspacemarket.com/products/d-sp6x-v/ Output power (BOL): 16.1-17.5 W Output power (BOL): 1-1.04 W @ (variant 2) Output power (BOL): 16.1-17.5 W @ (variant 3) Supply voltage: 18.2-19.3 ## D-SP8X-V — NPC Spacemind [solar-panels] https://newspacemarket.com/products/d-sp8x-v/ Output power (BOL): 23-25 W Output power (BOL): 1-1.04 W @ (variant 2) Output power (BOL): 23-25 W @ (variant 3) Supply voltage: 26-27.5 ## D-SP3X-L-1W — NPC Spacemind [solar-panels] https://newspacemarket.com/products/d-sp3x-l-1w/ Output power (BOL): 8-8.8 W Output power (BOL): 500-520 W @ (variant 2) Output power (BOL): 16-17.5 W @ (variant 3) Supply voltage: 18.2-19.3 ## D-SP3X-L-2W — NPC Spacemind [solar-panels] https://newspacemarket.com/products/d-sp3x-l-2w/ Output power (BOL): 16-17.6 W ## D-SP6X-L-2W — NPC Spacemind [solar-panels] https://newspacemarket.com/products/d-sp6x-l-2w/ Output power (BOL): 36.8-40 W ## D-SP8X-L-1W — NPC Spacemind [solar-panels] https://newspacemarket.com/products/d-sp8x-l-1w/ Output power (BOL): 23-25 W Output power (BOL): 1-1.04 W @ (variant 2) Output power (BOL): 23-25 W @ (variant 3) Supply voltage: 26-27.5 ## D-SP8X-L-2W — NPC Spacemind [solar-panels] https://newspacemarket.com/products/d-sp8x-l-2w/ Output power (BOL): 46-50 W ## SP2Z — NPC Spacemind [solar-panels] https://newspacemarket.com/products/sp2z/ Mass: 80 g Output power (BOL): 4.6-5.2 W Output power (BOL): 500-520 W @ (variant 2) Output power (BOL): 9.2-10 W @ (variant 3) Supply voltage: 10.4-11 ## SP4X — NPC Spacemind [solar-panels] https://newspacemarket.com/products/sp4x/ Mass: 160 g Output power (BOL): 10.35-11.7 W Output power (BOL): 500-520 W @ (variant 2) Output power (BOL): 20.7-22.5 W @ (variant 3) Supply voltage: 23.4-24.75 ## SP4Z — NPC Spacemind [solar-panels] https://newspacemarket.com/products/sp4z/ Mass: 180 g Output power (BOL): 9.2-10 W Output power (BOL): 500-520 W @ (variant 2) Output power (BOL): 18.4-20 W @ (variant 3) Supply voltage: 20.8-22 ## 77cm 2 Class (SuperCell) Triple Junction Solar Cell — Spectrolab [solar-panels] https://newspacemarket.com/products/77cm-2-class-supercell-triple-junction-solar-cell/ Cell efficiency: 30.7 Cell efficiency: 26.7 @ (variant 2) Form factor: 26-84 cm2 ## SASC Sub-Arcsecond Star Camera — StarSpec Technologies [star-trackers] https://newspacemarket.com/products/starspec-scanner-spec/ Max tracking slew rate: 1 Power consumption: 5 W Operating temperature: -40-85 °C ## Auriga Star Tracker — Sodern [star-trackers] https://newspacemarket.com/products/sodern-auriga-star-tracker/ Flight heritage: OneWeb constellation (1,800+ units), NASA Blue Ghost 1 lunar lander, DLR COMPASSO ## ASTROgyro Integrated Attitude Determination System — Jena-Optronik [star-trackers] https://newspacemarket.com/products/jena-optronik-astrogyro/ Update rate: 30 Hz Envelope (L×W×H): ~230 x 230 x 170 mm ## ASTRO 10 Star Tracker — Safran Electronics Defense Space [star-trackers] https://newspacemarket.com/products/safran-astro10-star-tracker/ Flight heritage: 50+ missions ## Micro Star Sensor — Pyxis Space [star-trackers] https://newspacemarket.com/products/pyxis-micro-star-sensor/ Envelope (L×W×H): <Ø70 mm × 100 mm Attitude accuracy (cross-boresight): 0.02 (max) ## Nano Star Sensor — Pyxis Space [star-trackers] https://newspacemarket.com/products/pyxis-nano-star-sensor/ Envelope (L×W×H): 36 × 36 × 46 mm³ Attitude accuracy (cross-boresight): 0.05 (max) ## Multi-Head Star Sensor — Pyxis Space [star-trackers] https://newspacemarket.com/products/pyxis-multi-head-star-sensor/ Attitude accuracy (cross-boresight): 0.05 (max) ## 16U Structure — EnduroSat [structures] https://newspacemarket.com/products/endurosat-16u-cubesat-structure/ Envelope (L×W×H): 226.3 x 226.3 x 366 mm ## 12U Structure — EnduroSat [structures] https://newspacemarket.com/products/endurosat-12u-cubesat-structure/ Envelope (L×W×H): 226.3 x 226.3 x 454 mm ## 3U Cubesat Platform — Glavkosmos [structures] https://newspacemarket.com/products/3u-cubesat-platform/ Design lifetime: 1 years Lead time: 12 Mass: 3000 g Power consumption: 12 W ## Conical Adapter. Type 2 — Glavkosmos [structures] https://newspacemarket.com/products/conical-adapter-type-2/ Mass: 34000 g ## Conical Adapter. Type 3 — Glavkosmos [structures] https://newspacemarket.com/products/conical-adapter-type-3/ Flight heritage: Flight-qualified since 2000 ## Conical Adapter. Type 4 — Glavkosmos [structures] https://newspacemarket.com/products/conical-adapter-type-4/ Mass: 62000 g Flight heritage: Flight-qualified since 2000 ## Conical Adapter. Type 5 — Glavkosmos [structures] https://newspacemarket.com/products/conical-adapter-type-5/ Mass: 91140 g Flight heritage: Flight-qualified since 2000 ## Load-bearing Structure of the Enclosure. Type 1-A — Glavkosmos [structures] https://newspacemarket.com/products/load-bearing-structure-of-the-enclosure-type-1-a/ Flight heritage: Flight-qualified since 2000 ## Load-bearing Structure of the Enclosure. Type 1-B — Glavkosmos [structures] https://newspacemarket.com/products/load-bearing-structure-of-the-enclosure-type-1-b/ Flight heritage: Flight-qualified since 2000 ## Load-bearing Structure of the Enclosure. Type 2 — Glavkosmos [structures] https://newspacemarket.com/products/load-bearing-structure-of-the-enclosure-type-2/ Flight heritage: Flight-qualified since 2000 ## Load-bearing Structure of the Enclosure. Type 3 — Glavkosmos [structures] https://newspacemarket.com/products/load-bearing-structure-of-the-enclosure-type-3/ Flight heritage: Flight-qualified since 2000 ## Load-bearing Structure of the Enclosure. Type 4 — Glavkosmos [structures] https://newspacemarket.com/products/load-bearing-structure-of-the-enclosure-type-4/ Flight heritage: Flight-qualified since 2000 ## Load-bearing Structure of the Enclosure. Type 5 — Glavkosmos [structures] https://newspacemarket.com/products/load-bearing-structure-of-the-enclosure-type-5/ Flight heritage: Flight-qualified since 2000 ## Load-bearing Structure of the Enclosure. Type 6 — Glavkosmos [structures] https://newspacemarket.com/products/load-bearing-structure-of-the-enclosure-type-6/ Flight heritage: Flight-qualified since 2000 ## Nanosatellite Platform of CubeSat 3U Format — Glavkosmos [structures] https://newspacemarket.com/products/nanosatellite-platform-of-cubesat-3u-format/ Design lifetime: 1 years Lead time: 12 Flight heritage: Not flight-qualified ## Nanosatellite Platform — Glavkosmos [structures] https://newspacemarket.com/products/nanosatellite-platform/ Design lifetime: 5 years Lead time: 18 Mass: 3500 g Mass: 1500 g @ (variant 2) Supply voltage: 3.2 Envelope (L×W×H): 100 x 100 x 300 mm TRL: 6 ## Satellite Platform CubeSat 1U — Glavkosmos [structures] https://newspacemarket.com/products/satellite-platform-cubesat-1u/ Design lifetime: 1 years Lead time: 5 Envelope (L×W×H): 108 × 108 × 113 mm Mass: 900 g Power consumption: 0.25 W Power consumption: 1 W @ (variant 2) ## Satellite Platform CubeSat 3U for Complex Missions — Glavkosmos [structures] https://newspacemarket.com/products/satellite-platform-cubesat-3u-for-complex-missions/ Design lifetime: 1 years Lead time: 9 Envelope (L×W×H): 108 × 108 × 340.5 mm Mass: 2000 g Power consumption: 2 W Power consumption: 1 W @ (variant 2) ## Satellite Platform CubeSat 3U — Glavkosmos [structures] https://newspacemarket.com/products/satellite-platform-cubesat-3u/ Design lifetime: 1 years Lead time: 5 Envelope (L×W×H): 108 × 108 × 340.5 mm Mass: 1500 g Power consumption: 1 W Power consumption: 1 W @ (variant 2) ## Satellite Platform CubeSat 6U — Glavkosmos [structures] https://newspacemarket.com/products/satellite-platform-cubesat-6u/ Design lifetime: 1 years Lead time: 14 Envelope (L×W×H): 108 × 221 × 340.5 mm Mass: 5000 g Power consumption: 4 W ## Space Platform 100 — Glavkosmos [structures] https://newspacemarket.com/products/space-platform-100/ Lead time: 18 ## Space Platform 50 — Glavkosmos [structures] https://newspacemarket.com/products/space-platform-50/ Lead time: 12 Flight heritage: Prototype flew as part of ICA "MIR", launched 28 July 2012 ## Space Platform 500 — Glavkosmos [structures] https://newspacemarket.com/products/space-platform-500/ Mass: 350000 g ## Structure 1U CubeSat with Separation System — Glavkosmos [structures] https://newspacemarket.com/products/structure-1u-cubesat-with-separation-system/ Design lifetime: 3 years Lead time: 2 Envelope (L×W×H): 100 × 100 × 113.5 mm Mass: 132 g Random vibration: 12 ## Structure 3U CubeSat with Separation System — Glavkosmos [structures] https://newspacemarket.com/products/structure-3u-cubesat-with-separation-system/ Design lifetime: 3 years Lead time: 2 Envelope (L×W×H): 100 × 100 × 340.5 mm Mass: 455 g Random vibration: 12 ## The Multipurpose Block-Modular Platform — Glavkosmos [structures] https://newspacemarket.com/products/the-multipurpose-block-modular-platform/ Design lifetime: 5 years Lead time: 16 Mass: 2500 g Envelope (L×W×H): 100 × 100 × 340.5 mm Power consumption: 140 W Power consumption: 5 W @ (variant 2) ## Universal Space Platform K — Glavkosmos [structures] https://newspacemarket.com/products/universal-space-platform-k/ Mass: 140000-210000 g Power consumption: 250-300 W Mass: 100000-130000 g @ (variant 2) ## Universal Space Platform N — Glavkosmos [structures] https://newspacemarket.com/products/universal-space-platform-n/ Mass: 850000-980000 g Power consumption: 600-1150 W Mass: 2600000 g ## Multi-layer Composite Structures — Glavkosmos [structures] https://newspacemarket.com/products/multi-layer-composite-structures/ Design lifetime: 20 years Lead time: 3 Envelope (L×W×H): up to 3 × 2.8 × 0.08m ## Honeycomb Panel with Composite Face Sheets — Glavkosmos [structures] https://newspacemarket.com/products/honeycomb-panel-with-composite-face-sheets/ Envelope (L×W×H): 5800 × 3000 mm ## Multi-Layer Honeycomb Panel — Glavkosmos [structures] https://newspacemarket.com/products/multi-layer-honeycomb-panel/ Envelope (L×W×H): 2.25, 2.5, 3, 3.5, 5.6 Mass: 17000-90000 g ## Temperature-controlled Honeycomb Panel — Glavkosmos [structures] https://newspacemarket.com/products/temperature-controlled-honeycomb-panel/ Envelope (L×W×H): 5800 × 3000 mm ## 3U platform — Orbital Systems [structures] https://newspacemarket.com/products/orbital-systems-3u-cubesat-platform/ Power consumption: 50 W Mass: 1000 g Envelope (L×W×H): 340×100×100 mm Mass: 1500 g @ (variant 2) Power consumption: 1.8 W @ (variant 2) Flight heritage: Since 2019 ## 6U CubeSat Platform — Orbital Systems [structures] https://newspacemarket.com/products/orbital-systems-6u-cubesat-platform/ Power consumption: 75 W Mass: 7500 g Envelope (L×W×H): 340×200×100 mm Mass: 4500 g @ (variant 2) Power consumption: 6 W @ (variant 2) Flight heritage: Since 2020 ## 12U/16U CubeSat Platform — Orbital Systems [structures] https://newspacemarket.com/products/orbital-systems-12u-cubesat-platform/ Power consumption: 100 W Mass: 16000 g Envelope (L×W×H): 322×215×215 mm Mass: 6500 g @ (variant 2) Power consumption: 7 W @ (variant 2) ## Geoscan 16U — Geoscan [structures] https://newspacemarket.com/products/%d0%b3%d0%b5%d0%be%d1%81%d0%ba%d0%b0%d0%bd-16u-innosat16-cubesat-platform/ Mass: 20000 g ## SIGI Satellite Mission — Reflex Aerospace [structures] https://newspacemarket.com/products/sigi/ Mass: 109000 g Power consumption: 900 W Power consumption: 330 W @ (variant 2) ## S-CLASS Satellite Bus — York Space Systems [structures] https://newspacemarket.com/products/s-class-satellite-bus/ Mass: 85000 g Power consumption: 274 W ## Photon Spacecraft Bus Platform — Rocket Lab – Photon [structures] https://newspacemarket.com/products/photon-satellite-bus-platform/ Mass: 50000 g Power consumption: 3 W Flight heritage: CAPSTONE lunar (2022), Varda Pioneer re-entry (2023), multiple LEO missions ## CubeSat Platforms — ISISPACE Group [structures] https://newspacemarket.com/products/isispace-cubesat-platforms/ Flight heritage: 73+ ISISPACE satellites launched ## Geoscan 16U CubeSat Platform (InnoSat16) — Geoscan [structures] https://newspacemarket.com/products/geoscan-16u-innosat16-cubesat-platform/ Mass: 20000 g Mass: 32000 g @ (variant 2) Envelope (L×W×H): 251.3×251.3×454 mm (251.3×251.3×512 mm with Tuna Can) Power consumption: 45 W Flight heritage: InnoSat16 launched July 25, 2025, Vostochny Cosmodrome, SSO 500 km ## Nova Satellite Bus — Apex [structures] https://newspacemarket.com/products/apex-nova/ Power consumption: 1 W Supply voltage: 28 ## Comet Mini Satellite Bus — Apex [structures] https://newspacemarket.com/products/apex-comet-mini/ Power consumption: 8 W Power consumption: 20 W @ (variant 2) ## XDSAT NS — XDLINX Space Labs [structures] https://newspacemarket.com/products/xdlinx-xdsat-ns/ Power consumption: 126 W Flight heritage: Launched 2023 ## XDSAT NL — XDLINX Space Labs [structures] https://newspacemarket.com/products/xdlinx-xdsat-nl/ Power consumption: 210 W Flight heritage: Q2-2024 ## XDSAT M200 — XDLINX Space Labs [structures] https://newspacemarket.com/products/xdlinx-xdsat-m200/ Mass: 25000-40000 g Power consumption: 350 W Flight heritage: Q4-2024 ## XDSAT M400 — XDLINX Space Labs [structures] https://newspacemarket.com/products/xdlinx-xdsat-m400/ Mass: 40000-75000 g Power consumption: 700 W Flight heritage: Q1-2025 ## XDSAT M600 — XDLINX Space Labs [structures] https://newspacemarket.com/products/xdlinx-xdsat-m600/ Power consumption: 1100 W Flight heritage: Q4-2024; in-orbit qualified June 2026 ## MINIATURE SATELLITES (PocketQubes) — Xavier Space Solutions (XavSat) [structures] https://newspacemarket.com/products/xavsat-pocketqube-satellite-bus/ Mass: 250 g (max) Mass: 250 g ## XavSat PocketQubes (1P to 3P) — Xavier Space Solutions (XavSat) [structures] https://newspacemarket.com/products/xavsat-xavsat-1-mission-satellite/ Mass: 250 g (max) Form factor: 5 Mass: 250 g ## Flamingo — Vyoma GmbH [structures] https://newspacemarket.com/products/vyoma-flamingo-1/ Flight heritage: Flamingo-1 launched and operational, providing follow-up capabilities and observations of otherwise impossible-to-attain orbital regions ## Flamingo Satellite Constellation — Vyoma GmbH [structures] https://newspacemarket.com/products/vyoma-flamingo-2/ Design lifetime: 5 years ## Triumph — Terran Orbital [structures] https://newspacemarket.com/products/tyvak-triumph/ Mass: 5000 g ## Excelsior — Terran Orbital [structures] https://newspacemarket.com/products/tyvak-excelsior/ Mass: 50000 g ## Enterprise — Terran Orbital [structures] https://newspacemarket.com/products/tyvak-enterprise/ Mass: 500000 g Mass: 1000000 g @ (variant 2) Mass: 1250000 g @ (variant 3) ## KAM/CSB/12U Smart Backplane Chassis — Curtiss-Wright Defense Solutions [structures] https://newspacemarket.com/products/curtiss-wright-defense-solutions-kam-csb-12u-smart-backplane/ Flight heritage: Boeing CST-100 Starliner, ESA/Avio Vega-C launcher, NASA SLS/Orion, Rocket Lab, SpaceX Falcon 9/Dragon, ESA IXV, ULA Delta IV, ISS ACLS ## CubeSat Kit™ Large Aperture Base Plate Assembly, Dual Switch — Pumpkin, Inc. [structures] https://newspacemarket.com/products/pumpkin-large-aperture-base-plate-dual-switch/ Flight heritage: Flight Hardware | Flight Qualified | Space Proven ## CubeSat Kit™ Cover Plate Assembly — Pumpkin, Inc. [structures] https://newspacemarket.com/products/pumpkin-cover-plate-assembly/ Envelope (L×W×H): 100 mm x 100 mm / 3.937 in x 3.937 in ## ADACS Payload Walls / 1U Chassis MAI-100/MAI-200 Extension — Pumpkin, Inc. [structures] https://newspacemarket.com/products/pumpkin-adacs-payload-walls-1u-chassis-mai-100-mai-200-extension/ Flight heritage: JPL/Stanford LMRST-Sat 3U mission Operating temperature: -40-85 °C Mass: 34 g Connector: 2.54 mm ## 3U CubeSat Frame — Princeton Satellite Systems [structures] https://newspacemarket.com/products/cubesat-3u-frame-pss/ Mass: 350 g Envelope (L×W×H): 10 × 10 × 10 cm ## 12-Unit cubesat structure — ISISPACE Group [structures] https://newspacemarket.com/products/12-unit-cubesat-structure/ Lead time: 8-12 ## SM CubeSat Structures — NPC Spacemind [structures] https://newspacemarket.com/products/npc-spacemind-sm-cubesat-structures/ Envelope (L×W×H): 113.5 x 100.0 x 100.0 mm, 1U, up to 6 deployment switches Envelope (L×W×H): 227.0 x 100.0 x 100.0 mm, 2U, up to 8 deployment switches @ (variant 2) Envelope (L×W×H): 340.5 x 100.0 x 100.0 mm, 3U, up to 8 deployment switches @ (variant 3) Envelope (L×W×H): 454.0 x 100.0 x 100.0 mm, 4U, up to 8 deployment switches @ (variant 4) Envelope (L×W×H): 340.5 x 226.3 x 100.0 mm, 6U, up to 8 deployment switches @ (variant 5) Envelope (L×W×H): 454.0 x 226.3 x 100.0 mm, 8U, up to 8 deployment switches, horizontal/vertical stack @ (variant 6) Envelope (L×W×H): 340.5 x 226.3 x 226.3 mm, 12U, up to 8 deployment switches, horizontal/vertical stack @ (variant 7) Envelope (L×W×H): 454.0 x 226.3 x 226.3 mm, 16U, up to 8 deployment switches, horizontal/vertical stack @ (variant 8) ## XO-BUS CubeSat Buses — Exobotics [structures] https://newspacemarket.com/products/exobotics-xo-bus-3u/ Mass: 3800 g (max) Power consumption: 25 W (max) Flight heritage: 4 missions ## German Orbital Systems Satellite Platforms — German Orbital Systems [structures] https://newspacemarket.com/products/gos-slot-platform/ Flight heritage: 12 ## SPARTA-G70 — Hemeria [structures] https://newspacemarket.com/products/hemeria-sparta-g70-platform/ Mass: 50000 g Mass: 15000-20000 g ## SPECTRA-L40 — Hemeria [structures] https://newspacemarket.com/products/hemeria-spectra-l40-platform/ Mass: 20000 g Mass: 20000 g @ (variant 2) ## CubeSat 3U Platform — IMT (Ingegneria Marketing Technologies) [structures] https://newspacemarket.com/products/imt-cubesat-3u-platform/ Mass: 6000 g (max) Radiation tolerance (TID): 15 krad (min) Random vibration: 10 Design lifetime: 5 years (max) ## CubeSat 6U Platform — IMT (Ingegneria Marketing Technologies) [structures] https://newspacemarket.com/products/imt-cubesat-6u-platform/ Power consumption: 10 W Power consumption: 50 W @ (variant 2) Power consumption: 115 W @ (variant 3) Design lifetime: 3 years ## SM01 — NPC Spacemind [structures] https://newspacemarket.com/products/npc-spacemind-sm01-1u-structure/ Form factor: 1 ## SM16 — NPC Spacemind [structures] https://newspacemarket.com/products/npc-spacemind-sm16-16u-structure/ Form factor: 16 ## LEOS-100 — Berlin Space Technologies [structures] https://newspacemarket.com/products/bst-leos-100-satellite-platform/ Mass: 250000 g Envelope (L×W×H): 2 m³ Power consumption: 154 W Design lifetime: 5 years Mass: 250000 g @ (variant 2) Envelope (L×W×H): 2 m³ @ (variant 2) Power consumption: 308 W @ (variant 2) Design lifetime: 5 years @ (variant 2) Mass: 250000 g @ (variant 3) Envelope (L×W×H): 2 m³ @ (variant 3) Design lifetime: 5 years @ (variant 3) ## 8U Platform Kit — GomSpace [structures] https://newspacemarket.com/products/gomspace-nanosat-8u-kit/ Envelope (L×W×H): 8U ## 16U Platform Kit — GomSpace [structures] https://newspacemarket.com/products/gomspace-nanosat-16u-kit/ Envelope (L×W×H): 16U ## 12U Platform Kit — GomSpace [structures] https://newspacemarket.com/products/gomspace-nanosat-12u-kit/ Envelope (L×W×H): 12U ## 16U Satellite Bus Platform — Nara Space [structures] https://newspacemarket.com/products/nara-space-16u-satellite-bus-platform/ Form factor: 16 Flight heritage: K-band communication mission (space-proven) ## 1U Cube Structure — Gran Systems [structures] https://newspacemarket.com/products/1u-cubesat-structure/ Envelope (L×W×H): Length 100 x Width 100 x Height 113.5 mm Form factor: 95.9 Mass: 118 g ## 3U CubeSat Structure — Gran Systems [structures] https://newspacemarket.com/products/3u-cubesat-structure/ Envelope (L×W×H): L 100 × W 100 × H 340 mm Form factor: 95.9 Envelope (L×W×H): L 104 × W 104 × H 340 mm @ (variant 2) Mass: 580 g ## 6U Cube Structure — Gran Systems [structures] https://newspacemarket.com/products/6u-cubesat-structure/ Envelope (L×W×H): L 100 × W 226.3 × H 366 mm Envelope (L×W×H): L 104 × W 230.3 × H 366 mm @ (variant 2) Mass: 916 g ## CubeSat Structure (1U / 2U / 3U) — KSF Space Foundation [structures] https://newspacemarket.com/products/ksf-space-cubesat-structure/ Form factor: 1 ## Modular CubeSat Structures — Serenum Space [structures] https://newspacemarket.com/products/serenum-modular-cubesat-structure/ Envelope (L×W×H): 226.3 x 100 x 340.5 mm Envelope (L×W×H): 88.4 x 214.7 x 318.5 mm @ (variant 2) Envelope (L×W×H): 100 x 100 x 340.5 mm @ (variant 3) Mass: 396 g Flight heritage: Yes ## CubeSat Aerospace Satellite Structures (1U–6U) — CubeSat Aerospace [structures] https://newspacemarket.com/products/cubesat-aerospace-dev-kits/ Envelope (L×W×H): 100 × 100 × 113.5 mm Envelope (L×W×H): 100 × 100 × 170.25 mm @ (variant 2) Envelope (L×W×H): 100 × 100 × 227 mm @ (variant 3) Envelope (L×W×H): 100 × 100 × 340.5 mm @ (variant 4) Envelope (L×W×H): 100 × 200 × 340.5 mm @ (variant 5) Warranty: 1 ## Cleon I — NPK Barl [structures] https://newspacemarket.com/products/okb5-cleon-i-cubesat-platform/ Flight heritage: Over 4 years Mass: 500 g Mass: 3000 g @ (variant 2) Mass: 6000 g @ (variant 3) Mass: 12000 g @ (variant 4) Power consumption: 4-6 W Power consumption: 10-15 W @ (variant 2) Power consumption: 12-20 W @ (variant 3) Power consumption: 30-50 W @ (variant 4) Power consumption: 3 W (max) Power consumption: 3 W (max) @ (variant 2) Power consumption: 3 W (max) @ (variant 3) Power consumption: 5 W (max) @ (variant 4) ## Arcturus MicroSat Bus Platform — ST Engineering Satellite Systems [structures] https://newspacemarket.com/products/ste-satsys-arcturus-microsat-bus/ Flight heritage: Flight-proven (TeLEOS-1, TeLEOS-2, NeuSAR) ## 1U CubeSat Structure — CubeSat Aerospace [structures] https://newspacemarket.com/products/1u-cubesat-structure-3654/ Envelope (L×W×H): 100 mm × 100 mm × 113.5 mm ## Bundle (1p,1.5p,2p,2.5p) Skeleton Wall PocketQube Structures — Alba Orbital [structures] https://newspacemarket.com/products/bundle-1p-1-5p-2p-2-5p-skeleton-wall-pocketqube-structures-1479/ Envelope (L×W×H): 1p,1.5p,2p,2.5p (Unit) ## Custom PocketQube Structural Panel — Alba Orbital [structures] https://newspacemarket.com/products/custom-pocketqube-structural-panel-1479/ Envelope (L×W×H): 1p/1.5p/2p/3p ## 1U Cubesat Structure — Aphelion Orbitals [structures] https://newspacemarket.com/products/1u-cubesat-structure-3474/ Mass: 92 g ## 8U CubeSat Structure — EnduroSat [structures] https://newspacemarket.com/products/8u-cubesat-structure/ Mass: 973 g Envelope (L×W×H): 100 x 226.3 x 454 mm ## CFRP Engineering — Perigee Aerospace [structures] https://newspacemarket.com/products/cfrp-engineering/ Mass: 36000 g Mass: 75000 g @ (variant 2) Operating temperature: -196 °C ## Nanostruct 16U — GomSpace [structures] https://newspacemarket.com/products/nanostruct-16u/ Mass: 1496 g ## BAE Systems Satellite Platform P10 — In Space Missions [structures] https://newspacemarket.com/products/bae-systems-satellite-platform-p10/ Mass: 35000 g Design lifetime: 5 years @ Low Earth Orbit ## 3U Cubesat Platform — Orbital Systems [structures] https://newspacemarket.com/products/3u-cubesat-platform-2/ Power consumption: 50 W Mass: 1000 g Form factor: 340 Mass: 1500 g @ (variant 2) Power consumption: 1.8 W @ (variant 2) Flight heritage: since 2019 ## 6U Cubesat Platform — Orbital Systems [structures] https://newspacemarket.com/products/6u-cubesat-platform/ Power consumption: 75 W Mass: 7500 g Form factor: 340 Mass: 4500 g @ (variant 2) Power consumption: 6 W @ (variant 2) ## 12U Cubesat Platform — Orbital Systems [structures] https://newspacemarket.com/products/12u-cubesat-platform/ Power consumption: 100 W Mass: 16000 g Form factor: 322 Mass: 6500 g @ (variant 2) Power consumption: 7 W @ (variant 2) ## SXC-SD-01 Sun Sensor — SPUTNIX [sun-sensors] https://newspacemarket.com/products/sputnix-sxc-sd-01-sun-sensor/ Envelope (L×W×H): 28 × 23 × 7 mm ## Sun Sensor — Glavkosmos [sun-sensors] https://newspacemarket.com/products/sun-sensor/ Design lifetime: 1 years Lead time: 3 Envelope (L×W×H): 28 × 23 × 11 mm Mass: 10 g Power consumption: 0.02 W ## Digital Sun Sensor (±64°) — Adcole Space (Redwire) [sun-sensors] https://newspacemarket.com/products/adcole-digital-sun-sensor-64/ Power consumption: 1 W Radiation tolerance (TID): 100 krad Flight heritage: Yes — Mars 2020, Parker Solar Probe, Cassini ## Digital Sun Sensor (±32°) — Adcole Space (Redwire) [sun-sensors] https://newspacemarket.com/products/adcole-digital-sun-sensor-32/ Radiation tolerance (TID): 100 krad Flight heritage: Yes ## TensorFSS-15M Fine Sun Sensor — Tensor Tech [sun-sensors] https://newspacemarket.com/products/tensor-tech-fss-30-discrete/ Radiation tolerance (TID): 24 krad (min) Envelope (L×W×H): 22 x 15 x 5.3 mm3 Supply voltage: 3.3 Mass: 3 g ## TensorFSS-30M Fine Sun Sensor — Tensor Tech [sun-sensors] https://newspacemarket.com/products/tensor-tech-fss-30m/ Supply voltage: 3.3 Radiation tolerance (TID): 24 krad (min) Envelope (L×W×H): 22 × 15 × 5.3 mm Mass: 3 g ## SS-D Sun Sensor — TY-Space Technology [sun-sensors] https://newspacemarket.com/products/ty-space-ss-d-sun-sensor/ Accuracy: 5 ° Envelope (L×W×H): 32× 36×13 Mass: 45 g Power consumption: 1.1 W Radiation tolerance (TID): 30 krad Design lifetime: 4 years ## Sun sensor — SPUTNIX [sun-sensors] https://newspacemarket.com/products/sun-sensor-2/ Envelope (L×W×H): 31.3 x 27.5 x 10.3 mm (±0.2 mm, with 66100411722 connector) Envelope (L×W×H): 31.3 x 27.5 x 8.6 mm (±0.2 mm, with 653104131822 connector) @ (variant 2) ## Solar sensor — SPUTNIX [sun-sensors] https://newspacemarket.com/products/solar-sensor/ Envelope (L×W×H): 43 x 43 x 16 (without fasteners) mm Mass: 45 g Accuracy: 0.15 ° ## HSNS — Solar MEMS Technologies [sun-sensors] https://newspacemarket.com/products/solar-mems-hsns/ Operating temperature: -30 °C Radiation tolerance (TID): 30 krad Envelope (L×W×H): 90 x 92 x 50 mm Mass: 120 g Design lifetime: 3 years ## Fine Sun Sensor — Space Inventor ApS [sun-sensors] https://newspacemarket.com/products/fine-sun-sensor/ Accuracy: 1 ° (max) ## MAI-SES IR Earth Sensor — Adcole Space (Redwire) [sun-sensors] https://newspacemarket.com/products/mai-ses-ir-earth-sensor/ Lead time: 90 ## MAI-KE Sun Sensor — Adcole Space (Redwire) [sun-sensors] https://newspacemarket.com/products/mai-ke-sun-sensor/ Lead time: 90 ## Tensor Tech FSS-15 Fine Sun Sensor — Tensor Tech [sun-sensors] https://newspacemarket.com/products/tensor-tech-fss-15-fine-sun-sensor/ Flight heritage: since 2022 Lead time: 2 Radiation tolerance (TID): 10 krad (min) ## Infrared (IR) Earth Horizon Sensor — CubeSpace ADCS [sun-sensors] https://newspacemarket.com/products/infrared-ir-earth-horizon-sensor/ Mass: 18 g Envelope (L×W×H): 35x24x20 mm Connector: Molex Pico-Lock Plus Supply voltage: 3.3 Power consumption: 0.28 W Power consumption: 0.2 W @ (variant 2) Radiation tolerance (TID): 24 krad ## Fine Sun Sensor – CubeSense Sun — CubeSpace ADCS [sun-sensors] https://newspacemarket.com/products/fine-sun-sensor-cubesense-sun/ Lead time: 12 ## S3 Smart Sun Sensor — Leonardo SpA (Space Division) [sun-sensors] https://newspacemarket.com/products/leonardo-s3-smart-sun-sensor/ Accuracy: 0.02 ° (max) Envelope (L×W×H): 112 x 12 x 43 mm Mass: 330 g (max) Operating temperature: -25-60 °C Design lifetime: 15 years (min) ## Coarse Sun Sensor — Pyramid Type — Redwire Corporation [sun-sensors] https://newspacemarket.com/products/redwire-css-pyramid/ Envelope (L×W×H): 89 × 89 × 43 mm (3.5 × 3.5 × 1.7 in) Mass: 130 g Radiation tolerance (TID): 100 krad (min) ## Coarse Sun Sensor — Cosine Type — Redwire Corporation [sun-sensors] https://newspacemarket.com/products/redwire-css-cosine/ Mass: 10 g Envelope (L×W×H): 28 × 19 × 12 mm (1.10 × 0.74 × 0.47 in) Output type: 500-1300 Radiation tolerance (TID): 100 krad (min) ## CubeSat Sun Sensor SXC-SD-01-3U — SPUTNIX [sun-sensors] https://newspacemarket.com/products/sputnix-sxc-sd-01-3u-sun-sensor/ Envelope (L×W×H): 31.3 × 27.5 × 10.3 mm Mass: 7 g Accuracy: 0.3 ° (max) Power consumption: 0.03-0.05 W ## Microsatellite Sun Sensor SX-SBOX-SUNS-01 — SPUTNIX [sun-sensors] https://newspacemarket.com/products/sputnix-sx-sbox-suns-01-sun-sensor/ Envelope (L×W×H): 43 × 43 × 16 mm Mass: 45 g Accuracy: 0.15 ° Power consumption: 0.4 W ## Eagle Sun Sensor — Needronix [sun-sensors] https://newspacemarket.com/products/needronix-eagle-sun-sensor/ Accuracy: 0.09 ° Mass: 12 g Supply voltage: 3.3 ## Eagle Plus Sun Sensor — Needronix [sun-sensors] https://newspacemarket.com/products/needronix-eagle-plus-sun-sensor/ Accuracy: 0.0015 ° Mass: 12 g Supply voltage: 3.3 ## NSS3 Sun Sensor — Serenum Space [sun-sensors] https://newspacemarket.com/products/serenum-nss3-sun-sensor/ Accuracy: 0.02 ° (max) Envelope (L×W×H): 20.5 x 10.5 x 4.8 mm Mass: 3 g Supply voltage: 2.7-3.7 Radiation tolerance (TID): 60 krad (min) Design lifetime: 2 years ## nanoSSOC-D60 Digital Sun Sensor — Solar MEMS Technologies [sun-sensors] https://newspacemarket.com/products/solar-mems-nanosoc-d60-digital-sun-sensor/ Accuracy: 0.5 ° (max) Mass: 5 g (max) Power consumption: 0.1 W (max) Operating temperature: -40 °C Supply voltage: 3.3 ## Nano Sun Sensor on a Chip (NanoSSOC) — Solar MEMS Technologies [sun-sensors] https://newspacemarket.com/products/solar-mems-nanossocd60/ Mass: 5 g (max) Power consumption: 0.1 W (max) ## Sun Sensor — Pyxis Space [sun-sensors] https://newspacemarket.com/products/pyxis-sun-sensor/ Envelope (L×W×H): 7 × 18 × 24 mm³ Mass: 12 g ## Bipropellant Tank with Stiff-Plastic Separation Devices (Diaphragms) — Glavkosmos [tanks-valves] https://newspacemarket.com/products/bipropellant-tank-with-stiff-plastic-separation-devices-diaphragms/ Media / propellant: UDMH/NTO Operating pressure (MEOP): 29.4 bar Mass: 15500 g Media / propellant: 40 dm³ @ (variant 2) Media / propellant: 2.2 dm³ @ (variant 3) Design lifetime: 15 years ## Composite Storage Tank — Glavkosmos [tanks-valves] https://newspacemarket.com/products/composite-storage-tank/ Operating pressure (MEOP): 142 bar Mass: 8700 g Mass: 71000 g @ (variant 2) Volume: 38.2 L Design lifetime: 22 years ## Composite Vessel — Glavkosmos [tanks-valves] https://newspacemarket.com/products/composite-vessel/ Operating pressure (MEOP): 176 bar Mass: 1950 g Mass: 5800 g @ (variant 2) Volume: 18 L Design lifetime: 15 years ## Metal Composite Xenon Tank XT-200 — Glavkosmos [tanks-valves] https://newspacemarket.com/products/metal-composite-xenon-tank-xt-200/ Design lifetime: 19 years Lead time: 12 Volume: 200 L Mass: 350000 g Operating pressure (MEOP): 90 bar Mass: 28000 g @ (variant 2) Design lifetime: 15.5 years @ (variant 2) ## Metal Composite Xenon Tank XT-350 — Glavkosmos [tanks-valves] https://newspacemarket.com/products/metal-composite-xenon-tank-xt-350/ Design lifetime: 19 years Lead time: 12 Volume: 350 L Operating pressure (MEOP): 110 bar Mass: 43500 g Design lifetime: 15.5 years @ (variant 2) ## Monopropellant Tank with Stiff-Plastic Separation Device (Diaphragm) — Glavkosmos [tanks-valves] https://newspacemarket.com/products/monopropellant-tank-with-stiff-plastic-separation-device-diaphragm/ Media / propellant: UDMH, NTO Operating pressure (MEOP): 16.7 bar Mass: 5200 g Media / propellant: 30.8 dm³ @ (variant 2) Media / propellant: 0.65 dm³ @ (variant 3) Design lifetime: 15 years ## Working Medium Tank MVSK — Glavkosmos [tanks-valves] https://newspacemarket.com/products/working-medium-tank-mvsk/ Media / propellant: Hydrazine Operating pressure (MEOP): 13.2 bar Mass: 2500 g Media / propellant: 8.4±0.1 dm³ @ (variant 2) Media / propellant: 0.2 dm³ @ (variant 3) Design lifetime: 12.5 years ## EJK Solenoid Valve — Glavkosmos [tanks-valves] https://newspacemarket.com/products/ejk-solenoid-valve/ Mass: 200 g ## Gas Feed Unit — Glavkosmos [tanks-valves] https://newspacemarket.com/products/gas-feed-unit/ Design lifetime: 19 years Lead time: 9 Media / propellant: 0.2 to 1.2 g/s Operating pressure (MEOP): 1.7 bar Operating temperature: -20-50 °C Design lifetime: 15.25 years @ (variant 2) Mass: 3100 g ## High Pressure Electric Valve — Glavkosmos [tanks-valves] https://newspacemarket.com/products/high-pressure-electric-valve/ Design lifetime: 19 years Lead time: 5 Supply voltage: 23-34 Power consumption: 0.25 W Design lifetime: 15.5 years @ (variant 2) Mass: 120 g ## Low Emission Electric Valve — Glavkosmos [tanks-valves] https://newspacemarket.com/products/low-emission-electric-valve/ Design lifetime: 19 years Lead time: 5 Operating pressure (MEOP): 250 bar Supply voltage: 25-34 Power consumption: 0.25 W Design lifetime: 15.5 years @ (variant 2) Mass: 40 g ## Low Pressure Electric Valve — Glavkosmos [tanks-valves] https://newspacemarket.com/products/low-pressure-electric-valve/ Design lifetime: 19 years Lead time: 5 Supply voltage: 24-34 Power consumption: 0.25 W Design lifetime: 15.5 years @ (variant 2) Mass: 80 g ## Pressure Reducer. Type 1 — Glavkosmos [tanks-valves] https://newspacemarket.com/products/pressure-reducer-type-1/ Design lifetime: 19 years Lead time: 5 Media / propellant: 1.5 to 17 Operating pressure (MEOP): 250-5 bar Operating pressure (MEOP): 1.75 bar Design lifetime: 15.5 years @ (variant 2) Mass: 150 g ## Pressure Reducer. Type 2 — Glavkosmos [tanks-valves] https://newspacemarket.com/products/pressure-reducer-type-2/ Design lifetime: 19 years Lead time: 5 Media / propellant: 4 to 15 mg/s Operating pressure (MEOP): 250-5 bar Operating pressure (MEOP): 2.6 bar Design lifetime: 15.5 years @ (variant 2) Mass: 150 g ## Pressure Reducer. Type 3 (for pressure integrity check unit) — Glavkosmos [tanks-valves] https://newspacemarket.com/products/pressure-reducer-type-3-for-pressure-integrity-check-unit/ Design lifetime: 19 years Lead time: 5 Media / propellant: 0.2 to 1.2 mg/s Operating pressure (MEOP): 1.7 bar Design lifetime: 15.25 years @ (variant 2) Mass: 150 g ## Pressure Reducing Electric Valve — Glavkosmos [tanks-valves] https://newspacemarket.com/products/pressure-reducing-electric-valve/ Design lifetime: 12 years Lead time: 9 Media / propellant: 0.036 to 9 kg/h Operating pressure (MEOP): 350-20 bar Operating pressure (MEOP): 4.5 bar Operating temperature: -40-50 °C Supply voltage: 27 Design lifetime: 10.5 years @ (variant 2) Mass: 1900 g ## Solenoid Valves 12 PT-01 — Glavkosmos [tanks-valves] https://newspacemarket.com/products/solenoid-valves-12-pt-01/ Mass: 40 g ## Solenoid Valves 12 PT — Glavkosmos [tanks-valves] https://newspacemarket.com/products/solenoid-valves-12-pt/ Mass: 40 g ## Solenoid Valves 26 RT-200 — Glavkosmos [tanks-valves] https://newspacemarket.com/products/solenoid-valves-26-%d1%80%d1%82-200/ Mass: 180 g ## Solenoid Valves RT 200-00-01 — Glavkosmos [tanks-valves] https://newspacemarket.com/products/solenoid-valves-%d1%80%d1%82-200-00-01/ Mass: 180 g ## Solenoid Valves RT 200-00-02-03 — Glavkosmos [tanks-valves] https://newspacemarket.com/products/solenoid-valves-%d1%80%d1%82-200-00-02-03/ Mass: 180 g ## Xenon Feed Unit. Type 1 — Glavkosmos [tanks-valves] https://newspacemarket.com/products/xenon-feed-unit-type-1/ Design lifetime: 19 years Lead time: 9 Media / propellant: 1.5 to 17 mg/s Operating pressure (MEOP): 250-5 bar Operating pressure (MEOP): 1.75 bar Operating temperature: -20-50 °C Design lifetime: 15.25 years @ (variant 2) Mass: 2600 g ## Xenon Feed Unit. Type 2 — Glavkosmos [tanks-valves] https://newspacemarket.com/products/xenon-feed-unit-type-2/ Design lifetime: 19 years Lead time: 9 Media / propellant: 4 to 15 mg/s Operating pressure (MEOP): 250-5 bar Operating pressure (MEOP): 2.6 bar Operating temperature: -20-50 °C Design lifetime: 15.5 years @ (variant 2) Mass: 2600 g ## Pressure Stabilization Unit — Glavkosmos [tanks-valves] https://newspacemarket.com/products/pressure-stabilization-unit/ Design lifetime: 10 years Lead time: 12 Media / propellant: (206 - 883) kPa Media / propellant: (167 - 187) kPa @ (variant 2) Power consumption: 5 W Envelope (L×W×H): 304 × 162 × 166 mm Mass: 5000 g (max) ## Propellant Management Assembly (PMA) — Glavkosmos [tanks-valves] https://newspacemarket.com/products/propellant-management-assembly-pma/ Design lifetime: 10 years Lead time: 12 Media / propellant: (1.6 - 1.9 ) kgf/cm2 Operating pressure (MEOP): 1.5 bar Media / propellant: (2..35) mg/s @ (variant 2) Mass: 3000 g ## Xenon Flow Controller for Low Power Plasma Thruster with 50 mm Diameter of the Accelerating Channel — Glavkosmos [tanks-valves] https://newspacemarket.com/products/xenon-flow-controller-for-low-power-plasma-thruster-with-50-mm-diameter-of-the-accelerating-channel/ Design lifetime: 10 years Lead time: 9 Mass: 320 g ## Xenon Flow Controller for Low Power Plasma Thruster with 70 mm Diameter of the Accelerating Channel — Glavkosmos [tanks-valves] https://newspacemarket.com/products/xenon-flow-controller-for-low-power-plasma-thruster-with-70-mm-diameter-of-the-accelerating-channel/ Lead time: 9 Mass: 320 g ## Xenon Flow Controller for Stationary Plasma Thruster with a Discharge Power of up to 5 kW — Glavkosmos [tanks-valves] https://newspacemarket.com/products/xenon-flow-controller-for-stationary-plasma-thruster-with-a-discharge-power-of-up-to-5-kw/ Design lifetime: 16 years Lead time: 9 Mass: 320 g ## Xenon Flow Controller for Stationary Plasma Thruster with a Nominal Discharge Power of 1350 W — Glavkosmos [tanks-valves] https://newspacemarket.com/products/xenon-flow-controller-for-stationary-plasma-thruster-with-a-nominal-discharge-power-of-1350-w/ Design lifetime: 20 years Lead time: 9 Mass: 320 g ## XFC unit — Glavkosmos [tanks-valves] https://newspacemarket.com/products/xfc-unit/ Design lifetime: 16 years Lead time: 9 Operating pressure (MEOP): 1.5 bar Supply voltage: 27 Supply voltage: 8 @ (variant 2) Envelope (L×W×H): 184 × 67 × 158 mm Mass: 1280 g ## VACCO Check and Relief Valves — VACCO Industries [tanks-valves] https://newspacemarket.com/products/vacco-check-and-relief-valves/ Flight heritage: Boeing HS601/HS702, Star-2, FS-1300, DS2000, GPS III, Cygnus, HTV, Solar Dynamics Observatory Operating pressure (MEOP): 37.9212 bar Operating pressure (MEOP): 56.8818 bar @ (variant 2) ## VACCO Fill and Drain Valves — VACCO Industries [tanks-valves] https://newspacemarket.com/products/vacco-fill-and-drain-valves/ Operating pressure (MEOP): 275.7904 bar Operating pressure (MEOP): 413.6856 bar @ (variant 2) Operating temperature: -7 °C Operating temperature: -40 °C @ (variant 2) Random vibration: 17.1 ## VACCO Universal Satellite Pressure Regulator (VUSPR) — VACCO Industries [tanks-valves] https://newspacemarket.com/products/vacco-universal-satellite-pressure-regulator-vuspr/ Media / propellant: Argon, helium, iodine, nitrogen, oxygen, water, xenon Flight heritage: Space Shuttle, SLS, Mars Science Laboratory (Curiosity) descent stage ## 12″ Cryogenic Prevalve — VACCO Industries [tanks-valves] https://newspacemarket.com/products/vacco-launch-vehicle-cryogenic-controls/ Flight heritage: Apollo, Space Shuttle, Space Launch System (SLS) Operating pressure (MEOP): 12.4106 bar Operating pressure (MEOP): 91.0108 bar @ (variant 2) ## Rocket Motor Hardware — Nozzles, Tankages & End Rings — Walchandnagar Industries [tanks-valves] https://newspacemarket.com/products/walchandnagar-rocket-motor-nozzles-tankages-end-rings/ Material: 15CDV6 alloy steel, high-strength maraging steel, titanium alloys, aluminium alloys Flight heritage: ISRO association since 1973 (SLV-3 motor cases) ## Zero Slosh Piston Tanks — Agile Space Industries [tanks-valves] https://newspacemarket.com/products/agile-space-hp250-thruster/ Material: Aluminum and PTFE seals ## memetis Microvalves & Microfluidic Systems — Memetis [tanks-valves] https://newspacemarket.com/products/memetis-nc-microvalves/ Volume: 6.5 L (max) ## memetis Microvalves — Memetis [tanks-valves] https://newspacemarket.com/products/memetis-customized-microvalves/ Material: Over 10 million ## Pressure Vessels and Cryogenic Tanks — MT Aerospace [tanks-valves] https://newspacemarket.com/products/mt-aerospace-tanks/ Material: Carbon fiber composites, metallic structures ## VACCO V1E10362-04 Low Pressure Dual Coil 3/8” Latch Valve — VACCO Industries [tanks-valves] https://newspacemarket.com/products/vacco-v1e10362-04-low-pressure-dual-coil-3-8-latch-valve/ Operating pressure (MEOP): 17.9264 bar Operating pressure (MEOP): 41.3686 bar @ (variant 2) Supply voltage: 21.5-54 ## VACCO V1E10405-04 Low Pressure ¼” Latch Valve — VACCO Industries [tanks-valves] https://newspacemarket.com/products/vacco-v1e10405-04-low-pressure-1-4-latch-valve/ Operating pressure (MEOP): 27.579 bar Operating pressure (MEOP): 62.0528 bar @ (variant 2) Supply voltage: 20-50 ## VACCO V1E10405-05 Low Pressure ¼” Latch Valve — VACCO Industries [tanks-valves] https://newspacemarket.com/products/vacco-v1e10405-05-low-pressure-1-4-latch-valve/ Operating pressure (MEOP): 31.0264 bar Operating pressure (MEOP): 62.0528 bar @ (variant 2) Supply voltage: 21-50 ## VACCO V1E10454-01 ¼” Low Pressure Latch Valve — VACCO Industries [tanks-valves] https://newspacemarket.com/products/vacco-v1e10454-01-1-4-low-pressure-latch-valve/ Operating pressure (MEOP): 31.0264 bar Operating pressure (MEOP): 67.2239 bar @ (variant 2) Supply voltage: 21-38.6 Material: All Titanium with 304L Stainless Steel Interface ## VACCO V1E10691-01 ½” Bi-Directional Latch Valve-Low Pressure — VACCO Industries [tanks-valves] https://newspacemarket.com/products/vacco-v1e10691-01-1-2-bi-directional-latch-valve-low-pressure/ Operating pressure (MEOP): 17.2369 bar Operating pressure (MEOP): 134.4478 bar @ (variant 2) Supply voltage: 18-32 ## VACCO V1E10362-01 Low Pressure Dual Coil 3/8” Latch Valve — VACCO Industries [tanks-valves] https://newspacemarket.com/products/vacco-v1e10362-01-low-pressure-dual-coil-3-8-latch-valve/ Operating pressure (MEOP): 17.9264 bar Operating pressure (MEOP): 41.3686 bar @ (variant 2) Supply voltage: 21.5-54 ## VACCO V1E10453-01 3/8” Low Pressure Propellant Latch Valve — VACCO Industries [tanks-valves] https://newspacemarket.com/products/vacco-v1e10453-01-3-8-low-pressure-propellant-latch-valve/ Operating pressure (MEOP): 20.6843 bar Operating pressure (MEOP): 51.7107 bar @ (variant 2) Supply voltage: 20-38.6 Material: All Titanium with 304L Stainless Steel Interface ## VACCO V1E10689-01 ½” Bi-Directional Latch Valve-Low Pressure — VACCO Industries [tanks-valves] https://newspacemarket.com/products/vacco-v1e10689-01-1-2-bi-directional-latch-valve-low-pressure/ Operating pressure (MEOP): 17.2369 bar Operating pressure (MEOP): 134.4478 bar @ (variant 2) Supply voltage: 18-32 ## Arterial Heat Pipes — Glavkosmos [thermal] https://newspacemarket.com/products/arterial-heat-pipes/ Lead time: 3 Power consumption: 1000 W ## Axial Grooved Heat Pipes — Glavkosmos [thermal] https://newspacemarket.com/products/axial-grooved-heat-pipes/ Lead time: 2 Flight heritage: Successfully operated on more than 100 Russian and foreign satellites Power consumption: 450 W Operating temperature: -133-227 °C ## Contour Heat Pipes — Glavkosmos [thermal] https://newspacemarket.com/products/contour-heat-pipes/ Lead time: 6 ## Low Temperature Heat Pipes — Glavkosmos [thermal] https://newspacemarket.com/products/low-temperature-heat-pipes/ Design lifetime: 23 years Lead time: 3 ## Electric Heaters for Manned Spacecraft — Glavkosmos [thermal] https://newspacemarket.com/products/electric-heaters-for-manned-spacecraft/ Design lifetime: 15 years Lead time: 4 ## Electric Heaters — Glavkosmos [thermal] https://newspacemarket.com/products/electric-heaters/ Design lifetime: 36 years Lead time: 3 Supply voltage: 2-120 Mass: 1-9 g ## Radiation Refrigerator — Glavkosmos [thermal] https://newspacemarket.com/products/radiation-refrigerator/ Design lifetime: 10 years Lead time: 6 ## Loop Heat Pipes (LHPs) — ACT (Advanced Cooling Technologies) [thermal] https://newspacemarket.com/products/act-lhp/ TRL: 6 Operating temperature: -120 °C ## Thermo-Modulating Heat Pipes (TMHPs) — ACT (Advanced Cooling Technologies) [thermal] https://newspacemarket.com/products/act-tmhp/ Envelope (L×W×H): Aluminum-ammonia Radiation tolerance (TID): 600 krad @ up to, Total Ionizing Dose (TID) ## HiK Plates / Heat Pipe Assemblies — ACT (Advanced Cooling Technologies) [thermal] https://newspacemarket.com/products/act-hik-plates/ Operating temperature: 20-150 °C Envelope (L×W×H): alumina Envelope (L×W×H): 29-39 W/m∙K @ (variant 2) Envelope (L×W×H): 10-100 kV/mm @ (variant 3) Power consumption: 64 W Power consumption: 6 W @ (variant 2) ## Vapor Chambers — ACT (Advanced Cooling Technologies) [thermal] https://newspacemarket.com/products/act-vapor-chambers/ Envelope (L×W×H): Up to 10" × 20" ## Thermal Blankets for Space Applications (MLI) — Arquimea [thermal] https://newspacemarket.com/products/arquimea-thermal-blankets-space/ Operating temperature: -150 °C ## Thermo-Structural Radiator Panels for Space — Arquimea [thermal] https://newspacemarket.com/products/arquimea-thermo-structural-panels/ Envelope (L×W×H): Up to 18 m² Operating temperature: -40 °C ## Deployable Radiators for Satellites — Arquimea [thermal] https://newspacemarket.com/products/arquimea-deployable-radiators-satellites/ Power consumption: 1 W ## Heat Pipes for Space Applications (Axial, Arterial, Diode) — Arquimea [thermal] https://newspacemarket.com/products/arquimea-heat-pipes-space/ Power consumption: 5 W ## Loop Heat Pipes for Space Applications — Arquimea [thermal] https://newspacemarket.com/products/arquimea-loop-heat-pipes-space/ Design lifetime: 15 years (min) ## OHP Heat Frames — Thermavant [thermal] https://newspacemarket.com/products/thermavant-ohp-heat-frames/ Operating temperature: -55 °C Mass: 600 g Operating temperature: -55 °C @ (variant 2) Flight heritage: Over 1,000 fielded OHP units for ground application; qualified through MIL-STD thermal cycling, vibration, shock, pressure cycling; TRL 9 ## OHP Chassis — Thermavant [thermal] https://newspacemarket.com/products/thermavant-ohp-chassis/ Mass: 995 g Operating temperature: -20 °C Mass: 1351 g @ (variant 2) Operating temperature: -55 °C @ (variant 2) Flight heritage: 200+ demonstrated OHP chassis units for air and space applications, ~30 currently on orbit; qualified thru MIL-STD thermal cycling, vibration, shock, and pressure cycling (TRL 9) ## OHP Radiators — Thermavant [thermal] https://newspacemarket.com/products/thermavant-ohp-radiators/ Envelope (L×W×H): Al 6061 T4, approx. 19" x 19" x 0.04-0.16" thick (variable thickness) Operating temperature: -20 °C Mass: 3200 g Operating temperature: -55 °C @ (variant 2) Flight heritage: +1,000 on-orbit or delivered-for-launch OHP spacecraft radiators as of mid-2025 (TRL 9); qualified thru MIL-STD vacuum chamber, thermal cycling, vibration, shock, pressure cycling Flight heritage: <10 units qualified and delivered for launch as of mid-2025; not yet deployed on lunar surface as of mid-2025 @ (variant 2) Flight heritage: Co-developed with Albedo: 30% mass reduction and 70% volume savings over legacy thermal systems for VLEO mid-size satellites @ (variant 3) ## Cold Plates — Thermavant [thermal] https://newspacemarket.com/products/thermavant-cold-plates/ Envelope (L×W×H): From less than 1 mm thickness up to 2 m length; customizable widths from < 2 cm to > 1 m; flat or 3D plate with bosses, through or blind holes ## LPT6510 Pulse-tube Cryocooler — Thales Cryogenics [thermal] https://newspacemarket.com/products/thales-cryogenics-lpt6510/ Random vibration: 2 (max) Mass: 3200 g (max) ## LPT 9310 HP COTS+ — Thales Cryogenics [thermal] https://newspacemarket.com/products/thales-cryogenics-lpt-9310-hp-cots/ Envelope (L×W×H): 24 x 90 x 204 mm ## LPT 9510 COTS+ — Thales Cryogenics [thermal] https://newspacemarket.com/products/thales-cryogenics-lpt-9510-cots/ Power consumption: 85 W Envelope (L×W×H): 18 x 122 x Ø 60 mm ## Copper Cable Thermal Straps (CuTS) — Technology Applications Inc (TAI) [thermal] https://newspacemarket.com/products/tai-thermal-cuts-copper-strap/ Flight heritage: NASA TRL 9 Warranty: 1 ## Cryocooler Series Thermal Straps (CS-CuTS) — Technology Applications Inc (TAI) [thermal] https://newspacemarket.com/products/tai-thermal-cryocooler-series-straps/ Lead time: 6-7 ## Graphite Fiber Thermal Straps (GFTS) — Technology Applications Inc (TAI) [thermal] https://newspacemarket.com/products/tai-thermal-gfts-graphite-fiber-strap/ Flight heritage: NASA TRL 9; flown on Orion, ASTRO-H, CST-100 Starliner, Solar Orbiter, EnMAP, IXPE ## PyroFlex PGS & Graphene Thermal Straps (X-Series) — Technology Applications Inc (TAI) [thermal] https://newspacemarket.com/products/tai-thermal-pyroflex-pgs-graphene-strap/ Flight heritage: NASA TRL 9; flown on Orion (Artemis II/III), Blue Origin New Glenn, JHU APL IMAP, HyTI CubeSat, Turion Space DROID 002 Lead time: 8-10 ## k-Core Encapsulated Graphite Thermal Solutions — Boyd Corporation [thermal] https://newspacemarket.com/products/boyd-corporation-k-core-encapsulated-graphite/ Operating temperature: -40 °C Flight heritage: NASA/JHU-APL DART mission radiator panels (2022); U.S. Space Force WSF-M/USSF-62 thermal doubler (2024) ## Pridwen Heatshield — Space Forge Limited [thermal] https://newspacemarket.com/products/spaceforge-pridwen/ Flight heritage: Parabolic flight deployment test (May 2025); operational on ForgeStar-1 (June 2025) ## Control unit of the thermal regime support system — SPUTNIX [thermal] https://newspacemarket.com/products/control-unit-of-the-thermal-regime-support-system/ Envelope (L×W×H): 200 x 130 x 30 mm Mass: 600 g Supply voltage: 22-33 Power consumption: 5 W Power consumption: 60 W @ (variant 2) ## PSG Thermal Links (Pyrolytic Graphite Flexible Thermal Straps) — Lidax [thermal] https://newspacemarket.com/products/lidax-psg-thermal-links/ Flight heritage: BepiColombo, EarthCARE, PLATO, James Webb Space Telescope ## xRAD™ Extruded Thermal Control Radiator — Paragon Space Development Corporation [thermal] https://newspacemarket.com/products/paragon-xrad-thermal-control-radiator/ Flight heritage: Sierra Space Dream Chaser Cargo Module ## Altom14 Series — LHP Evaporator Modules for Power Electronics — Allatherm [thermal] https://newspacemarket.com/products/allatherm-altom14-lhp-power-electronics/ Envelope (L×W×H): 40×160 mm (1SL), 100×140 mm (2CPL) ## OrbShield™ — Orbital Composites [thermal] https://newspacemarket.com/products/orbital-composites-orbshield/ Envelope (L×W×H): 1U Envelope (L×W×H): available upon request @ (variant 2) ## Aerospace Thermal Control Materials — Sheldahl (Multek Flexible Circuits) [thermal] https://newspacemarket.com/products/sheldahl-aerospace-thermal-control/ Flight heritage: Space thermal control material heritage since 1958 ## IberEspacio Satellite Thermal Control Hardware — Arquimea [thermal] https://newspacemarket.com/products/iberespacio-thermal-control-systems/ Design lifetime: 15 years (min) Flight heritage: Sentinel-1/2/6, Alphasat, ExoMars, EDRS-A/C, Intelsat 19/20, Star One C4, Astro-H ## KULR Thermal Runaway Shield for Space — KULR Technology [thermal] https://newspacemarket.com/products/kulr-thermal-runaway-shield/ Flight heritage: NASA Orion MPCV (crew vehicle) program qualification ## Custom Cryostats — Lidax [thermal] https://newspacemarket.com/products/lidax-custom-cryostats/ Envelope (L×W×H): In-house test asset volume: 300 x 300 mm ## COOLCAT Cryogenic Superinsulation — Beyond Gravity (ex-RUAG Space) [thermal] https://newspacemarket.com/products/beyond-gravity-coolcat-cryogenic-superinsulation/ Envelope (L×W×H): Maximum width 2.7 m, maximum length 3.0 m ## Flexible Thermal Protection for Launchers — Beyond Gravity (ex-RUAG Space) [thermal] https://newspacemarket.com/products/beyond-gravity-flexible-thermal-protection-launchers/ Mass: 1270-1650 g Mass: 510 g Mass: 280 g @ (variant 2) Mass: 30-120 g @ (variant 2) ## Satellite Multi-Layer Insulation (MLI) — Beyond Gravity (ex-RUAG Space) [thermal] https://newspacemarket.com/products/beyond-gravity-satellite-multi-layer-insulation/ Flight heritage: MLI for over 800 satellites across 50 space projects; Euclid, Juice, BepiColombo, Eutelsat OneWeb, Galileo ## Thermal Control Unit — CAVU Aerospace [thermal] https://newspacemarket.com/products/thermal-control-unit/ Envelope (L×W×H): 160 mm × 170 mm × 38 mm Power consumption: 1.5 W Supply voltage: 28 Design lifetime: 3-5 years ## Sun Shields — Aerospace Fabrication and Materials, LLC [thermal] https://newspacemarket.com/products/sun-shields/ Envelope (L×W×H): up to 3 meters ## PolaWrap™ — Aerospace Fabrication and Materials, LLC [thermal] https://newspacemarket.com/products/polawrap/ Layers (MLI): 0.34 Layers (MLI): 0.034 @ (variant 2) Layers (MLI): 29 @ (variant 3) Layers (MLI): 0.51 @ (variant 4) Layers (MLI): 0.56 @ (variant 5) Layers (MLI): 31 @ (variant 6) Layers (MLI): 0.68 @ (variant 7) Layers (MLI): 0.62 @ (variant 8) Layers (MLI): 32 @ (variant 9) ## Scintilla Propulsion Engine — Space Machines Company [propulsion] https://newspacemarket.com/products/smc-scintilla-propulsion-engine/ Thrust: 50000 mN ## Hybrid Rocket Motors — DELTAV Space Technologies [propulsion] https://newspacemarket.com/products/hibrit-roket-teknolojileri/ Thrust: 1000 mN ## WiRan S-Band antenna — WiRan [antennas] https://newspacemarket.com/products/wiran-s-band-antenna/ Frequency band: S Frequency: 2025-2290 MHz Gain: 7.5 Beamwidth: 70 (max) Polarization: RHCP @ by default Polarization: LHCP @ available Antenna type: omni-directional coverage patch antenna Mass: 87 g Envelope (L×W×H): 95 x 95 x 17.7 mm (height without connector) Connector: SMA female Operating temperature: -75-90 °C Flight heritage: flight-proven ## S-Band Diplexer — WiRan [antennas] https://newspacemarket.com/products/wiran-s-band-diplexer/ Frequency band: S Frequency: 2025-2290 Mass: 220 g Envelope (L×W×H): 80 x 29 Power consumption: 2.5 W Connector: SMA female Operating temperature: -40-75 °C Flight heritage: flight-proven ## WiRan X-Band Antenna — WiRan [antennas] https://newspacemarket.com/products/wiran-x-band-antenna/ Frequency band: X Frequency: 7145-7235 MHz Frequency: 8000-8500 MHz @ (variant 2) Gain: 9.5 Beamwidth: 45 Polarization: RHCP Antenna type: X-band antenna Mass: 39 g Envelope (L×W×H): 95 (X or Y) Envelope (L×W×H): 24.5 (Z) @ (variant 2) Envelope (L×W×H): 21.5 (height without connector) @ (variant 3) Power consumption: 15 W Connector: SMP male connector Operating temperature: -75-90 °C ## SPAN-X-T3 — Syrlinks [antennas] https://newspacemarket.com/products/syrlinks-span-x-t3-patch-antenna/ Frequency band: X Antenna type: Patch design Flight heritage: Q1-2018 (upon request) ## SPAN-S-T3 — Syrlinks [antennas] https://newspacemarket.com/products/syrlinks-span-s-t3-patch-antenna/ Frequency band: S Antenna type: Patch design Flight heritage: Q1-2018 (upon request) ## BEAMSAT K-Band Patch Antenna — PicoSaTs [antennas] https://newspacemarket.com/products/picosats-beamsat-k-band-patch-antenna/ Antenna type: Patch antenna Frequency band: K Frequency: 17300-21200 MHz Gain: 22 Beamwidth: 10.2 Polarization: LHCP Connector: SMP Mass: 135 g @ with enclosure Envelope (L×W×H): 110.0 mm x 96.0 mm x 14.0 mm @ with enclosure ## VISION 300 Optical Payload — Satrev (SatRevolution) [cameras] https://newspacemarket.com/products/satrev-vision-300-optical-payload/ Focal length: 300 Focal length: 5.6 @ f-number Spectral bands: 4 @ RGB, B, NIR Ground sample distance: 5.8 m @ @500 km ## GAUSS Mini Ground Dongle — GAUSS Srl [ground-stations] https://newspacemarket.com/products/gauss-mini-ground-dongle/ Frequency band: UHF @ for TT&C EIRP: -15 dBW (max) Data rate: 0.3 kbps (min) Data rate: 100 kbps (max) Data rate: 250 kbps @ with 4GFSK Data interface: USB Connector: SMA connector for antenna ## ASTROFEIN ACM Magnetometer — EXA (Astro-und Feinwerktechnik) [magnetometers] https://newspacemarket.com/products/acm-magnetometer/ Measurement range: 60 µT (max) @ up to 140000 nT on request Resolution: 100 nT Noise density: 150 nT @ @ 60000 nT Mass: 280 g (max) @ without connector Envelope (L×W×H): 138 mm x 55 mm x 39 mm Supply voltage: 16-40 Power consumption: 1 W (max) @ @ 24 V, Earth field Power consumption: 1.2 W (max) @ @ 24 V, Full range Data interface: RS-485 @ others on request Operating temperature: -20-50 °C Survival temperature: -30-60 °C Design lifetime: 7 years ## ABACUS On-Board Computer — GAUSS Srl [obc-computers] https://newspacemarket.com/products/gauss-abacus-obc/ Processor: Two cores (MCU MSP430 and FPGA Spartan-3E) CPU clock: 25 MHz @ running up to CPU clock: 25 MHz @ FPGA running at RAM: 16 MB Storage: 2 GB Storage: 0.0156 GB @ (variant 2) Mass: 59 g @ about Supply voltage: 5 @ powered from Power consumption: 0.05 W @ for low power consumption Data interface: RS422/485 Data interface: I2C @ (variant 2) Data interface: SPI @ (variant 3) Data interface: LVDS @ (variant 4) Operating temperature: -40 °C @ operating temperature range Operating temperature: 85 °C @ operating temperature range (variant 2) Flight heritage: UniCubeSat-GG (2012 , CubeSat 1U); UniSat-5 (2013, microsatellite of 32kg); UniSat-6 (2014, microsatellite of 26kg); TigriSat (2014, CubeSat 3U); Serpens (2015, CubeSat 3U). ## Lyra 1 — Tesseract [propulsion] https://newspacemarket.com/products/tesseract-lyra-1/ Propulsion type: chemical Thrust: 1000 mN Specific impulse: 280 (max) Min impulse bit: 2.7 mN·s @ minimum Mass: 240 g ## Lyra 22 — Tesseract [propulsion] https://newspacemarket.com/products/tesseract-lyra-22/ Thrust: 22000 mN Specific impulse: 300 (min) Min impulse bit: 110 mN·s Mass: 590 g ## Rigel 500 — Tesseract [propulsion] https://newspacemarket.com/products/tesseract-rigel-500/ Thrust: 500000 mN Thrust: 498200.64 mN @ (variant 2) Specific impulse: 300 (min) Specific impulse: 2942 (min) @ (variant 2) Mass: 3500 g Mass: 7.7 g @ (variant 2) ## GAUSS RADIO UHF – 2W/5W — GAUSS Srl [radios] https://newspacemarket.com/products/gauss-uhf-radio/ TX power: 5 W Frequency band: UHF Data rate: 300 kbps (min) Data rate: 100000 kbps (max) RX sensitivity: -122 @ 300bps RX sensitivity: -119 @ 9.6kbps RX sensitivity: -109 @ 50kbps Data interface: I2C Data interface: UART @ (variant 2) Data interface: SPI @ (variant 3) Data interface: CAN @ (variant 4) Modulation: FSK/MSK/GFSK/GMSK Supply voltage: 3.3 @ logic Supply voltage: 7 @ power amplifier Supply voltage: 12 @ power amplifier (variant 2) Operating temperature: -40 °C (min) Operating temperature: 110 °C (max) Connector: SMA Connector: MCX @ (variant 2) Data interface: USB @ Mini Ground Dongle ## EDT-01 Series Telemetry Transmitters — Emhiser Research [radios] https://newspacemarket.com/products/digital-transmitters-edt-series/ Frequency: 1435.5 MHz (min) @ single frequency or channelized Frequency: 2399.5 MHz (max) @ single frequency or channelized TX power: 0.15 W TX power: 0.5 W @ (variant 2) TX power: 1 W @ (variant 3) TX power: 2 W @ (variant 4) Data rate: 100 kbps (max) Data rate: 1200 kbps (max) @ (variant 2) Modulation: digital Modulation: telemetry @ (variant 2) Modulation: video @ (variant 3) Mass: 3 g Envelope (L×W×H): 3.3 Inches (L) x 1.3 Inches (W) x 1.865 Inches (H) Supply voltage: 12 (nominal) Supply voltage: 28 (nominal) @ (variant 2) Power consumption: 0.15 W @ maximum input Power consumption: 0.2 W @ maximum input (variant 2) Power consumption: 0.4 W @ maximum input (variant 3) Power consumption: 0.65 W @ maximum input (variant 4) Power consumption: 2 W @ maximum input (variant 5) Power consumption: 3 W @ maximum input (variant 6) Data interface: RS-422 Data interface: RS-485 @ (variant 2) Operating temperature: -20 °C (min) Operating temperature: 70 °C (max) Survival temperature: -55 °C (min) Survival temperature: 100 °C (max) ## HIRCOM CubeSat UHF Transceiver — HIRCOM [radios] https://newspacemarket.com/products/hircom-cubesat-uhf-transceiver/ Frequency band: UHF Frequency: 400-438 MHz TX power: 1.585 W @ Maximum Output Power Data rate: 1.2-9.6 kbps @ baud rate RX sensitivity: -30 @ Maximum RX Input Power Modulation: GMSK/AFSK Mass: 85 g Envelope (L×W×H): 95mmX90mmX15mm Supply voltage: 3.3 @ Transceiver and controller Supply voltage: 5 @ Power amplifier Power consumption: 0.63 W @ Receiving Mode Power consumption: 4.8 W @ Transmitting Mode Power consumption: 0.11 W @ Low Power Mode Data interface: CAN Data interface: SPI @ (variant 2) Data interface: other @ RF Operating temperature: -35-80 °C ## EWC27 – X-Band Transmitter — Syrlinks [radios] https://newspacemarket.com/products/syrlinks-ewc27-x-band-transmitter/ Data rate: 100000 kbps @ High DataRate TeleMetry Design lifetime: 2 years @ LEO missions Flight heritage: GOMX-3, ESA-Gomspace (2015) Flight heritage: OHB group (2017) @ (variant 2) Flight heritage: EYE-SAT, CINES (2017) @ (variant 3) Flight heritage: OPS-SAT, ESA (2018) @ (variant 4) Flight heritage: HawkEye 360 (2017/2018) @ (variant 5) Flight heritage: Based on EWC28 family XBT series inflight proven (2013) @ (variant 6) ## EWC31 – S/S Band Transponder — Syrlinks [radios] https://newspacemarket.com/products/syrlinks-ewc31-ss-band-transponder/ Design lifetime: 2 years @ LEO missions Flight heritage: EYE-SAT, CNES (2017) Flight heritage: OPS-SAT, ESA (2018) @ (variant 2) ## EWC34 – Ultra High Speed X-Band Transmitter — Syrlinks [radios] https://newspacemarket.com/products/syrlinks-ewc34-x-band-transmitter/ Data rate: 600000 kbps @ High performance Modulation: 8PSK 4D TCM Design lifetime: 10 years @ LEO missions Flight heritage: Pléiades Neo, Airbus D&S (April & August 2021, 2 others in 2022) ## EWC15-NG – S/S-Band Transceiver – CCSDS — Syrlinks [radios] https://newspacemarket.com/products/syrlinks-ewc15-ng-ss-band-transceiver/ Design lifetime: 7 years @ LEO missions ## Solar arrays — Hemeria [solar-panels] https://newspacemarket.com/products/solar-arrays/ Design lifetime: 8 years Flight heritage: solar arrays for the KINEIS constellation (180), and for the Idefix rover (MMX) ## C-band Band-pass Filter — Glavkosmos [antennas] https://newspacemarket.com/products/c-band-band-pass-filter/ Frequency band: C ## Multiple-beam Feed — Glavkosmos [antennas] https://newspacemarket.com/products/multiple-beam-feed/ Antenna type: critical component of a mirror antenna system Frequency band: Ka Frequency band: Q @ (variant 2) ## Hydra 2 — Dual-Link Ka Satellite Terminal — All.Space [antennas] https://newspacemarket.com/products/allspace-hydra-2/ Frequency band: Ka Frequency band: Ka @ (variant 2) ## Hydra 4 — Quad-Link Multi-Band MilSatCom Terminal — All.Space [antennas] https://newspacemarket.com/products/allspace-hydra-4/ Frequency band: Ka Frequency band: Ku @ (variant 2) Frequency band: L @ (variant 3) ## Gimbaled Deployable Ka-Band Antenna for CubeSats and SmallSats — Arquimea [antennas] https://newspacemarket.com/products/arquimea-deployable-ka-band-antenna/ Frequency band: Ka Frequency: 26500-40000 MHz Antenna type: gimbaled deployable Ka-band antenna Flight heritage: flight-proven ## L-Band Single Patch Antenna (PATCH1-L-R) — Space Inventor ApS [antennas] https://newspacemarket.com/products/l-band-single-patch-antenna-patch1-l-r/ Frequency band: L Frequency: 1518-1560 MHz Frequency: 1626-1675 MHz @ (variant 2) Antenna type: patch ## PATCH1-S-R — Space Inventor ApS [antennas] https://newspacemarket.com/products/s-band-single-patch-antenna-patch1-s-r/ Frequency band: S Frequency: 2025-2110 MHz Frequency: 2200-2290 MHz @ (variant 2) Antenna type: patch Flight heritage: used across multiple Space Inventor satellite platforms, including the Space Domain Awareness microsatellite, Geostationary BIU Microsatellite, ESM Satellite Platform, Astro Observatory, 16U GEO for BIU, 16U Hyperspectral 200mm, 16U Satellite, 12U Satelli ## S-Band 2×2 Antenna Array (PATCH2X2-S-R) — Space Inventor ApS [antennas] https://newspacemarket.com/products/s-band-2x2-antenna-array-patch2x2-s-r/ Frequency band: S Antenna type: patch ## X-Band Patch 4 antenna — Space Inventor ApS [antennas] https://newspacemarket.com/products/x-band-4x4-antenna-array-patch4x4-x-r/ Frequency band: X Frequency: 7250-7750 MHz Antenna type: patch ## EXA GCA01 – Compact GNSS Active Patch Antenna — EXA (Ecuadorian Space Agency) [antennas] https://newspacemarket.com/products/exa-gca01-compact-gnss-active-patch-antenna/ Antenna type: active patch Frequency band: L ## EXA SSA01 – Wide Bandwidth S-band Patch Antenna — EXA (Ecuadorian Space Agency) [antennas] https://newspacemarket.com/products/exa-ssa01-wide-bandwidth-s-band-patch-antenna/ Frequency band: S Frequency: 2025-2120 MHz Frequency: 2200-2300 MHz @ (variant 2) Antenna type: patch ## EXA SSA02- 34dB Wide Bandwidth amplified S-band Patch Antenna — EXA (Ecuadorian Space Agency) [antennas] https://newspacemarket.com/products/exa-ssa02-34db-wide-bandwidth-amplified-s-band-patch-antenna/ Frequency band: S Antenna type: Patch Antenna Lead time: immediately ## Multi-Band Antenna — Helical Communication Technologies (HCT) [antennas] https://newspacemarket.com/products/hct-multi-band-antenna/ Frequency: 100-3000 Antenna type: multi-band antenna ## Parabolic Series Maritime — Intellian Technologies [antennas] https://newspacemarket.com/products/intellian-oneweb-parabolic-maritime/ Operating temperature: -40 °C (min) ## Antenna Feeds & Feed Clusters — Optisys [antennas] https://newspacemarket.com/products/optisys-antenna-feeds-feed-clusters/ Antenna type: antenna feeds Frequency band: L Frequency band: S @ (variant 2) Frequency band: C @ (variant 3) Frequency band: X @ (variant 4) Frequency band: Ku @ (variant 5) Frequency band: Ka @ (variant 6) ## Ka user terminal — Greenerwave [antennas] https://newspacemarket.com/products/ka-user-terminal/ Frequency band: Ka ## AirTRx 30Ka Business Aviation SATCOM — Orbit Communication Systems [antennas] https://newspacemarket.com/products/airtrx-30ka-business-aviation-satcom/ Frequency band: Ku Frequency band: Ka @ (variant 2) Data interface: Ethernet Data interface: other @ (variant 2) Data interface: other @ (variant 3) ## SWATH – Spiral Wrap Antenna Technology — Opterus Research and Development [antennas] https://newspacemarket.com/products/swath/ Frequency: 100000 MHz (min) Antenna type: deployable solid surface parabolic dish antenna ## VICTS Phased Array – Commercial In-Flight Connectivity Antenna — ThinKom Solutions, Inc. [antennas] https://newspacemarket.com/products/thinkom-victs-commercial-ifc-antenna/ Frequency band: Ku Frequency band: Ka @ (variant 2) Antenna type: phased array ## VICTS Gateway Array Antenna — ThinKom Solutions, Inc. [antennas] https://newspacemarket.com/products/thinkom-victs-gateway-array/ Frequency band: Ka Frequency band: V @ (variant 2) Antenna type: electronically steered array ## Satellite Terminals (Aurora / Ares) — Thorium Space Technology [antennas] https://newspacemarket.com/products/thorium-satellite-terminals/ Frequency: 27500000 MHz (min) @ Tx Frequency: 31000 MHz (max) @ Tx Frequency: 17700000 MHz (min) @ Rx Frequency: 21200000 MHz (max) @ Rx Antenna type: phased array Data interface: Ethernet ## Direct Radiating Array Antenna — Anywaves [antennas] https://newspacemarket.com/products/direct-radiating-array-antenna/ Frequency band: Ku Frequency band: Ka @ (variant 2) Gain: 30 (min) Polarization: LHCP Polarization: RHCP @ (variant 2) Antenna type: patch array ## KULR ONE Space (K1S) Battery System — KULR Technology [batteries] https://newspacemarket.com/products/kulr-one-space-k1s-battery/ Capacity: 100 Wh @ series configuration Capacity: 200 Wh @ series configuration (variant 2) Capacity: 300 Wh @ LT series configuration Capacity: 400 Wh @ series configuration (variant 3) Cell chemistry: lithium-ion cells Connector: space-rated connectors ## GRAPHIUM Very High Resolution Telescope — Satlantis [cameras] https://newspacemarket.com/products/satlantis-graphium/ Ground sample distance: 0.5 m ## Quantum Camera Platform — Diffraqtion [cameras] https://newspacemarket.com/products/diffraqtion-galileo-1-vspu/ Data interface: USB Connector: USB-C Connector: M8/M12 @ (variant 2) Connector: custom outputs @ (variant 3) ## 0.5m panchromatic(PAN) & 2m multispectral(MS) Camera — MinoSpace [cameras] https://newspacemarket.com/products/minospace-camera-0-5m-pan-2m-ms/ Ground sample distance: 0.5 m @ panchromatic Ground sample distance: 2 m @ multispectral Swath width: 12 km (min) ## 1U visible light camera — MinoSpace [cameras] https://newspacemarket.com/products/minospace-camera-10m-visible/ Ground sample distance: 10 m Flight heritage: successfully deployed on multiple satellites utilizing the company’s MN10 platform ## 2m panchromatic(PAN) & 8m multispectral(MS) camera — MinoSpace [cameras] https://newspacemarket.com/products/minospace-camera-2m-pan-8m-ms/ Ground sample distance: 2 m @ panchromatic Ground sample distance: 8 m @ multispectral Mass: 2670 g @ approx Swath width: 15.8 km @ greater than ## SpaceTV-1 — Live 4K ISS Earth Streaming Camera Payload — Sen [cameras] https://newspacemarket.com/products/sen-spacetv-1-iss-payload/ Ground sample distance: 60 m @ nadir camera Swath width: 240 km @ nadir camera; horizontal scene dimension Swath width: 180 km @ nadir camera; vertical scene dimension ## SMPOD03-NOIR — NPC Spacemind [deployers] https://newspacemarket.com/products/npc-spacemind-smpod03-noir/ Capacity: 1-3 ## SMPOD16-C — NPC Spacemind [deployers] https://newspacemarket.com/products/npc-spacemind-smpod-deployer/ Actuation: non-pyro ## SmallSat EPS — EnduroSat [eps] https://newspacemarket.com/products/endurosat-smallsat-eps/ Output rails: 12, 28 V Supply voltage: 30-50 @ System bus (vBatt) Mass: 19.5 g @ base ## Power Distribution Unit — Space Inventor ApS [eps] https://newspacemarket.com/products/power-distribution-unit-pdu-p4/ Output rails: battery voltage feedthrough (normal and high power), regulated 12-volt output, regulated 5-volt output, regulated 3.3-volt variant Protections: current sensing on all 8 outputs, programmable battery input under and overvoltage protection, output channel current limits Data interface: CAN Connector: 4 rugged 8-pin M80 connectors ## PCDU NANO Power Conditioning and Distribution Unit — EREMS [eps] https://newspacemarket.com/products/erems-pcdu-nano/ Output power (total): 10 W @ Distribution module @5V Output power (total): 6 W @ Distribution module @3.3V Output power (total): 50 W @ Conversion & distribution module @28V Output rails: 5V @ Distribution module Output rails: 3.3V @ Distribution module (variant 2) Output rails: 28V @ Conversion & distribution module Protections: LCL-protected @ Distribution module Protections: LCL @ Conversion & distribution module ## Vyunok Educational Satellite Data Reception Station — SPUTNIX [ground-stations] https://newspacemarket.com/products/sputnix-vyunok-educational-station/ Frequency: 136-146 MHz Frequency: 435-438 MHz @ (variant 2) Data rate: 9600 kbps @ Max ## General Dynamics Satellite Ground Terminal — 7.3-Metre Earth Station Antenna — General Dynamics Mission Systems [ground-stations] https://newspacemarket.com/products/general-dynamics-satellite-ground-terminal-7-3-metre-earth-station-antenna/ Frequency band: X @ TX/RX Frequency band: Ka @ TX/RX (variant 2) ## Xen-Node — Xenesis [ground-stations] https://newspacemarket.com/products/xenesis-xen-node/ Data interface: Ethernet Data interface: Ethernet @ (variant 2) ## skyEGSE-comm (S-band) — SkyLabs d.o.o. [ground-stations] https://newspacemarket.com/products/skylabs-skyegse-comm-sband/ Frequency band: S @ TX/RX ## skyEGSE-comm (UHF/VHF) — SkyLabs d.o.o. [ground-stations] https://newspacemarket.com/products/skylabs-skyegse-comm-uhf-vhf/ Frequency band: UHF @ TX/RX Frequency band: VHF @ TX/RX (variant 2) Frequency: UHF/VHF ## ELARA X-Band Multibeam Ground Antenna — Quasar Satellite Technologies [ground-stations] https://newspacemarket.com/products/qsat-elara-x-band-multibeam-antenna/ Frequency band: X ## QS RF Measurement System (QS 1-18 DL) — Quadsat ApS [ground-stations] https://newspacemarket.com/products/quadsat-qs-rf-1-18-dl/ Frequency: 1000 MHz (min) Frequency: 18000 MHz (max) Frequency band: L @ Applicable bands Frequency band: S @ Applicable bands (variant 2) Frequency band: Ku @ Applicable bands (variant 3) ## Leaf Key — Dedicated Ground Station — Leaf Space [ground-stations] https://newspacemarket.com/products/leaf-space-leaf-key/ Frequency band: S @ TX/RX Frequency band: X @ TX/RX (variant 2) ## Equatorial Stargate — Astralintu Space Technologies [ground-stations] https://newspacemarket.com/products/astralintu-equatorial-stargate/ Frequency band: S @ TX/RX Frequency band: X @ TX/RX (variant 2) Frequency band: Ka @ TX/RX (variant 3) Antenna diameter: 3.7 m @ initial operation Q4 2026 Antenna diameter: 7.3 m @ initial operation Q4 2026 (variant 2) Antenna diameter: 5.4 m @ future expansion ## S-Band Receiver for HISPICO (Ground Station) — IQ Spacecom [ground-stations] https://newspacemarket.com/products/s-band-receiver-for-hispico-ground-station/ Lead time: 4 ## EMPOSAT 1.8m Portable Ground Station — Emposat Co., Ltd. [ground-stations] https://newspacemarket.com/products/1-8m-portable-ground-station/ Frequency band: S @ standard Frequency band: X @ standard (variant 2) Frequency band: C @ optional Frequency band: Ka @ optional (variant 2) Data rate: 100000 kbps @ X-band Antenna diameter: 1.8 m ## LNB/LNA Low Noise Amplifiers — EUROSATCOM [ground-stations] https://newspacemarket.com/products/eurosatcom-lnb-lna-amplifiers/ Frequency band: C @ LNB Frequency: 3400000-4200000 MHz Frequency band: Ku @ LNB (variant 2) Frequency: 10700000-12750000 MHz @ (variant 2) Frequency band: Ka @ LNB (variant 3) Frequency: 17700000-22200000 MHz @ (variant 3) ## Tracker 6000 X/C Band Tracking Antenna — CM Technology (CMT) [ground-stations] https://newspacemarket.com/products/cmt-tracker-6000-xc-band/ Frequency band: X @ Frequency Frequency band: C @ Frequency (variant 2) ## The Array — Commercial Dish Array Network — Cascade Space [ground-stations] https://newspacemarket.com/products/cascadespace-the-array/ Frequency band: S @ Mini configuration G/T: 25.6 @ Mini configuration EIRP: 66.9 dBW @ Mini configuration Frequency band: X @ Mini configuration (variant 2) G/T: 35.4 @ Mini configuration (variant 2) EIRP: 76.9 dBW @ Mini configuration (variant 2) Frequency band: S @ Lunar configuration G/T: 28.6 @ Lunar configuration EIRP: 72.9 dBW @ Lunar configuration Frequency band: X @ Lunar configuration (variant 2) G/T: 38.4 @ Lunar configuration (variant 2) EIRP: 82.9 dBW @ Lunar configuration (variant 2) Frequency band: S @ Deep configuration G/T: 37.7 @ Deep configuration EIRP: 91 dBW @ Deep configuration Frequency band: X @ Deep configuration (variant 2) G/T: 47.5 @ Deep configuration (variant 2) EIRP: 101 dBW @ Deep configuration (variant 2) Frequency band: S @ Deep+ configuration G/T: 42.6 @ Deep+ configuration EIRP: 101 dBW @ Deep+ configuration Frequency band: X @ Deep+ configuration (variant 2) G/T: 52.4 @ Deep+ configuration (variant 2) EIRP: 111 dBW @ Deep+ configuration (variant 2) ## HAWK Optical Ground Station — Mynaric [ground-stations] https://newspacemarket.com/products/mynaric-hawk-optical-ground-station/ Data rate: 200000 kbps @ aggregate per site ## MinoPad portable station — MinoSpace [ground-stations] https://newspacemarket.com/products/minospace-minopad/ Antenna diameter: 0.3 m @ equivalent-aperture Frequency band: Ku @ RX Frequency band: Ku @ TX Mass: 5500 g ## 0.6 m Portable Monitoring Antenna — MinoSpace [ground-stations] https://newspacemarket.com/products/minospace-ttc-station-0-6m-kaku/ Antenna diameter: 0.6 m ## S-Band Multibeam Phased Array Ground Station — Quasar Satellite Technologies [ground-stations] https://newspacemarket.com/products/quasar-sband-phased-array/ Frequency band: S @ TX/RX ## X-Band Multibeam Phased Array Ground Station — Quasar Satellite Technologies [ground-stations] https://newspacemarket.com/products/quasar-xband-phased-array/ Frequency band: X @ TX/RX ## Ground Station as a Service (GSaaS) — Spacecomm [ground-stations] https://newspacemarket.com/products/spacecomm-satcom-platform/ Frequency band: C @ ground station infrastructure Frequency band: VHF @ ground station infrastructure (variant 2) Frequency band: UHF @ ground station infrastructure (variant 3) ## VICTS Ground Terminal – Mobile and Fixed SATCOM — ThinKom Solutions, Inc. [ground-stations] https://newspacemarket.com/products/thinkom-victs-ground-terminal/ Frequency band: Ku @ TX/RX Frequency band: Ka @ configurable ## X-band Satellite Data Reception Station — Lorett [ground-stations] https://newspacemarket.com/products/lorett-xband-ground-station/ Frequency band: X @ RX ## Global Ground Station Network — KSAT (Kongsberg Satellite Services) [ground-stations] https://newspacemarket.com/products/ksat-ground-station-network/ Frequency band: X @ downlink Frequency band: S @ downlink (variant 2) Frequency band: Ka @ downlink (variant 3) Frequency band: S @ uplink Frequency band: X @ uplink (variant 2) ## Ground Station Network — GEOVIS / Zhongke Xingtu [ground-stations] https://newspacemarket.com/products/ground-station-network-3807/ Frequency band: S @ RX Frequency band: X @ RX (variant 2) Frequency band: Ka @ RX (variant 3) Data rate: 2000000 kbps @ RX ## Mobile Station Centre — Groundcom.space [ground-stations] https://newspacemarket.com/products/mobile-station-centre/ Data rate: 300000 kbps ## Small-sized Unit for Measuring Angular Velocity 2 — Glavkosmos [imus-gyros] https://newspacemarket.com/products/small-sized-unit-for-measuring-angular-velocity-2/ Supply voltage: 27 (nominal) Power consumption: 52 W (max) Mass: 6100 g ## Spacemag®-2 — Bartington Instruments [magnetometers] https://newspacemarket.com/products/spacemag-2/ Noise density: 0.02 nT @ at 1 Hz Flight heritage: Deployed in space aboard Iota Technology’s CubeSat Io-1 satellite, launched March 30, 2026 ## Magnetic torquers — SPUTNIX [magnetorquers] https://newspacemarket.com/products/magnetic-torquers/ Magnetic dipole moment: 1 A·m² @ sx-mt-1 Power consumption: 0.4 W @ sx-mt-1 Mass: 200 g @ sx-mt-1 Envelope (L×W×H): 140x30x30 mm @ sx-mt-1 Magnetic dipole moment: 5 A·m² @ sx-mt-5 Power consumption: 0.6 W @ sx-mt-5 Mass: 350 g @ sx-mt-5 Envelope (L×W×H): 220x50x35 mm @ sx-mt-5 Magnetic dipole moment: 10 A·m² @ sx-mt-10 Power consumption: 0.7 W @ sx-mt-10 Mass: 550 g @ sx-mt-10 Envelope (L×W×H): 320x50x35 mm @ sx-mt-10 Magnetic dipole moment: 15 A·m² @ sx-mt-15 Power consumption: 0.8 W @ sx-mt-15 Mass: 650 g @ sx-mt-15 Envelope (L×W×H): 400x50x35 mm @ sx-mt-15 Magnetic dipole moment: 20 A·m² @ sx-mt-20 Power consumption: 1 W @ sx-mt-20 Mass: 800 g @ sx-mt-20 Envelope (L×W×H): 470x50x35 mm @ sx-mt-20 Magnetic dipole moment: 25 A·m² @ sx-mt-25 Power consumption: 1.2 W @ sx-mt-25 Mass: 1000 g @ sx-mt-25 Envelope (L×W×H): 470x50x35 mm @ sx-mt-25 Magnetic dipole moment: 30 A·m² @ sx-mt-30 Power consumption: 1.8 W @ sx-mt-30 Mass: 1200 g @ sx-mt-30 Envelope (L×W×H): 440x50x40 mm @ sx-mt-30 Supply voltage: 10 (nominal) ## MT-P4 — Space Inventor ApS [magnetorquers] https://newspacemarket.com/products/magnetorquer-mt-p4/ Magnetic dipole moment: 2 A·m² (nominal) Supply voltage: 28 (nominal) ## NCTR-M002 Magnetorquer Rod — NewSpace Systems (NSS) [magnetorquers] https://newspacemarket.com/products/nctr-m002-magnetorquer-rod/ Supply voltage: 5 (nominal) ## CubeSat OBC / ADCS Motherboard SXC-MB-04-ADC — SPUTNIX [obc-computers] https://newspacemarket.com/products/sputnix-sxc-mb-04-adc-obc/ Processor: Raspberry Pi CM3/CM3+ Data interface: CAN Data interface: SPI @ (variant 2) Data interface: I2C @ (variant 3) Data interface: UART @ (variant 4) Data interface: USB @ (variant 5) Data interface: Ethernet @ (variant 6) ## SX-SBOX Onboard Computing (Microsatellite) — SPUTNIX [obc-computers] https://newspacemarket.com/products/sputnix-sx-sbox-onboard-computing/ Envelope (L×W×H): 171 × 111 × 51 mm Mass: 860 g Power consumption: 10 W (max) Data interface: CAN Data interface: SpaceWire @ (variant 2) Data interface: MIL-STD-1553 @ (variant 3) Supply voltage: 22 (min) Supply voltage: 34 (max) ## SE-1 Space Edge Computer — Spiral Blue [obc-computers] https://newspacemarket.com/products/spiralblue-se1/ Processor: NVIDIA Jetson Xavier NX Flight heritage: flight-proven ## OBCU-500-NS — Airbus Defence and Space [obc-computers] https://newspacemarket.com/products/airbus-pureline-amethyst-obc/ Design lifetime: 10 years @ LEO rating ## LX2160A Radiation-Tolerant Network-on-Chip Processor for Space — Teledyne e2v [obc-computers] https://newspacemarket.com/products/e2v-lx2160a-radiation-tolerant-noc-processor/ Processor: 16 ARM Cortex-A72 cores Processor: NXP QorIQ LX2160A SoC @ (variant 2) CPU clock: 2000000 MHz (max) Data interface: 100G Ethernet Data interface: PCIe Gen3 @ (variant 2) Data interface: USB @ (variant 3) Data interface: UART @ (variant 4) ## Aurora 1000 Satellite-Borne Intelligent Computer — Zhongke Tiansuan (Comospace) [obc-computers] https://newspacemarket.com/products/comospace-aurora-1000/ Flight heritage: 1,000+ cumulative days (multiple satellites) ## ORC3990 — Space-Grade Processing SoC for Satellite Avionics — Totum Labs [obc-computers] https://newspacemarket.com/products/totum-labs-orc3990-space-grade-soc/ Data interface: SpaceWire Data interface: CAN @ (variant 2) Data interface: UART @ (variant 3) Data interface: SPI @ (variant 4) Data interface: I2C @ (variant 5) ## RTM60S 6U OpenVPX I/O Rear Transition and Carrier Module — Mercury Systems [obc-computers] https://newspacemarket.com/products/rtm60s-6u-openvpx-i-o-rear-transition-and-carrier-module/ Data interface: 10/100/1000BASE-T Ethernet Data interface: 10/100BASE-T Ethernet @ (variant 2) ## Beam Pointing Systems (CPA / FPA) — General Atomics Synopta GmbH [pointing-mechanisms] https://newspacemarket.com/products/synopta-beam-pointing-systems/ Travel range: 2.5 @ mechanical ## Bipropellant Low Thrust Rocket Engine — Glavkosmos [propulsion] https://newspacemarket.com/products/bipropellant-low-thrust-rocket-engine/ Propulsion type: chemical ## RUDRA Hall Effect Thruster — Bellatrix Aerospace [propulsion] https://newspacemarket.com/products/rudra-hall-effect-thruster/ Propulsion type: electric Propellant: xenon ## AURORA-1 Aerospike Engine — Pangea Aerospace [propulsion] https://newspacemarket.com/products/aurora-1-aerospike-engine/ Propulsion type: chemical Propellant: liquid-fuelled ## ExoMG Hall Effect Thruster — Exotrail [propulsion] https://newspacemarket.com/products/exomg-hall-effect-thruster/ Thrust: 1 mN (min) Thrust: 20 mN (max) Specific impulse: 1000 (min) Specific impulse: 2000 (max) Propellant: xenon ## HPGP High Performance Green Propellant Thruster — Bradford Space [propulsion] https://newspacemarket.com/products/hpgp-high-performance-green-propellant-thruster/ Propulsion type: chemical Specific impulse: 260 @ up to Propellant: LMP-103S Flight heritage: PRISMA satellite, NASA's GPIM demonstrator, Planet Labs Doves, and multiple commercial and government satellites ## NPT30-I2 Iodine Ion Thruster for CubeSats and SmallSats — ThrustMe [propulsion] https://newspacemarket.com/products/npt30-i2-iodine-ion-thruster-for-cubesats-and-smallsats/ Propulsion type: electric Thrust: 0.9 mN @ at 75 W input power Specific impulse: 1550 Propellant: iodine Power at thrust: 75 W Flight heritage: demonstrated aboard CubeSat 1UC-PW1 in November 2021 Design lifetime: 5 years @ deorbit regulations ## HPGP 200N Thruster — High-Performance Green Propellant Propulsion — Bradford Space [propulsion] https://newspacemarket.com/products/hpgp-200n-thruster-high-performance-green-propellant-propulsion/ Propulsion type: chemical Thrust: 200000 mN Specific impulse: 254 Propellant: LMP-103S Flight heritage: LRO (Lunar Reconnaissance Orbiter) successor studies, ESA's MYRIADE and LAPAN-A2 satellites, and NASA's Lunar Flashlight (2022) ## M-10 / DM-1650 Solid Rocket Booster Motors for Ariane 5 and Ariane 6 — Nammo [propulsion] https://newspacemarket.com/products/m-10-dm-1650-solid-rocket-booster-motors-for-ariane-5-and-ariane-6/ Propulsion type: solid Propellant: solid rocket motor ## KRE-075 Rocket Engine — Nuri/KSLV-II First Stage Propulsion by Hanwha — Hanwha Aerospace [propulsion] https://newspacemarket.com/products/kre-075-rocket-engine-nuri-kslv-ii-first-stage-propulsion-by-hanwha/ Propulsion type: chemical Specific impulse: 298 @ at sea level Specific impulse: 315 @ in vacuum Propellant: liquid oxygen (LOX) and kerosene (RP-1) ## AEPS Advanced Electric Propulsion System — Hall-Effect Ion Thruster for NASA Gateway — Lanzo Batteries [propulsion] https://newspacemarket.com/products/aeps-advanced-electric-propulsion-system-hall-effect-ion-thruster-for-nasa-gateway/ Propulsion type: electric Thrust: 500 mN @ min Thrust: 600 mN @ max Propellant: xenon Specific impulse: 3000 Power at thrust: 13000 W ## Highly concentrated, pure hydrogen peroxide — Thaliana Space [propulsion] https://newspacemarket.com/products/thaliana-space-htp-catalyst-systems/ Propellant: hydrogen peroxide ## Kreios Space VLEO Propulsion System — Kreios Space [propulsion] https://newspacemarket.com/products/kreios-vleo-satellite-platform/ Propulsion type: electric @ runs only on ambient air and solar power Propellant: ambient air ## AF-M315E (ASCENT) Green Monopropellant — Digital Solid State Propulsion [propulsion] https://newspacemarket.com/products/dssp-af-m315e-ascent/ Propellant: hydroxylammonium nitrate (HAN) ## AF-M315E (ASCENT) — Digital Solid State Propulsion [propulsion] https://newspacemarket.com/products/dssp-sierra-gem-monopropellant/ Propulsion type: chemical Propellant: AF-M315E ## AYAP Lunar Propulsion System — DELTAV Space Technologies [propulsion] https://newspacemarket.com/products/deltav-space-ayap-lunar/ Propulsion type: hybrid ## M-10 and M-100 Solid Rocket Motors — Nammo [propulsion] https://newspacemarket.com/products/nammo-solid-rocket-motors/ Propulsion type: solid Propulsion type: solid @ (variant 2) Flight heritage: sounding rockets ## XR-5 Hall Thruster System — Aerojet Rocketdyne (L3Harris) [propulsion] https://newspacemarket.com/products/aerojet-xr-5-hall-thruster-system/ Propulsion type: electric Flight heritage: Flight proven, in service, on AEHF constellation, Northrop Grumman GEOStar-3 and Mission Extension Vehicles, Lockheed Martin LM2100 ## Hall Thruster Systems — aliena [propulsion] https://newspacemarket.com/products/hall-thruster-systems/ Propulsion type: electric Supply voltage: 25-36 @ Spacecraft bus input Supply voltage: 25-36 @ TCU input Data interface: CAN @ TCU comms Data interface: RS-422 @ TCU comms (TBD) ## TacSat-2 — Busek Co. [propulsion] https://newspacemarket.com/products/tacsat-2/ Propulsion type: electric Power at thrust: 200 W @ primary propulsion system Flight heritage: TacSat-2 satellite ## 1-20N Monopropellant System — OHB Sweden AB [propulsion] https://newspacemarket.com/products/1-20n-monopropellant-system/ Propulsion type: chemical Propellant: hydrazine ## Cold Gas System — OHB Sweden AB [propulsion] https://newspacemarket.com/products/cold-gas-system/ Propulsion type: cold-gas ## Electric Propulsion System — OHB Sweden AB [propulsion] https://newspacemarket.com/products/electric-propulsion-system/ Propulsion type: electric Flight heritage: extensive flight heritage ## ASELSAN Satellite Communication Terminal — Aselsan (Space Division) [radios] https://newspacemarket.com/products/aselsan-satellite-communication-terminal/ Frequency band: Ku Frequency band: Ka @ (variant 2) Frequency band: X @ (variant 3) Frequency band: UHF @ (variant 4) ## SkyEdge II-c VSAT Platform — Satellite Broadband Terminal for Rural Connectivity — Gilat Satellite Networks [radios] https://newspacemarket.com/products/skyedge-ii-c-vsat-platform-satellite-broadband-terminal-for-rural-connectivity/ Frequency band: Ka @ RX Frequency band: Ku @ RX (variant 2) Frequency band: Ka @ TX Frequency band: Ku @ TX (variant 2) Data rate: 150000 kbps (max) @ per terminal Modulation: DVB-S2X/DVB-RCS2 ## TRX-U UHF Satellite Transceiver — AAC SpaceQuest (AAC Clyde Space subsidiary) [radios] https://newspacemarket.com/products/aac-spacequest-trx-u/ Frequency band: UHF @ TX + RX Flight heritage: extensive flight heritage from AAC SpaceQuest satellite missions ## Outdoor Frequency Converter (UPC-Ext) — TTI Norte [radios] https://newspacemarket.com/products/tti-norte-outdoor-frequency-converter/ Frequency band: Ku @ UPC-Ext, Ku band Frequency band: Ku @ UPC-Ext, DBS band Frequency: 950 MHz (min) @ UPC-Ext, Ku band Up-converter, Input (3) Frequency: 1450 MHz (max) @ UPC-Ext, Ku band Up-converter, Input (3) Frequency: 12750 MHz (min) @ UPC-Ext, Ku band Up-converter, Output (3) Frequency: 13250 MHz (max) @ UPC-Ext, Ku band Up-converter, Output (3) Frequency: 950 MHz (min) @ UPC-Ext, Ku band Up-converter, Input (4) Frequency: 1700 MHz (max) @ UPC-Ext, Ku band Up-converter, Input (4) Frequency: 13750 MHz (min) @ UPC-Ext, Ku band Up-converter, Output (4) Frequency: 14500 MHz (max) @ UPC-Ext, Ku band Up-converter, Output (4) Frequency: 950 MHz (min) @ UPC-Ext, Ku band Up-converter, Input (5) Frequency: 1700 MHz (max) @ UPC-Ext, Ku band Up-converter, Input (5) Frequency: 12750 MHz (min) @ UPC-Ext, Ku band Up-converter, Output (5) Frequency: 14500 MHz (max) @ UPC-Ext, Ku band Up-converter, Output (5) Frequency: 950 MHz (min) @ UPC-Ext, DBS band Up-converter, Input (2) Frequency: 2050 MHz (max) @ UPC-Ext, DBS band Up-converter, Input (2) Frequency: 17300 MHz (min) @ UPC-Ext, DBS band Up-converter, Output (2) Frequency: 18400 MHz (max) @ UPC-Ext, DBS band Up-converter, Output (2) ## CENTAURI 25G — Transcelestial [radios] https://newspacemarket.com/products/transcelestial-centauri-25g/ Data rate: 25000 kbps @ full-duplex ## EWC31-NG S/S-Band Transponder — Syrlinks [radios] https://newspacemarket.com/products/syrlinks-ewc31-ng-sband-transponder/ Frequency band: S @ TX and RX ## Scotty LEO User Terminal — Skyloom Global Corp. [radios] https://newspacemarket.com/products/skyloom-scotty-leo-terminal/ Data rate: 20000000 kbps @ LEO-GEO links ## Satellite RF Communication Payload Equipment — Antwerp Space [radios] https://newspacemarket.com/products/antwerp-space-rf-payload/ Frequency band: S @ TT&C transponders Frequency band: X @ data transmitters Frequency band: Ka @ channelizers ## Iridium Certus Maritime Terminals (C200M, C700, C700 Winterized) — Intellian Technologies [radios] https://newspacemarket.com/products/intellian-iridium-certus-maritime/ Data rate: 352 kbps @ C700 uplink Data rate: 704 kbps @ C700 downlink Data rate: 176 kbps @ C200m upload Data rate: 176 kbps @ C200m download Frequency band: L @ Network Data interface: Ethernet @ Power-over-Ethernet (PoE) Data interface: other @ Wi-Fi Flight heritage: C700 terminal used by the Monkey Fist Adventures team for transatlantic rowing ## Cormorant UHF/VHF Transceiver — Needronix [radios] https://newspacemarket.com/products/needronix-cormorant-uhf-vhf-transceiver/ Frequency band: UHF @ uplink Frequency band: VHF @ downlink ## STARCOM Optical Communications Terminal — Mbryonics [radios] https://newspacemarket.com/products/mbryonics-starcom-optical-terminal/ Data rate: 400000 kbps @ targeted by 2027 ## Kacific CommsBox — Kacific Broadband Satellites [radios] https://newspacemarket.com/products/kacific-commsbox-vsat-terminal/ Data rate: 6000 kbps @ download burst Data rate: 2400 kbps @ download standard Data rate: 700 kbps @ upload Frequency band: Ka @ satellite ## Kacific CommsBox Ultra — Kacific Broadband Satellites [radios] https://newspacemarket.com/products/kacific-commsbox-ultra-vsat/ Data rate: 30000 kbps @ download Data rate: 10000 kbps @ upload ## S-Band TM/TC Transceiver — Azista Space (Azista Aerospace) [radios] https://newspacemarket.com/products/azista-sband-tmtc-transceiver/ Frequency band: S ## X-Band TM Transmitter — Azista Space (Azista Aerospace) [radios] https://newspacemarket.com/products/azista-xband-tm-transmitter/ Frequency band: X @ TX Frequency: X-band frequency range ## LinkStar Radio System — sci_Zone / QuickSAT [radios] https://newspacemarket.com/products/scizone-quicksat-vms/ Power consumption: 0.35 W @ min operation ## Syrlinks EWC36 L-band transmitter — Syrlinks [radios] https://newspacemarket.com/products/syrlinks-ewc36-l-band-transmitter/ Frequency band: L @ TX Frequency: 1698 MHz (min) @ TX Frequency: 1710 MHz (max) @ TX Design lifetime: 7.5 years ## T-XPDR Tactical Adaptive Satellite Transponder — Thorium Space Technology [radios] https://newspacemarket.com/products/thorium-t-xpdr-tactical-transponder/ Frequency band: Ka @ TX and RX ## QR026 High Performance Wideband Receiver — Teledyne Defence & Space [radios] https://newspacemarket.com/products/teledyne-qr026-high-performance-receiver/ Frequency: 500-18000 MHz Frequency: 500-40000 MHz @ optional extensions ## QR035 Multi-Channel High Performance Receiver — Teledyne Defence & Space [radios] https://newspacemarket.com/products/teledyne-qr035-multi-channel-receiver/ Frequency: 500000-18000 MHz Frequency: 40000 MHz @ optional extension ## NRWA Reaction Wheels — NewSpace Systems (NSS) [reaction-wheels] https://newspacemarket.com/products/nss-nrwa-reaction-wheels/ Data interface: digital spacecraft bus @ simple Flight heritage: First flight: 2014 Flight heritage: Units sold: > 800 @ (variant 2) Flight heritage: Failure-free hours (T065): > 3,000,000 @ (variant 3) ## Reaction Wheels — Blue Canyon Technologies [reaction-wheels] https://newspacemarket.com/products/reaction-wheels-2/ Angular momentum storage: 0.015 N·m·s @ minimum Angular momentum storage: 16 N·m·s @ maximum Flight heritage: 3,300 wheels manufactured and hundreds on-orbit ## Solar Array Drive Assembly (SADA) — MMA Design [sadm] https://newspacemarket.com/products/mma-solar-array-drive-assembly/ Wheel speed: 2.2 (max) Slip-ring channels: 16 (max) ## SADM — Comat [sadm] https://newspacemarket.com/products/sadm/ Power transfer: 400 W @ per wing Max torque: 350 mN·m @ Maximum Design lifetime: 5 years @ minimum in LEO ## X-band SDR — EnduroSat [sdr-modems] https://newspacemarket.com/products/endurosat-x-band-sdr/ Frequency: 2200 MHz (min) @ Tx (commercial) Frequency: 2290 MHz (max) @ Tx (commercial) ## TREVO — Modular High-Performance SDR — Alén Space [sdr-modems] https://newspacemarket.com/products/alen-trevo-sdr/ Flight heritage: Flight Heritage ## NSR-SDR-X/S — Vulcan Wireless [sdr-modems] https://newspacemarket.com/products/vulcan-nsr-sdr-x-s/ Frequency: X-band Data rate: low Mbps to >500 Mbps @ Downlink Data rate: low Mbps to >500 Mbps @ Uplink TX power: 5 W @ SSPA Modulation: DVB-S2, variable modulation and coding Protocols / waveforms: DVB-S2 Protocols / waveforms: CCSDS @ (variant 2) ## NSR-SDR-K/Ka-HDR-DVB — Vulcan Wireless [sdr-modems] https://newspacemarket.com/products/vulcan-nsr-sdr-k-ka-hdr-dvb/ Frequency: 20000 MHz (min) @ Transmitter Frequency: 21200 MHz (max) @ Transmitter Frequency: 30000 MHz (min) @ Receiver Frequency: 31000 MHz (max) @ Receiver Data rate: 500000 kbps (max) @ Downlink speed Data rate: 500000 kbps (max) @ Uplink speed TX power: 5 W (typical) Modulation: DVB-S2 Uplink/Downlink with Variable Modulation and Coding Protocols / waveforms: DVB-S2 Uplink/Downlink ## DMSS 3990 Endpoint SoC — Totum Labs [sdr-modems] https://newspacemarket.com/products/totum-labs-dmss-3990-endpoint-soc/ Frequency: 2400 MHz RX sensitivity: -143 @ Effective ## UHF COMM 4G0 Half Duplex Modem — NanoAvionics [sdr-modems] https://newspacemarket.com/products/nanoavionics-uhf-comm-4g0-modem/ Frequency: 401-403 MHz @ commercial Frequency: 430-440 MHz @ amateur RX sensitivity: -122 @ 2400 bps GFSK2 RX sensitivity: -119 @ 9600 bps GFSK2 Data interface: CAN @ server interface Connector: RCA @ Pa enable output Connector: SMA @ Sdr monitoring output, optional ## SL100x Universal Demodulator — Saankhya Labs [sdr-modems] https://newspacemarket.com/products/saankhya-labs-sl-100x-universal-demodulator/ Supply voltage: 3.3 Supply voltage: 2.5 @ (variant 2) Supply voltage: 1.2 @ (variant 3) ## SL900x Universal Modulator — Saankhya Labs [sdr-modems] https://newspacemarket.com/products/saankhya-labs-sl-900x-universal-modulator/ Modulation: QPSK @ single carrier Modulation: 16/32/64/128/256 QAM @ single carrier (variant 2) Modulation: QPSK @ multicarrier (OFDM) Modulation: 16/32/64/128/256 QAM @ multicarrier (OFDM) (variant 2) Protocols / waveforms: ATSC, DVB-T, ISDB-T, Clear QAM, DVB-C, ISDB-C Envelope (L×W×H): 12×12 mm Supply voltage: 3.3 Supply voltage: 2.5 @ (variant 2) Supply voltage: 1.2 @ (variant 3) Data interface: I2C @ for programming and waveform download Data interface: JTAG @ for diagnostics and debug Data interface: UART @ for diagnostics and debug (variant 2) ## TARANG L-Band Multi-Channel Burst Demodulator — Saankhya Labs [sdr-modems] https://newspacemarket.com/products/saankhya-labs-tarang-l-band-multichannel-burst-demodulator/ Frequency: 950 MHz (min) Frequency: 2150 MHz (max) RX sensitivity: -70 (min) RX sensitivity: -45 (max) Data rate: 1.2 kbps @ selectable Data rate: 2.4 kbps @ selectable (variant 2) Data rate: 2.7 kbps @ selectable (variant 3) Data rate: 4.8 kbps @ selectable (variant 4) Data interface: Ethernet @ control and data interfaces ## GENUS DIGITAL Module – RF over IP — ETL Systems [sdr-modems] https://newspacemarket.com/products/genus-digital-module-rf-over-ip/ Frequency: 850-2450 MHz TX power: 0.002 W RX sensitivity: -60 Data interface: Ethernet @ Digital Interface Data Protocols / waveforms: DIFI, IEEE-ISTO 4900-2001 protocol @ Digital Interface Data Data interface: Ethernet @ Digital Interface Control ## V-Series Software Modem — WORK Microwave [sdr-modems] https://newspacemarket.com/products/v-series-software-modem/ Protocols / waveforms: DVB-S2/S2X, CCSDS, ECSS standards, DIFI standard Modulation: CCM, VCM and ACM ## Modular Deployment Sequencer — ISISPACE Group [separation-systems] https://newspacemarket.com/products/isispace-modular-deployment-sequencer/ Mass: 1000 g (max) @ 4 deployers, external power Mass: 2000 g (max) @ 8 deployers, internal power Envelope (L×W×H): 250 x 100 mm base area Supply voltage: 28 (nominal) Supply voltage: 4 Release time: 100 ms (min) Release time: 2000 ms (max) Data interface: RS-485 Data interface: RS-422 @ (variant 2) Data interface: UART @ (variant 3) Data interface: CAN @ (variant 4) Data interface: Ethernet @ (variant 5) Data interface: other @ (variant 6) ## Satellite Payload Release & Sequencing System (PRSS) — PacSci EMC [separation-systems] https://newspacemarket.com/products/pacsci-emc-satellite-payload-release-sequencing/ Release time: 1 ms @ Timing and simultaneity Data interface: RS-422 Flight heritage: successful deployment of 34 satellites into Low Earth Orbit (LEO) on March 21, 2020, and has successfully sequenced 4,000 on-orbit events to deploy 500 satellites to date ## TiNi Pin Puller P5 — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/ebad-p5/ Preload / holding force: 0.022 kN Mass: 18 g Release time: 130 ms (max) Operating temperature: -65-70 °C Flight heritage: Mars Global Surveyor mission (since 1996) ## TiNi Pin Puller P10 — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/ebad-p10/ Preload / holding force: 0.044 kN Mass: 30 g Release time: 100 ms Cycles / reuses: 50 @ minimum Operating temperature: -65 °C (min) Operating temperature: 70 °C (max) Flight heritage: extensive heritage in space applications since the 1996 Mars Global Surveyor mission ## TiNi Pin Puller P25 — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/ebad-p25/ Preload / holding force: 0.111 kN @ pull force Release time: 130 ms (max) Mass: 48 g Operating temperature: -65 °C (min) Operating temperature: 70 °C (max) Flight heritage: Mars Global Surveyor mission ## TiNi Pin Puller P50 — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/ebad-p50/ Preload / holding force: 0.222 kN Mass: 75 g Release time: 100 ms (max) @ @ 4 A Cycles / reuses: 50 Operating temperature: -60 °C (min) Operating temperature: 70 °C (max) Flight heritage: Mars Global Surveyor mission since 1996 ## TiNi Pin Puller P100 — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/ebad-p100/ Preload / holding force: 0.445 kN @ pull force Release time: 100 ms (max) Cycles / reuses: 50 @ minimum Mass: 150 g Operating temperature: -60-70 °C Flight heritage: Mars Global Surveyor mission ## TiNi Pin Puller P1000 — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/ebad-p1000/ Preload / holding force: 4.45 kN @ pull force Mass: 360 g Release time: 75 ms (max) Operating temperature: -60 °C (min) Operating temperature: 70 °C (max) Flight heritage: Mars Global Surveyor mission since 1996 ## TiNi™ Pin Puller P10 — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/tini-pin-puller-p10/ Mass: 30 g Release time: 100 ms (max) Cycles / reuses: 100 @ min Operating temperature: -65 °C (min) Operating temperature: 70 °C (max) Flight heritage: flight pedigree ## TiNi™ Pin Puller P25 — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/tini-pin-puller-p25/ Preload / holding force: 0.111 kN @ pull force Release time: 130 ms (max) Mass: 48 g Operating temperature: -65 °C (min) Operating temperature: 70 °C (max) Flight heritage: flight pedigree ## TiNi™ Pin Puller P50 — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/tini-pin-puller-p50/ Mass: 75 g Release time: 100 ms (max) Operating temperature: -60 °C (min) Operating temperature: 70 °C (max) Flight heritage: flight pedigree ## TiNi™ Pin Puller P100 — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/tini-pin-puller-p100/ Preload / holding force: 0.445 kN (nominal) @ pull force Release time: 100 ms (max) Mass: 150 g (nominal) Operating temperature: -60 °C (min) Operating temperature: 70 °C (max) Flight heritage: flight pedigree ## TiNi™ Pin Puller P1000 — Ensign-Bickford Aerospace & Defense (EBAD) [separation-systems] https://newspacemarket.com/products/tini-pin-puller-p1000/ Preload / holding force: 4.45 kN @ pull force Mass: 482 g Release time: 75 ms (max) Cycles / reuses: 50 @ min Operating temperature: -60 °C (min) Operating temperature: 70 °C (max) Flight heritage: flight pedigree ## Maverick 4-Point Lightweight Separation System (M4P-L) — Maverick Space Systems [separation-systems] https://newspacemarket.com/products/maverick-m4p-l-separation-system/ Flight heritage: flight-proven heritage ## Mercury-6T Tab-Based 6U CubeSat Dispenser — Maverick Space Systems [separation-systems] https://newspacemarket.com/products/maverick-mercury-6t-dispenser/ Flight heritage: Flight-proven heritage ## Mercury-12T Tab-Based 12U CubeSat Dispenser — Maverick Space Systems [separation-systems] https://newspacemarket.com/products/maverick-mercury-12t-dispenser/ Flight heritage: Flight-proven heritage ## ROSA Roll-Out Solar Array — Redwire Corporation [solar-panels] https://newspacemarket.com/products/rosa-roll-out-solar-array/ Flight heritage: International Space Station in June 2017 (ISS Expedition 52) ## CubeSat Kit Fixed Solar Panel: End Panel — Pumpkin, Inc. [solar-panels] https://newspacemarket.com/products/pumpkin-cubesat-kit-fixed-solar-panel-end-panel/ Cell efficiency: 28 (min) Cell efficiency: 32 (max) Form factor: End panel Deployable: no Flight heritage: Over 600 PMDSAS panels flown since 2008 with 100% on-orbit success rate, LEO through GTO ## EXA DMSA – Deployable Multifunction Solar Array — EXA (Ecuadorian Space Agency) [solar-panels] https://newspacemarket.com/products/exa-dmsa-deployable-multifunction-solar-array/ Form factor: CubeSat in the range of 1U to 6U Deployable: yes, multiple wings (folds into a panel, deploys to full extension) ## Flexible Blanket Solar Array — Dcubed [solar-panels] https://newspacemarket.com/products/flexible-blanket-solar-array/ Form factor: deployed wing ## CubeSat GaAs Solar Panel — NanoAvionics [solar-panels] https://newspacemarket.com/products/nanoavionics-cubesat-gaas-solar-panels/ Cell efficiency: 29.5 ## Body-Mounted Solar Array — Dcubed [solar-panels] https://newspacemarket.com/products/dcubed-body-mounted-solar-array/ Output power (BOL): 400 W (max) Cell efficiency: 28 (min) Form factor: 1U–6U side Deployable: no Design lifetime: 3 years (min) Design lifetime: 5 years (max) ## 24U CubeSat Solar Array (Very High Power) — MMA Design [solar-panels] https://newspacemarket.com/products/mma-24u-cubesat-solar-array/ Output power (BOL): 330 W @ single deployed wing Form factor: 24U CubeSat Deployable: single deployed wing Flight heritage: Largest deployable CubeSat solar array flown (per MMA) ## DragonSCALES Silicon Solar Cell Technology — mPower Technology [solar-panels] https://newspacemarket.com/products/mpower-dragonscales-solar-cells/ Design lifetime: 15 years (min) @ with annealing/recovery Design lifetime: 20 years (max) @ with annealing/recovery ## GaInP/GaAs/Ge Lattice Matched 3J Solar Cells — Spectrolab [solar-panels] https://newspacemarket.com/products/spectrolab-xtj-prime-solar-cell/ Cell efficiency: 32 (max) ## Satellite Solar Panels and Power Systems — Azista Industries [solar-panels] https://newspacemarket.com/products/azista-space-solar-panels/ Cell efficiency: 28 (min) @ triple-junction GaAs Cell efficiency: 30 (max) @ triple-junction GaAs ## MAI-SS Space Sextant — Adcole Space (Redwire) [star-trackers] https://newspacemarket.com/products/mai-ss-space-sextant/ Attitude accuracy (cross-boresight): 46.8 @ cross-boresight ## Nano Star Tracker (NST) — Blue Canyon Technologies [star-trackers] https://newspacemarket.com/products/bct-nst-nano-star-tracker/ Limiting star magnitude: 7.5 ## CubeSat Kit™ Base Plate Assembly — Pumpkin, Inc. [structures] https://newspacemarket.com/products/pumpkin-base-plate-assembly/ Material: Al 5052-H32, plated per CubeSat Design Specification (CDS) Flight heritage: Flight Qualified and Space Proven ## CubeSat Kit™ Payload Adapter Plate — Pumpkin, Inc. [structures] https://newspacemarket.com/products/pumpkin-payload-adapter-plate/ Material: Al 5052-H32, plated per CubeSat Design Specification (CDS) Flight heritage: Flight Qualified and Space Proven ## CubeSat Kit™ Payload Cover Plate Assembly — Pumpkin, Inc. [structures] https://newspacemarket.com/products/pumpkin-payload-cover-plate-assembly/ Material: Al 5052-H32, plated per CubeSat Design Specification (CDS) Flight heritage: Flight Qualified and Space Proven ## CubeSat Kit™ Large Aperture Cover Plate Assembly — Pumpkin, Inc. [structures] https://newspacemarket.com/products/pumpkin-large-aperture-cover-plate-assembly/ Material: Al 5052-H32, plated per CubeSat Design Specification (CDS) ## CubeSat Kit™ Base Plate Assembly for AntS Antenna — Pumpkin, Inc. [structures] https://newspacemarket.com/products/pumpkin-base-plate-assembly-ants-antenna/ Material: Al 5052-H32, plated per CubeSat Design Specification (CDS) Flight heritage: Flight Qualified and Space Proven ## 16-Unit cubesat structure — ISISPACE Group [structures] https://newspacemarket.com/products/16-unit-cubesat-structure/ Form factor: 16 ## CubeSat Structural Frame — NanoAvionics [structures] https://newspacemarket.com/products/nanoavionics-cubesat-structural-frame/ Material: 7075-T7351 aluminum alloy Material: Hard-anodized black or natural @ (variant 2) Form factor: 6 Form factor: 8 @ (variant 2) Form factor: 12 @ (variant 3) Form factor: 16 @ (variant 4) ## SM02 — NPC Spacemind [structures] https://newspacemarket.com/products/npc-spacemind-sm02-2u-structure/ Form factor: 2 Envelope (L×W×H): 227.0 x 100.0 x 100.0 mm ## SM03 — NPC Spacemind [structures] https://newspacemarket.com/products/npc-spacemind-sm03-3u-structure/ Form factor: 3 (nominal) Envelope (L×W×H): 340.5 x 100.0 x 100.0 mm ## SM04 — NPC Spacemind [structures] https://newspacemarket.com/products/npc-spacemind-sm04-4u-structure/ Form factor: 4 Envelope (L×W×H): 454 x 100.0 x 100.0 mm ## SM06 — NPC Spacemind [structures] https://newspacemarket.com/products/npc-spacemind-sm06-6u-structure/ Form factor: 6 Envelope (L×W×H): 340.5 x 226.3 x 100.0 mm ## SM08 — NPC Spacemind [structures] https://newspacemarket.com/products/npc-spacemind-sm08-8u-structure/ Form factor: 8 Envelope (L×W×H): 454.0 x 226.3 x 100.0 mm @ without KS ## SM12 — NPC Spacemind [structures] https://newspacemarket.com/products/npc-spacemind-sm12-12u-structure/ Form factor: 12 Envelope (L×W×H): 340.5 x 226.3 x 226.3 mm ## PEEK CubeSat Structures — Lamb Space Tec [structures] https://newspacemarket.com/products/lambspace-fg-one-sma-actuator/ Material: PEEK ## V-BUS Modular CubeSat Platform — Serenum Space [structures] https://newspacemarket.com/products/serenum-vbus-platform/ Lead time: 6 ## KSCS CubeSat Structure — Kairo Space [structures] https://newspacemarket.com/products/kairo-space-kscs-structure/ Material: Aerospace-grade aluminum alloy ## NSS CubeSat Sun Sensor — NewSpace Systems (NSS) [sun-sensors] https://newspacemarket.com/products/nss-cubesat-sun-sensor/ Field of view: 57 @ half-angle Accuracy: 0.5 ° @ RMS ## Coarse Sun Sensor (CSS) — Bradford Space [sun-sensors] https://newspacemarket.com/products/bradford-css-coarse-sun-sensor/ Field of view: 180 @ hemispherical Flight heritage: LEO, MEO, HEO, GEO, planetary and interplanetary orbits ## SX-SBOX Thermal Control (Microsatellite) — SPUTNIX [thermal] https://newspacemarket.com/products/sputnix-sx-sbox-thermal-control/ Envelope (L×W×H): 200 × 130 × 30 mm Mass: 600 g Power consumption: 5 W (max) @ heaters off Supply voltage: 22 (min) Supply voltage: 33 (max) Data interface: CAN ## Space Copper-Water Heat Pipes (SCWHPs) — ACT (Advanced Cooling Technologies) [thermal] https://newspacemarket.com/products/act-scwhp/ Flight heritage: 2017, ISS (APTx experiment) ## Variable Conductance Heat Pipes (VCHPs) — ACT (Advanced Cooling Technologies) [thermal] https://newspacemarket.com/products/act-vchp/ Flight heritage: NASA planetary lander programs including Peregrine and VIPER ## Custom Cold Plates — Thermal Space Ltd. [thermal] https://newspacemarket.com/products/thermal-space-custom-cold-plates/ Data interface: USB Data interface: Ethernet @ (variant 2) Data interface: other @ Serial ## Acusil® Thermal Protection System (TPS) — Peraton Space [thermal] https://newspacemarket.com/products/acusil-thermal-protection-system-tps-4204/ Design lifetime: 30 years @ durability Flight heritage: NASA’s 2012 Mars Science Laboratory (Curiosity Rover), the Mars 2020 Lander (Perseverance Rover), SpaceX’s Dragon I Capsule, NASA’s Pegasus Booster, Patriot Advanced Capability (PAC) 3 Interceptor Missile, Evolved Sea Sparrow Missile (ESSM) ## SmartHeat™ SLT Thin-Film Heaters — Minco Products, Inc [thermal] https://newspacemarket.com/products/smartheat-slt-thin-film-heaters/ Operating temperature: -45 °C (min) Operating temperature: 100 °C (max) ## Cryogenic Multilayer Superinsulation — Aerospace Fabrication and Materials, LLC [thermal] https://newspacemarket.com/products/cryogenic-multilayer-superinsulation/ Operating temperature: -100 °C (min) @ below ## Multilayer Insulation Blankets — Aerospace Fabrication and Materials, LLC [thermal] https://newspacemarket.com/products/multilayer-insulation-blankets/ Operating temperature: -250 °C (min) Operating temperature: 1300 °C (max) ## High Temperature Plume Shields — Aerospace Fabrication and Materials, LLC [thermal] https://newspacemarket.com/products/high-temperature-plume-shields/ Operating temperature: 26.9-726.9 °C @ and above