Other Products — Space Hardware Marketplace

Bradford Standard Accuracy Pressure Transducer

• ModelStandard
• Max Pressure Range1–310 bar
• Accuracy (BoL)±0.3% FS

Space-qualified pressure transducer, 1–310 bar range, ±0.3% FS BoL accuracy, 250 g, compatible with hydrazine, MON, MMH and…

Bradford Miniaturised Pressure Transducer

• ModelMiniaturised
• Max Pressure Range3–320 bar
• Accuracy (BoL)±0.3% FS

Ultra-compact 180 g space-qualified pressure transducer, 3–320 bar range, ±0.3% FS accuracy, for small spacecraft propulsion systems.

MAG28 Analogue Magnetometer

• Dynamic Field Range±70,000 nT
• Noise≤40 nT (2σ)
• Offset≤500 nT

Fully qualified 3-axis AMR analogue magnetometer on +28 V supply with ±70,000 nT range and >1.4 Mh MTBF.…

MAG15 Analogue Magnetometer

• Dynamic Field Range±64,000 nT
• Noise≤3 nT/√Hz (3σ)
• Offset≤500 nT

Fully qualified 3-axis AMR analogue magnetometer with ±15 V supply and ±64,000 nT range for LEO attitude reference.…

DMAG Digital Magnetometer

• Dynamic Field Range±65,000 nT
• Noise≤20 nT (1σ)
• Offset≤500 nT

3-axis digital magnetometer with RS-485/422 interface and ±65,000 nT range for LEO attitude reference, ITAR/EAR-free and customizable to…

Redwire Star Field Simulator

Hardware-in-the-loop star field simulator providing as-you-fly ground test operation of Redwire star trackers.

Redwire CubeStack Payload Adapter

• ConfigurationESPA-class ring adapter
• CapacityUp to 8 3U CubeSat dispensers
• Product familyRedwire Payload Adapters (with XPOD, LoFF, CubeCone)

ESPA-class ring adapter from Redwire's payload-adapter line that can hold up to eight 3U CubeSat dispensers.

Redwire CubeCone Payload Adapter

• ConfigurationTransitional ring adapter
• FunctionCan also accommodate secondary payloads
• Product familyRedwire Payload Adapters (with XPOD, LoFF, CubeStack)

Transitional conical ring adapter from Redwire's payload-adapter line that can also accommodate secondary payloads.

Redwire XPOD CubeSat Deployer

• ConfigurationCustom adapter hosting 3 XPOD CubeSat dispensers
• Product familyRedwire Payload Adapters (with LoFF, CubeCone, CubeStack)
• Mission heritageORS-3, Spaceflight SSO-A, SpaceX Rideshare, Spaceflight GTO-1, SpaceIL Lunar Lander

Custom Redwire payload adapter configuration designed to host three XPOD CubeSat dispensers on a single rideshare interface.

IRES Infrared Earth Sensor

• Operating Band14-16.25 um (thermal IR)
• Earth Acquisition Range15,300-53,000 km
• Operational AltitudeUp to 140,000 km

Two-axis infrared Earth horizon sensor for GEO/MEO 3-axis spacecraft: 14-16.25 um band, <0.05 deg accuracy, 10Hz, <2.5kg, <4W,…

Mini-PHM Passive Hydrogen Maser

• Output Frequency10.00285741 MHz (fH/142)
• Output Level+7 dBm
• Frequency Drift/Day<=1e-14 (after 1 week); <1e-15 (after 30 days)

Miniaturized space passive hydrogen maser atomic clock: 12kg, <=54W, ADEV 6.5e-13 @ 1s, <1e-15/deg C thermal sensitivity, next-gen…

PHM Passive Hydrogen Maser

• Output Frequency10.00285741 MHz (fH/142)
• Output Level+7 dBm
• Frequency Drift/Day<=1e-14 (after 1 week); <1e-15 (after 30 days)

Space passive hydrogen maser — master clock of Galileo navigation system: 18.2kg, <=70W, ADEV 1.8e-12 @ 1s, 40+…

MASIMU02 Inertial Measurement Unit

• TechnologyMEMS gyroscopes and accelerometers
• Drift0.2 deg/min
• InterfaceRS-485 Serial

Improved MEMS-based IMU for small satellites: 20g bare board, 0.6W, RS-485, 0.2 deg/min drift — 5x better than…

MASIMU03 Inertial Measurement Unit

• Technology6-DOF MEMS with data fusion (multiple gyro + accelerometer)
• Drift<0.013 deg/min
• InterfaceRS-485 / RS-232

Advanced 6-DOF MEMS IMU with data fusion: <0.013 deg/min drift, 100g bare board, 1.3W, RS-485/232, integrates with sun/horizon…

MASIMU01 Inertial Measurement Unit

• TechnologyMEMS gyroscopes and accelerometers
• Drift1.0 deg/min
• InterfaceRS-485 Serial

Compact MEMS-based IMU for small satellite attitude detection: 40g (80g with enclosure), 0.6W, RS-485, 1.0 deg/min drift. Flight…

Antelope Advanced Data Processing Unit

• ProcessorAMD Zynq UltraScale+ MPSoC (ZU2/3/4/5 variants)
• CPU CoresQuad ARM Cortex-A53 @ up to 1.5 GHz + Dual Cortex-R5
• FPGAIncluded (programmable fabric)

PC-104 CubeSat data processing unit with AMD Zynq UltraScale+ MPSoC, 160 GOPS, 4-8GB DDR4 ECC, enabling onboard AI…

Satellite Pressurant Tanks

• FunctionHigh-pressure pressurant storage (He / N2)
• ApplicationPressure-feed for mono- and bipropellant systems
• Compatible systemsHydrazine, MMH/MON3, Hydrazine/NTO

IHI Aerospace flight-proven high-pressure pressurant tanks for satellite propulsion systems, providing regulated helium/nitrogen pressure feed for bipropellant and…

Satellite Propellant Tanks

• Tank TypesDiaphragm (propellant management device)
• Volume Range3 L to 552 L
• ConfigurationsSpherical and cylindrical

IHI Aerospace flight-proven diaphragm propellant tanks in 3L to 552L sizes for hydrazine and bipropellant systems, with titanium…