
27G RadNano-EB Evaluation Board
A complete evaluation setup containing a RadNano-EM model with additional circuitry and connectors, also serving as an add-on board for development projects.
| UART Protocol | 9600 8-N-1 |
| I2C Protocol | Standard |
NewSpace Market · Sector Catalogue
Every unit we list in this sector — specifications, manufacturers and where to ask for a quote. Compiled from the live NewSpace Market catalogue.
About this catalogue
This catalogue lists 243 test equipment & egse products offered by 80 manufacturers across 22 countries. Of those, 64 carry a manufacturer datasheet and 16 publish a price; the rest are quoted on request — normal in this market, where configuration drives cost.
Entries are grouped alphabetically by manufacturer. Every product links back to its page on newspacemarket.com, where you will find the full specification, the datasheet and a quote form that reaches the manufacturer directly.
Compiled 15 August 2026 from the live catalogue. Specifications are as published by the manufacturers; we normalise units but do not re-measure. Where a figure looked implausible it was left out rather than guessed.
Overview
| Product | Manufacturer | Country | Key specification | Price |
|---|---|---|---|---|
| “TERRA” complex of space environment simulators | Glavkosmos | Russia | Year of release: 2017 | on request |
| 1.5P VibePOD | Wyrm Engineering | Netherlands | Dimensions w/o plate: 98mm x 96mm x 117mm | on request |
| 12U MyPOD2 | Gran Systems | United States | Temperature range: -50°C to +100°C | on request |
| 1p/2p/3p Horizontal Integration Support Jig | Alba Orbital | United Kingdom | Length: 272 mm | on request |
| 1U CubeSat Vibration Shaker Test Jig | CubeSat Aerospace | India | Supported CubeSat Size: 1U (100 mm × 100 mm × 113.5 mm) | on request |
| 27G RadNano-EB Evaluation Board | 27G Technology | Hungary | UART Protocol: 9600 8-N-1 | on request |
| 2P VibePOD | Wyrm Engineering | Netherlands | Dimensions w/o plate: 147mm x 98mm x 96mm | on request |
| 3P Vibe POD | Wyrm Engineering | Netherlands | Dimensions w/o plate: 211mm x 98mm x 96mm | on request |
| 3U MyPOD1 | Gran Systems | United States | Temperature range: -50°C to +100°C | on request |
| 3U MyPOD2 | Gran Systems | United States | Temperature range: -50°C to +100°C | on request |
| 410-DHR Reflectometer | Surface Optics Corporation | United States | Measurement type: Integrated directional-hemispherical reflectance | on request |
| 5402 GTEM Test Cell | ETS-Lindgren | United States | Compliance standards: IEC 61000-4-20, ANSI C63.4 | on request |
| 5405 GTEM Test Cell | ETS-Lindgren | United States | Compliance standards: IEC 61000-4-20, ANSI C63.4 | on request |
| 5407 GTEM Test Cell | ETS-Lindgren | United States | Compliance standards: IEC 61000-4-20, ANSI C63.4 | on request |
| 5903-HST High Speed Reverberation Tuner | ETS-Lindgren | United States | Max continuous rotation speed: 100 RPM | on request |
| 5G NTN Network Emulator (NEMU) | Gatehouse Satcom | Denmark | — | on request |
| A Set of Stationary Control and Verification Equipment (SSCVE) | Glavkosmos | Russia | Year of release: 2017 | on request |
| AAA Engineering & Test Lab | AAA Engineering & Test Lab | United States | Testing standards: MIL-STD-202, MIL-STD-461, MIL-STD-750, MIL-STD-883, MIL-… | on request |
| Active Weightlessness System | Glavkosmos | Russia | Purpose: Ground modal testing under conditions simulating weightlessness an… | on request |
| Aerotable test bench for mutual movement of spacecraft | SPUTNIX | Russia | Overall dimensions: 5000x4000x3000 mm | on request |
| Air Bearing (15 kg) | Glavkosmos | Russia | Max carrying capacity, kg: 15 | on request |
| Air Bearing (160 kg) | Glavkosmos | Russia | Max carrying capacity, kg: 160 | on request |
| Air Bearing (35 kg) | Glavkosmos | Russia | Max carrying capacity, kg: 35 | on request |
| Air Bearing (65 kg) | Glavkosmos | Russia | Max carrying capacity, kg: 65 | on request |
| AMS-5700 Compact 5G Antenna Measurement System | ETS-Lindgren | United States | Format: Tabletop, 2D (optional 3D roll-axis stage) | on request |
| AMS-5703 5G CATR Antenna Measurement System | ETS-Lindgren | United States | Quiet zone diameter: 60 cm | on request |
| Anechoic chamber | SPUTNIX | Russia | Working volume: not less than 2x2x2 m | on request |
| Anyfields Fieldisplay — Antenna EM Radiation Visualizer | TechTheMoon | France | Function: Electromagnetic radiation visualization and antenna performance m… | on request |
| ASTROFEIN ACS Test Bed | EXA (Astro-und Feinwerktechnik) | Germany | Rotation around vertical axis: free 360° | on request |
| ATE for Space Systems | Data Patterns (India) Ltd. | India | — | on request |
| ATLAS ICU (Initiation Control Unit) | SPACERACE s.r.o. | Czech Republic | Actuation steps: Activation, arming, fire | on request |
| Automated Multi-Purpose Tester UTP 9085 | NOFFZ Technologies | Germany | Handling: Automatic rotary/indexing table through multiple test/inspection … | on request |
| Automated Test Equipment (ATE) for Aerospace and Space Applications | Data Patterns (India) Ltd. | India | Initial Product: DP-800 Multi Programmer (1994) | on request |
| Autonomous Measurements System | Glavkosmos | Russia | Purpose: Designed to verify the work of attitude determination and control … | on request |
| Board-Level Tester UTP 9011 RF | NOFFZ Technologies | Germany | DUT capacity: Up to 4 DUTs tested in parallel | on request |
| CANDELABRA | Spartan Space | France | System type: Artificial sun simulator / precision lighting array | on request |
| CanSat Kit | Hex-Star Universe | India | Sensors: Temperature, humidity, barometric pressure, altitude, GPS, acceler… | on request |
| CATR Radar Test System UTP 5069 | NOFFZ Technologies | Germany | Test technology: CATR (Compact Antenna Test Range) with integrated paraboli… | on request |
| CAVACam | XCAM | United Kingdom | Vacuum Compatibility: UHV / XHV / UCV | on request |
| Changchun Optical Payload Manufacturing AIT Center | MinoSpace | China | Integrating Sphere Diameter: 3-meter | on request |
| Climats EXCAL3 1000 Environmental Test Chamber | Climats | France | Internal dimensions (W x D x H): 1000mm x 1000mm x 1000mm | on request |
| Climats EXCAL3 140 Environmental Test Chamber | Climats | France | Internal dimensions (W x D x H): 540mm x 400mm x 700mm | on request |
| Climats EXCAL3 220 Environmental Test Chamber | Climats | France | Internal dimensions (W x D x H): 540mm x 600mm x 700mm | on request |
| Climats EXCAL3 770 Environmental Test Chamber | Climats | France | Internal dimensions (W x D x H): 900mm x 950mm x 900mm | on request |
| Comprehensive Testing Services | Experior Laboratories | United States | Vacuum level: 10⁻⁷ torr | on request |
| Control Complex of a Large-sized Products | Glavkosmos | Russia | Purpose: Real time control of large-sized product forms (from 10 m and more) | on request |
| Cryogenic Testing Services | Experior Laboratories | United States | Minimum test temperature: 4K (-269°C) | on request |
| CubeDynA | Nautilus Navigation in Space | Israel | Supported platforms: 1U to 12U CubeSats | on request |
| CubeSat ADCS Testing Facility | Glavkosmos | Russia | Purpose: Designed for functional testing of CubeSat 3U orientation and stab… | on request |
| CubeSat Kit GEN1 | Hex-Star Universe | India | Dimensions: 10 × 10 × 10 cm (1U) | on request |
| CubeSat Mechanical Ground Support Equipment (MGSE) | Serenum Space | Czech Republic | Vertical/Horizontal Support Jig material: Aluminium 2025, PA/PEEK clamps, A… | on request |
| Custom Cryostats | Lidax | Spain | Operating temperature: In-house test asset: 20 to 300 K | on request |
| Custom Thermal Vacuum Chambers | Lidax | Spain | Interface: Custom-configured size, temperature range, vacuum level, and opt… | on request |
| Customized Air Bearing System | ElmSpace | Germany | Type: Customized air bearing for ADCS ground testing | on request |
| Customized Air Bearing Test System | ElmSpace | Germany | Type: Air-bearing frictionless ADCS test platform | on request |
| Customized Air Bearings | ElmSpace | Germany | Application: Ground-based ADCS testing (frictionless air bearing tables) | on request |
| Data Logger | Magson GmbH | Germany | Channels: 3 channels | on request |
| Detector Evaluation Systems | XCAM | United Kingdom | CIS 120 Sensor Format: 2048 x 2048 pixels | on request |
| DHS 514 Pressure Converter | Glavkosmos | Russia | Estimated production / delivery time: 6 months | on request |
| DHS 517 Pressure Converter | Glavkosmos | Russia | Purpose: Measurement of sound pressure of non-aggressive gaseous media acti… | on request |
| Direct Field Acoustic Testing (DFAT) | Experior Laboratories | United States | Process time: Load-in to load-out in ≤4 days for large satellite | on request |
| DRSA-2500B / TRSA-2500B Dual/Triple Spectrum Analyzer | AVCOM of Virginia | United States | Frequency Range: 5 MHz – 2,300 MHz | on request |
| Dynamic Pressure Sensor Vt 206 | Glavkosmos | Russia | Purpose: Measurement of the static-dynamic pressure of liquid and gaseous a… | on request |
| Dynamic Spectrum Environment Emulator (DYSE®) | Parsons Space | United States | Tuning range: up to 20 GHz | on request |
| Dynamic Star Simulator DSS-25 | TY-Space Technology | China | Field Of View: 20x20 deg | on request |
| Dynamic Star Simulators (DSS-14) | TY-Space Technology | China | Field Of View: 20°×20° | on request |
| Dynamic Test System | TY-Space Technology | China | Dynamic Star Simulator: Receives quaternion from simulator computer; output… | on request |
| Dynamics Testing Services | Element Defense | United States | Acceleration Test Centrifuge Diameter: 1ft (0.3m) to 62 ft (16m) | on request |
| EGSE Box & Software | Pyxis Space | Germany | PC Interface: USB | €5 000 |
| EHP High Performance Microwave Pyramidal Absorber | ETS-Lindgren | United States | Frequency range: 30 MHz-100 GHz | on request |
| EMI/EMC Testing Services | Element Defense | United States | Radiated Susceptibility: up to 200V/m, 10kHz to 40GHz | on request |
| Emtech Space Snapshot Multi-Magnetometer Facility (Snapshot-MMF) | Emtech Space | Greece | Sensor array: 12 Bartington Mag-13MS fluxgate magnetometers | on request |
| Emtech Space Suitcase Multi-Magnetometer Facility (Suitcase-MMF) | Emtech Space | Greece | Frequency range: DC to 50,000 Hz | on request |
| End-of-Line Tester UTP 6010 RF | NOFFZ Technologies | Germany | Test type: RF functional test, end-of-line / board-level (FKT/EOL) | on request |
| End-of-Line Tester UTP 9010 RF | NOFFZ Technologies | Germany | Test type: Parallel RF functional test, EOL | on request |
| Engine Firing Test Facility — Rocket Propulsion Testing | Hokkaido Spaceport (SPACE COTAN) | Japan | Location: Launch Complex 0 (LC0), Bisei, Taiki-cho, Hiroo-gun, Hokkaido, Japan | on request |
| Environmental Simulation Testing | Element Defense | United States | — | on request |
| Environmental Stress Screening Chamber Type E1 (<3m³) | Climats | France | Temperature Range: -80°C to +200°C (+250°C on request) | on request |
| Environmental Test Chamber for Battery Testing | Climats | France | Temperature Range: -90°C to +220°C | on request |
| Environmental Test Chamber for Photovoltaic (PV) Panel Testing | Climats | France | Application: Photovoltaic (PV) module environmental and power qualification… | on request |
| Environmental Testing Services | Needronix | Poland | Test types: TVAC, vibration, shock, EMC/EMI | on request |
| Equipment for determining the center-of-mass position and inertia characteristics of nanosatellites | Glavkosmos | Russia | Inaccuracy of the center-of-mass position determining: not more then 1 mm | on request |
| EVO-CLM (Rev B) Compact Spectrum Analyzer | AVCOM of Virginia | United States | Frequency Range (Model 2290): 900–2200 MHz | on request |
| Excal GT-FC Air Generator | Climats | France | Temperature Range: -70°C to +200°C | on request |
| EXCAL³ | Climats | France | Available volumes: 150 L / 225 L / 400 L / 540 L / 770 L / 1,000 L / 1,400 … | on request |
| Extreme 320 | Climats | France | Temperature Range: +180°C to -90°C (+200°C to -100°C optional) | on request |
| EyasSat Single axis air bearing for Attitude Control Studies | EyasSat | United States | Manufacturer: EyasSat | €1 093 |
| FlatSat Ground Test Rig | HEX20 | India | PC-104 slots: 6 (CDH, EPS, COMMs, Interface Card, 2 spares) | on request |
| Flight Switch Simulator Module | Pumpkin, Inc. | United States | Simulated RBF switches: 1 | $425 |
| Force Sensor Vt 114 | Glavkosmos | Russia | Estimated production / delivery time: 6 months | on request |
| Gradiometer (MFG-2S) | Magson GmbH | Germany | Sensor configuration: Two independent fluxgate sensors in spatial gradient … | on request |
| GSE Clampband | RUAG Space | Switzerland | Clampband PAS 937 S: Manufactured per Ariane 5 User's Manual (Issue 5 Rev 2… | on request |
| Hardware Testing for Extreme Environments | Lunar Research Service | Ukraine | — | on request |
| HFF-AMF InnoWave 4 (Horizontal Far Field Antenna Measurement Facility) | Sisir Radar | India | Angular Precision: 0.45 deg | on request |
| High Altitude Balloon 300g | Hex-Star Universe | India | Mass: 300 g | on request |
| High-Temperature Thermal Chamber ESS +265°C | Climats | France | Temperature Range: -80°C to +265°C | on request |
| High-Vacuum Testing Service | OhmSpace | Italy | Minimum pressure: 1×10⁻⁶ mbar | on request |
| Hydraulics Testing Services | Element Defense | United States | — | on request |
| Hydrocarbon Safety Chamber (MIL-DO-160) | Climats | France | Temperature Range: -70°C to +180°C | on request |
| IABG Space Systems Testing and Qualification Services | IABG | Germany | Thermal vacuum chamber (Phenix, ESTEC/ETS): 4 m diameter × 10 m length, <10… | on request |
| Imager Control System (ICS) | XCAM | United Kingdom | Sensor: Teledyne e2v 'Capella', 2k x 2k back-illuminated, 10 µm pixels | on request |
| Imager Control System (ICS) for Detector Evaluation | XCAM | United Kingdom | Sensor: Teledyne e2v CIS 300 | on request |
| Instrument SCOE | CELESTIA Satellite Test & Simulation | Netherlands | Form factor: Integrated 19" rack or tabletop enclosure | on request |
| ISISPACE Training Platform | ISISPACE Group | Netherlands | Manufacturer: ISISPACE | €9 800 |
| JFPC-C8051 Programming Adapter | Pumpkin, Inc. | United States | SKU: 710-00488 | $50 |
| JFPC-MSP430 Programming Adapter | Pumpkin, Inc. | United States | SKU: 634-00334 | $50 |
| JFPC-PIC24 Programming Adapter | Pumpkin, Inc. | United States | SKU: 710-00540 | $50 |
| LABCAL | Climats | France | Available Volumes: 20 L, 30 L, 60 L, 100 L | on request |
| Labsat – Test and Development Setup | Alba Orbital | United Kingdom | — | on request |
| LabSat 3 | LabSat | United Kingdom | Constellations: GPS/Galileo/SBAS/QZSS, GLONASS, or BeiDou | on request |
| LabSat 3 Wideband | LabSat | United Kingdom | Constellations: GPS L1, L2, L5; Galileo E1, E5a/b, E6; GLONASS G1, G2, G3; … | on request |
| LabSat 4 | LabSat | United Kingdom | Constellations: GPS L1, L2, L5; Galileo E1, E5a/b, E6; GLONASS G1, G2, G3; … | on request |
| Launch Pad Count Down Test System (SDSC-SHAR) | Data Patterns (India) Ltd. | India | — | on request |
| LCS MiniNODE | LiquidCool Solutions | United States | Ingress protection: IP67 | on request |
| LCS Small-Scale Server (SSS) | LiquidCool Solutions | United States | Power range: 1.1 - 8 kW | on request |
| LCS ZPServer (Zero-Pressure Server) | LiquidCool Solutions | United States | Cooling capacity: up to 4 kW per 2U | on request |
| Load Board | Pumpkin, Inc. | United States | SKU: 711-00651 | $255 |
| Load Module | Pumpkin, Inc. | United States | VCC_SYS: +3.3V | on request |
| LoadPath 3U CubeSat Mass Simulator | LoadPath (Redwire) | — | Design simulates: mass and center of mass of a 3U CubeSat | on request |
| LoadPath 6U CubeSat Mass Simulator | LoadPath (Redwire) | — | Design simulates: mass and center of mass of a 6U CubeSat | on request |
| LRS Hardware Testing for Extreme Environments | Lunar Research Service | Ukraine | Test capabilities: Vibration testing, vibroacoustics, modal characteristics… | on request |
| Lumen Thermal Vacuum (TVAC) Test System | Hypernova Space Technologies | South Africa | Facility location: Cape Town, South Africa | on request |
| Lunar Research Service (LRS) | Lunar Research Service | Ukraine | — | on request |
| Lunar Research Service (LRS) Hardware Testing & Mission Services | Lunar Research Service | Ukraine | Flight heritage: LRS 3U satellite launch agreement with Rocket Factory Augs… | on request |
| LVDS Front-End | CELESTIA Satellite Test & Simulation | Netherlands | Channels: Up to 4 parallel inputs/outputs (8-bit) | on request |
| MA61C EGSE | Space Products and Innovation (SPiN) | Italy | Interfaces supported: SpaceWire, I2C, CAN, UART, MIL-STD-1553, GPIO | on request |
| MADS 3D Dynamic Simulator | Adcole Space (Redwire) | United States | Manufacturer: MAI | €8 661 |
| Magnetic Field Simulator | Glavkosmos | Russia | Purpose: Designed for magnetic field simulation along the orbital trajector… | on request |
| Mass-spectrometer Helium Leak Detector Type | Glavkosmos | Russia | Year of release: 2011 | on request |
| Measuring Instrument KS T-406N Tester | Glavkosmos | Russia | Purpose: T-406N KS tester is intended to control technical characteristics … | on request |
| Mechanical Shock Testing | Element Defense | United States | — | on request |
| Mechanical Shock Testing Services | Experior Laboratories | United States | Classical shock: Up to 1,500 G | on request |
| Metrology | General Atomics Synopta GmbH | Switzerland | Capabilities: Point spread function, focal length, distortion, magnificatio… | on request |
| MIL-1553 Front-End | CELESTIA Satellite Test & Simulation | Netherlands | Form factor: 19" 2U hardware platform | on request |
| MinoSpace Advanced Equipment Manufacturing Laboratory | MinoSpace | China | Total area: nearly 5,000 square meters | on request |
| Model 2265 Multi-Channel PCM Bit Synchronizer | GDP Space Systems | United States | Channels: Up to 4 per 2U chassis | on request |
| Model 2267C Multi-Channel Correlating Best Source Selector | GDP Space Systems | United States | Input streams: Up to 16 | on request |
| Modular Chamber (CM) Volume over 3m³ | Climats | France | Volumes: from 8 to 100 m³ | on request |
| Modular Chamber for Burn-In (RELY STATION) | Climats | France | Temperature Range: 0°C to +70°C | on request |
| MPT-G Multi-Purpose Trolley Giga | RUAG Space | Switzerland | Motion: Table tilts and rotates to any attitude between spin axis vertical … | on request |
| Multi-DUT Burn-In / Screening Tester UTP 9065 | NOFFZ Technologies | Germany | Test type: Multi-DUT burn-in, screening, long-term functional test | on request |
| Multi-Purpose Interface Platform (MPIP) | CELESTIA Satellite Test & Simulation | Netherlands | Chassis: 3U 19" rack mountable or tabletop (4U/2U variants available) | on request |
| Munitions Testing | Element Defense | United States | — | on request |
| Nanosatellite Debug Board | Glavkosmos | Russia | Purpose: Board designed to allow debugging of any onboard system or full na… | on request |
| NF-AMF Hexahedron (Near Field Antenna Measurement Facility) | Sisir Radar | India | Maximum Scanning Area: 1.5 m x 1.5 m | on request |
| NPL Space Metrology and Calibration Services | National Physical Laboratory (NPL) | United Kingdom | Services: Precision metrology, sensor calibration | on request |
| Optical Star Pattern Simulator (OSPS) | TY-Space Technology | China | Field Of View: 15°×15° | on request |
| OSI Optical Sky Stimulator | Jena-Optronik | — | Function: Dynamic closed-loop end-to-end star sensor testing | on request |
| OSPS Optical Star Pattern Stimulator | Jena-Optronik | — | Function: Static star pattern simulation (open-loop) | on request |
| PEB1 VA416X0 Radiation-Hardened MCU Development Kit | VORAGO Technologies | United States | Target MCU Options: VA41620 or VA41630 (ARM Cortex-M4, HARDSIL) | on request |
| PFO 1040 | XCAM | United Kingdom | Total Detection Area: 4 cm2 | on request |
| Piezoelectric Pressure Pulsation Sensor LH 604 | Glavkosmos | Russia | Estimated production / delivery time: 6 months | on request |
| Piezoelectric Pressure Pulsation Sensor LH 608 | Glavkosmos | Russia | Range of measurements of pressure pulsations, Mpa: 0,05-5,0 | on request |
| PJP-CP26 Conformal Printer | Space Foundry | United States | Process: Single-step atmospheric-pressure plasma jet printing, no pre- or p… | on request |
| PJP-DT155 Desktop System | Space Foundry | United States | Process: Single-step atmospheric-pressure plasma jet printing, no pre- or p… | on request |
| Platform for Installation of Cubesat 3U satellite | Glavkosmos | Russia | Purpose: Designed for CubeSat 3U satellite with ADCS installation to test o… | on request |
| Platform for Installation of Tabletsat Devices | Glavkosmos | Russia | Purpose: Designed for "TabletSat" satellite devices installation to test on… | on request |
| Platform for Installation of the Satellite Tabletsat | Glavkosmos | Russia | Purpose: Designed for "TabletSat" satellite installation to test on air-bea… | on request |
| Pneumatic Testing Services | Element Defense | United States | — | on request |
| Precision Electronic Component Testing for Critical Systems | AAA Engineering & Test Lab | United States | Years of hands-on expertise in MIL-STD and NASA programs: 15+ | on request |
| Primary Linear Displacement Transducer Vt 718 | Glavkosmos | Russia | Purpose: Measurement of linear displacements of objects in rocket and space… | on request |
| PSA-2500C Portable Spectrum Analyzer | AVCOM of Virginia | United States | Frequency Range: 5 MHz–2300 MHz | on request |
| PSA-4200C | AVCOM of Virginia | United States | Applications: Satellite, TV and Radio Broadcasting, CATV, Wireless, TCSM, a… | on request |
| QS RF Locator | Quadsat ApS | Denmark | Function: Drone-based RF interference localization | on request |
| QS RF Measurement System (QS 1-18 DL) | Quadsat ApS | Denmark | Frequency Range: 1–18 GHz | on request |
| Quadsat Antenna Measurement System | Quadsat ApS | Denmark | Measurement capabilities: Pointing accuracy, tracking and handover, radiati… | on request |
| Rackmount SUPERNOVA Satellite Simulator (RS3) | Pumpkin, Inc. | United States | Form factor: 2U rackmount unit | $45 000 – $60 485 |
| Radar Seeker Integrated Tester | Beijing Huali Chuangtong Technology Co., Ltd. | China | — | on request |
| Radar Test System UTP 5065 | NOFFZ Technologies | Germany | Test type: Direct near-field radar sensor test | on request |
| Radian Reusable Reentry Vehicle (R3V) | Radian Aerospace | United States | Flight profiles: High-speed, high-stress (launch through hypersonic transit… | on request |
| Research Flights | Zero-G Solutions | United States | Parabolas per research flight: 30 (double standard flight) | on request |
| RF SCOE | CELESTIA Satellite Test & Simulation | Netherlands | Form factor: 19" rack | on request |
| RF Suitcase | CELESTIA Satellite Test & Simulation | Netherlands | Form factor: Transportable system | on request |
| Robotic Arm Integration Printer | Space Foundry | United States | Process: Single-step atmospheric-pressure plasma jet printing, orientation … | on request |
| Robotic Testbed for Satellite Servicing | Lunasa Space | United Kingdom | Arm Payload capacity: Upto 30 kg | on request |
| S-Band Test Cap | WiRan | Poland | Frequency range: 2025-2290 MHz | on request |
| SA-MOD-1-9-B Embedded Spectrum Analyzer Module | AVCOM of Virginia | United States | Frequency Range (Model 2290): 900–2200 MHz | on request |
| Satellite Qualification & Acceptance Testing Services | Serenum Space | Czech Republic | Mechanical test types: Resonance search, quasistatic, sine, random, shock | on request |
| Satellite Transport and Shipping Containers | RUAG Space | Switzerland | Container types: Hat-off, tilt-lid, door-type roll-in, large An124-compatib… | on request |
| SatSim — Satellite Pass Emulator | Quadsat ApS | Denmark | Function: Orbital trajectory emulation via UAV | on request |
| SBS2-2150E-RSA | AVCOM of Virginia | United States | Input Frequency Range: 950MHz to 2150MHz (extended L-Band) | on request |
| SCAL CTH2 | Climats | France | Touchscreen: Extra-large 15″ touchscreen | on request |
| SCAL CTH3/CTY Thermal Shock Chamber (3 environments) | Climats | France | Temperature Range: -90°C to +180°C (+220°C optional) | on request |
| SCAL CTK | Climats | France | SCAL 230CTK7.5 Temperature Range: -80/+180°C | on request |
| SCAL-CTR | Climats | France | Display: Extra-large 15" touchscreen | on request |
| SCO-M Spacecraft Container Mega | RUAG Space | Switzerland | Product line: Beyond Gravity spacecraft containers (SCO) | on request |
| Sensor of Rapidly Varying Pressure 612M | Glavkosmos | Russia | Estimated production / delivery time: 6 months | on request |
| Set of Fixing Devices of Nanosatellite | Glavkosmos | Russia | Purpose: Designed for fixing of the nanosatellite at the desktop of the equ… | on request |
| Signal Analyzers / Spectrum & Beacon Receivers | EUROSATCOM | France | EVO-CLM (Rev B): L-Band or 400-3000 MHz, compact form factor | on request |
| Silicon Labs USB Debug Adapter | Pumpkin, Inc. | United States | SKU: 633-00489 | $100 |
| SIMAC-6 Multi-Constellation GNSS Simulator | Accord | India | Channels: 120+ | on request |
| Single Sampler EGSE | Lens R&D | Netherlands | Manufacturer: Lens R&D | €11 887 |
| skyEGSE-comm (S-band) | SkyLabs d.o.o. | Slovenia | Type: CCSDS-compliant SDR ground station equipment | on request |
| skyEGSE-comm (UHF/VHF) | SkyLabs d.o.o. | Slovenia | Type: CCSDS-compliant SDR ground station equipment | on request |
| skyEGSE-LINK2 | SkyLabs d.o.o. | Slovenia | Standard: IPC Class 3+ | on request |
| Small Space Environment Simulation System | Xi'an Institute of Optics and Precision Mechanics (XIOPM) | China | Type: Thermal-vacuum space environment simulation chamber | on request |
| SNG-2500C | AVCOM of Virginia | United States | Design: Simple and easy to use design at a low price | on request |
| SOC-100 Hemispherical Directional Reflectometer | Surface Optics Corporation | United States | Spectral Range: 2.0 – 25.0 λ (μm) / 5000 – 400 cm-1 Range can be modified b… | on request |
| SOC-210 Bidirectional Reflectometer | Surface Optics Corporation | United States | Spectral range: 0.35-14 micron | on request |
| Solar Panel Check Stand | Glavkosmos | Russia | Purpose: Provides weight relief and opening-out testing of small-size Produ… | on request |
| Solar Weightless System | Glavkosmos | Russia | Purpose: Designed for ground testing (weightlessness) of spacecraft equipme… | on request |
| Space PFO | XCAM | United Kingdom | Total Detection Area: 4 cm2 | on request |
| Space Qualified Coaxial Termination | KRYTAR | United States | Model T1M-SQ: DC-20.0 GHz, 1.05 max VSWR, 3.5mm male | on request |
| Spacecraft Interface Simulator (SIS) | CELESTIA Satellite Test & Simulation | Netherlands | Flight heritage: SOHO, CLUSTER, ROSETTA | on request |
| Spacecraft Lifting Devices | RUAG Space | Switzerland | Actuation: Electrical or manual | on request |
| SPECTRAN V6 TABLET | Aaronia AG | Germany | Frequency range (family): 9 kHz up to 18 GHz (model-dependent, up to 140 GH… | on request |
| SpinLaunch Suborbital Accelerator | SpinLaunch | United States | Vacuum chamber span: 33 meters | on request |
| Standard Fluxgate Magnetometer | Magson GmbH | Germany | Sensor type: Tri-axial fluxgate, single or dual sensor configuration | on request |
| Starry Sky Simulator | Glavkosmos | Russia | Purpose: Designed for star trackers testing together with other ADCS compon… | on request |
| Static Test System | TY-Space Technology | China | Optical Star Pattern Simulator: Static star simulator, North Pole Area/Cust… | on request |
| Sun Simulator (halogen) | Glavkosmos | Russia | Purpose: Designed for testing of ADCS Sun orientation capability | on request |
| Synthesis System of IR Images | Glavkosmos | Russia | Purpose: Designed to create dynamic infrared images of arbitrary topology i… | on request |
| TDEMI ULTRA | GAUSS Instruments | Germany | Frequency range: DC to 40 GHz | on request |
| Technical Condition Monitoring System | Glavkosmos | Russia | Year of release: 2014 | on request |
| Term, SMA-m, 26.5GHz, 1W (Item #2001-61XX-0X-CRYO) | XMA Corporation | United States | Item #: 2001-61XX-0X-CRYO | on request |
| Test Bench for Mutual Movement of Spacecraft | Glavkosmos | Russia | Dimensions, mm: 5000kh6000kh3000 | on request |
| Test Bench For Nanosatellite Attitude Control System | Glavkosmos | Russia | Purpose: Conducting testing of control algorithms. Training of students and… | on request |
| Test Bench for RASCube Modules | Robinson Aerospace Systems | Australia | Compatibility: RASCube V1, V2 and LB | on request |
| Test Bench to Examine Radio-Technical Performance of Antennas | Glavkosmos | Russia | Purpose: High precision transfer and rotation of the target object in the 3… | on request |
| Test Space | TRL Space | Czech Republic | shaker force: 45 kN (90 kN Shock) | on request |
| Thermoelectric Converter DT 27 | Glavkosmos | Russia | Purpose: Temperature measurement of aggressive (liquid oxygen) and non-aggr… | on request |
| TILT | TRL Space | Czech Republic | Integrate CubeSats of sizes from: 6-16 U | on request |
| TM/TC Front-End | CELESTIA Satellite Test & Simulation | Netherlands | Form factor: 19" 3U hardware platform | on request |
| TM/TC IPU (Telemetry & Telecommand Interface Unit) | SSBV Aerospace & Technology | Netherlands | — | on request |
| Total Phase Beagle I2C/SPI Protocol Analyzer | Pumpkin, Inc. | United States | SKU: 634-00522 | $495 |
| Tpod L CubeSat Test Fixture | LAUNCH42 | Netherlands | Size: TPOD-L | €15 800 |
| Tpod M CubeSat Test Fixture | LAUNCH42 | Netherlands | Size: TPOD-M | €11 500 |
| Transformable Reflectors Weightless System | Glavkosmos | Russia | Year of release: 2016 | on request |
| TTC Modem for AIT (TTC-IMBU) | CELESTIA Satellite Test & Simulation | Netherlands | IF inputs/outputs: 2 (typically 70MHz) | on request |
| UAV Satcom Test Tools | Gatehouse Satcom | Denmark | — | on request |
| Ultra-High-Speed Streak Camera | Xi'an Institute of Optics and Precision Mechanics (XIOPM) | China | Technology: Photoelectric streak tube with CCD/CMOS readout | on request |
| UNISEC Europe Bus Starter Kit | S4 - Smart Small Satellite Systems GmbH | Germany | Satellite bus connector: Compact/robust backplane, redundant power + high/l… | on request |
| Universal Wireless Tester (UWT) | NOFFZ Technologies | Germany | Standards supported: 5G NR, LTE, WCDMA, GSM, V2X, 802.11 a/b/g/n/ac/ax/p, B… | on request |
| USB Debug Adapter | Pumpkin, Inc. | United States | Connector: 4-pin FPC serial terminal/debug connector | on request |
| VacCam | XCAM | United Kingdom | Dimensions: 50 x 50 x 60 mm (excl. lens and USB connector) | on request |
| VACCO ∆TEL Differential Pressure Indicator | VACCO Industries | United States | Material: Aluminum (std), Corrosion Resistant Steel (optional) | on request |
| VFF-AMF InnoWave 4 (Vertical Far Field Antenna Measurement Facility) | Sisir Radar | India | Angular Precision: 0.45 deg | on request |
| Volume over 3m³ Rigid Structure Type G | Climats | France | Volumes: from 3 m3 to 100 m³ | on request |
| Weight-measuring Platform Devices | Glavkosmos | Russia | Purpose: Weighing of transport fuelling containers in the static weighing m… | on request |
| WINCAL | Climats | France | Chamber type: Walk-in chamber, rigid structure | on request |
| WizardLink Front-End | CELESTIA Satellite Test & Simulation | Netherlands | Channels: Up to 4 WizardLink channels in parallel | on request |
| XO-VAC | Exobotics | United Kingdom | Price: From £48,000 (base model) | from £48 000 |
| Zero Bias Schottky Detectors 203A | KRYTAR | United States | Minimum Frequency: 10 MHz | on request |
Products
R&D company providing miniaturized radiation dosimeters and EMC filters for space and ground applications. TRL-9 flight heritage.

A complete evaluation setup containing a RadNano-EM model with additional circuitry and connectors, also serving as an add-on board for development projects.
| UART Protocol | 9600 8-N-1 |
| I2C Protocol | Standard |
AAA Engineering & Test Lab provides precision electronic component testing, upscreening, failure analysis, and counterfeit mitigation services for aerospace, space, defense, medical, and industrial ap

AAA Engineering & Test Lab delivers rigorous semiconductor and electronic component testing to MIL-STD-202, MIL-STD-461, MIL-STD-750, MIL-STD-883, MIL-STD-1580, and NASA specif
| Testing standards | MIL-STD-202, MIL-STD-461, MIL-STD-750, MIL-STD-883, MIL-STD-1580, NASA specifications |
| Key standards & certifications - Military & NASA | MIL-STD-202, MIL-STD-461, MIL-DT-750, MIL-STD-883, MIL-STD-1580; NASA MIL-PRF for environm |
| Key standards & certifications - Quality Systems | ISO 9001, AS9100, ISO/IEC 17025, AS6081/AS6171, ANSI ESD S20.20 |
| Key standards & certifications - Regulatory | ITAR Registered, EAR Compliant, DFARS/FAR Adherent |
| Experience | 15+ Years of hands-on expertise in MIL-STD and NASA programs |

AAA Engineering & Test Lab offers comprehensive electronic component testing services, including electrical, environmental, mechanical, and chemical testing, to ensure reliabil
| Years of hands-on expertise in MIL-STD and NASA programs | 15+ |
| Accreditation for electrical, environmental and mechanical testing scopes | ISO 9001/AS9100 |
| Accreditation for counterfeit mitigation testing and authentication | ISO/IEC 17025 AS6081/AS6171 |
| Key Standards & Certifications - Military & NASA | MIL-STD-202, MIL-STD-461, MIL-DT-750, MIL-STD-883, MIL-STD-1580; NASA MIL-PRF for environm |
| Key Standards & Certifications - Quality Systems | ISO 9001, AS9100, ISO/IEC 17025, AS6081/AS6171, ANSI ESD S20.20 |
Aaronia AG develops and manufactures spectrum analyzers, spectrum analysis software, and drone detection and defense systems, all produced in Germany.

A rugged, handheld real-time spectrum analyzer in a tablet form factor, offered in configurations up to 18 GHz for detecting and geolocating RF interference during live satellite g
| Frequency range (family) | 9 kHz up to 18 GHz (model-dependent, up to 140 GHz across full V6 line) |
| Real-Time Bandwidth | 44 MHz (up to 490 MHz on other V6 tablet variants) |
| Sweep speed | max. 3 THz/s; well over 1.5 THz/s at 18 GHz span |
| Sensitivity (DANL) | -170 dBm/Hz |
| Internal storage | max. 16 TB |
Accord Software & Systems designs and manufactures customized GPS/GNSS receivers for space applications and GPS/GNSS semiconductor chips for defense and commercial markets.

120+ channel dual-frequency GNSS simulator supporting GPS, GLONASS, Galileo, BeiDou, NavIC, SBAS, and DGNSS with high-dynamics simulation for receiver testing.
| Channels | 120+ |
| Constellations | GPS, GLONASS, Galileo, BeiDou, NavIC, SBAS, DGNSS |
| Frequencies | Dual-frequency including NavIC L5 and S-band |
| Hardware update rate | Up to 10 ms |
| Output formats | RINEX, NMEA |
Redwire is an integrated aerospace and defense company providing advanced technologies for space infrastructure, autonomous systems, and multi-domain operations to government agencies and defense cont

The dynamic simulator provides a HITL (Hardware In The Loop) test set for the MAI-400 which verifies and validates all software and hardware functions in a bench top setting. In…
| Manufacturer | MAI |
| Lead time | 90 days |
Alba Orbital manufactures PocketQube satellites, provides launch and ground station services, and operates a fleet of nighttime imaging satellites for government and commercial clients.

A horizontal integration jig that supports the assembly of 1p, 2p, or 3p PocketQube stacks into the primary structure, with a raised design suitable for testing deployables like an
| Length | 272 mm |
| Width | 125 mm |
| Height (without Spacecraft) | 40 |
| Clearance below Spacecraft | 10 mm |
| Material | Acetal |

The Labsat is a test and development setup designed for PocketQube boards, allowing users to safely test and characterize single boards or full stacks without direct interaction.
AVCOM of Virginia is a satellite communications equipment manufacturer founded in 1976, specializing in spectrum analyzers, satellite beacon receivers, and RF signal monitoring products.

Dual or triple embedded spectrum analyzers in 1U rack, for simultaneous multi-carrier satellite signal monitoring.
| Frequency Range | 5 MHz – 2,300 MHz |
| Span Width | Up to 1300 MHz |
| Resolution Bandwidth | 10 kHz, 100 kHz, 300 kHz, 1 MHz |
| RF Sensitivity | >-85 dBm typical |
| Dynamic Range | 50 dBm GUI window |

Compact spectrum analyzer built on DSP/FPGA platform, supports Ethernet/USB, 900–3000 MHz or 400–3000 MHz.
| Frequency Range (Model 2290) | 900–2200 MHz |
| Frequency Range (Model 3040) | 400–3000 MHz |
| Max Span Width | 1300 MHz |
| Resolution Bandwidth | 1 kHz, 3 kHz, 10 kHz, 30 kHz, 100 kHz, 300 kHz, 1 MHz |
| RF Sensitivity (-40 REF LVL) | -100 dBm |

Portable spectrum analyzer covering 5 MHz–2300 MHz with Li-Ion battery, for satellite installation and testing.
| Frequency Range | 5 MHz–2300 MHz |
| Span Width | Up to 1300 MHz |
| Resolution Bandwidth | 10 kHz, 100 kHz, 300 kHz, 1 MHz |
| RF Sensitivity | >-85 dBm typical |
| Amplitude Range | 0 dBm to -85 dBm (standard); 0 to -105 dBm (preamp) |

A portable C-band spectrum analyzer for satellite, TV/radio broadcasting, CATV, wireless, TCSM, and GPS signal monitoring, with LNA/LNB power output and remote control software.
| Applications | Satellite, TV and Radio Broadcasting, CATV, Wireless, TCSM, and GPS |
| L.O. Frequency Offsets | Displays Direct Frequency Readout |
| Presets/Memory | 10 Customizable Presets/50 User Memory Locations |
| Refresh Rate | Up to 13/sec |
| LNA/LNB Power | 13/18Vdc/22kHz |

Ultra-compact embedded spectrum analyzer module, 3"×3.5"×1", 8-33 VDC, -40 to +70°C, 40,000 ft altitude.
| Frequency Range (Model 2290) | 900–2200 MHz |
| Frequency Range (Model 3040) | 400–3000 MHz |
| Frequency Range (Model 6070) | 70–6000 MHz |
| RF Sensitivity (-40 REF LVL) | -100 dBm |
| Spur Free Dynamic Range (3 kHz RBW) | 60 dB |

The SBS2-2150E-RSA is a remote L-Band spectrum analyzer module designed for OEM integration, providing remote signal monitoring and control for satcom applications via Ethernet or
| Input Frequency Range | 950MHz to 2150MHz (extended L-Band) |
| Reference Signal Monitoring | 10MHz reference signal viewing capability |
| Input Voltage | +15 to +24VDC |
| Power Consumption | 7W |
| Communication Interfaces | Ethernet or USB (commercial connectors or header connectors) |

Rack-mount spectrum analyzer for monitoring and measuring satellite communications and broadcast carriers, including uplink, downlink, L-band, IF, and TT&C signals.
| Design | Simple and easy to use design at a low price |
| Presets | 10 customizable presets |
| Display | VGA color display |
| Mounting | Fits into Tektronix 1700 series dual mount tub |
| Refresh Rate | Up to 13/sec |
Huali Chuangtong (华力创通, Hwacreate) is a Chinese satellite navigation and IoT technology company listed on the Shenzhen Stock Exchange, headquartered in Beijing, developing GNSS (GPS/BeiDou) navigation modules, IoT terminals, and satellite c

The radar seeker integrated tester generates passive radar test signals and active radar echo signals, and captures and analyzes active radar transmit signals. It comprehensively t
Celestia Satellite Test & Simulation provides ground-based solutions for satellite simulation, testing, communication, and data processing, including EGSE, TT&C, and Optical Modems.

Turn-key system providing electrical and protocol interfaces to satellite instruments during development and AIT — power, control/monitor, and science interfaces.
| Form factor | Integrated 19" rack or tabletop enclosure |
| Isolation | Galvanic isolation, FMEA compliant |

LVDS Data/Clock interface unit for satellite flight equipment across all AIT levels — up to 4 parallel channels, up to 2Gbps at 16-bit.
| Channels | Up to 4 parallel inputs/outputs (8-bit) |
| Data rate | Up to 1Gbps per channel (8-bit), teaming to 16-bit at 2Gbps |
| Clocking | >125MHz |
| Compliance | TIA/EIA-644-A |
| Data streaming | 10Gbit LAN |

EGSE unit controlling, monitoring, and simulating flight equipment on the satellite onboard data handling bus — MIL-STD-1553B BC/RT/BM functions, ECSS compliant.
| Form factor | 19" 2U hardware platform |
| Functions | MIL-STD-1553B Bus Controller/RT/Bus Monitor |
| Minor frame interval | Configurable (e.g. 125/50/12.5ms) |
| Compliance | ECSS-E-ST-50-13C |

Modular, scalable EGSE testing spacecraft electrical/data interfaces — supports up to 16 modules, >400 channels, ESA/ECSS compliant.
| Chassis | 3U 19" rack mountable or tabletop (4U/2U variants available) |
| Interface modules | Up to 16 |
| Channels | >400 fully equipped |
| Data interfaces | Discrete/TM/TC/Power/Digital Data (up to 800Mbps) |
| Ethernet ports | 2x Gigabit |

Radio Frequency Special Check-Out Equipment validating satellite RF subsystems — flight heritage on ESA missions including Sentinel-2, EarthCare, SeoSat.
| Form factor | 19" rack |
| Flight heritage | Sentinel-2, EarthCare, SeoSat, Apogee AS250, VHR |

Transportable system for ground station and satellite RF compatibility testing — built using Engineering Models of transponder, TWTAs, diplexer, and filters.
| Form factor | Transportable system |
| Components | Engineering Models of transponder, TWTAs, diplexer, filters |

Testing equipment allowing an instrument or spacecraft unit to be developed and tested prior to overall spacecraft integration — flight heritage on SOHO, CLUSTER, ROSETTA.
| Flight heritage | SOHO, CLUSTER, ROSETTA |

Telemetry and telecommand unit for direct spacecraft control during AIT and launch phases — 60x RS422/LVDS pairs, galvanically isolated.
| Form factor | 19" 3U hardware platform |
| Baseband interfaces | 60x RS422/LVDS pairs |
| Isolation | Galvanically isolated, FMEA compliant |

Integrated modem and baseband unit for direct spacecraft control/monitoring in EGSE environments — FPGA-based real-time modulation/demodulation, Doppler/ranging processing.
| IF inputs/outputs | 2 (typically 70MHz) |
| Data rates | 7.8125bps-10Mbps |
| Suppressed carrier modes | BPSK/QPSK/OQPSK/GMSK |
| Remnant carrier modes | SPL/PM, BPSK/PM |
| Ranging standards | ESA Standard/Tone/PN Ranging (T2B, T4B) |

High-speed serial interface unit for spacecraft flight equipment validation — up to 4 parallel channels at 2Gbps each, 10Gbit LAN data streaming.
| Channels | Up to 4 WizardLink channels in parallel |
| Data rate | Up to 2Gbps per channel |
| Chipset | TI TLK2711-SP/TLK2711A |
| Clock | Programmable 80-125MHz |
| Data streaming | 10Gbit LAN (SFP+) |
Climats is a French manufacturer of high-precision environmental and climatic test chambers, including customized thermal-vacuum chambers for space qualification testing.

A universal environmental test chamber with 1000 liters internal volume, offering temperature ranges down to -85°C and various cooling/heating rates.
| Internal dimensions (W x D x H) | 1000mm x 1000mm x 1000mm |
| External dimensions (W x D x H) | 1285mm x 2325mm x 2165mm |
| Internal volume | 1000 LITERS |
| Minimum temperature | -50°C (EXCAL 10052-T/H, EXCAL 10053-T/H), -70°C (EXCAL 10023-T/H), -75°C (EXCAL 10024-T/H, |
| Rate of cooling (IEC 60068-3-5) | 4 K/min (EXCAL 10052-T/H), 13.5 K/min (EXCAL 10053-T/H), 2 K/min (EXCAL 10023-T/H), 4.5 K/ |

A compact environmental test chamber with 151 liters internal volume, offering temperature ranges down to -80°C and various cooling/heating rates.
| Internal dimensions (W x D x H) | 540mm x 400mm x 700mm |
| External dimensions (W x D x H) | 783mm x 1634mm x 1842mm |
| Internal volume | 151 LITERS |
| Minimum temperature | -50°C (EXCAL 1451-T/H, EXCAL 1452-T/H), -70°C (EXCAL 1421-T/H), -80°C (EXCAL 1423-T/H*) |
| Rate of cooling (IEC 60068-3-5) | 7 K/min (EXCAL 1451-T/H), 11 K/min (EXCAL 1452-T/H), 5 K/min (EXCAL 1421-T/H), 12 K/min (E |

A compact environmental test chamber with 227 liters internal volume, offering temperature ranges down to -80°C and various cooling/heating rates.
| Internal dimensions (W x D x H) | 540mm x 600mm x 700mm |
| External dimensions (W x D x H) | 783mm x 1912mm x 1842mm |
| Internal volume | 227 LITERS |
| Minimum temperature | -50°C (EXCAL 2251-T/H, EXCAL 2252-T/H), -70°C (EXCAL 2221-T/H), -80°C (EXCAL 2223-T/H, EXC |
| Rate of cooling (IEC 60068-3-5) | 4.2 K/min (EXCAL 2251-T/H), 10 K/min (EXCAL 2252-T/H), 5 K/min (EXCAL 2221-T/H), 10 K/min |

A high-performance environmental test chamber with 769 liters internal volume, offering temperature ranges down to -90°C and various cooling/heating rates.
| Internal dimensions (W x D x H) | 900mm x 950mm x 900mm |
| External dimensions (W x D x H) | 1181mm x 2279mm x 2064mm |
| Internal volume | 769 LITERS |
| Minimum temperature | -50°C (EXCAL 7752-T/H, EXCAL 7753-T/H), -70°C (EXCAL 7723-T/H), -75°C (EXCAL 7724-T/H), -8 |
| Rate of cooling (IEC 60068-3-5) | 5 K/min (EXCAL 7752-T/H), 15 K/min (EXCAL 7753-T/H), 4 K/min (EXCAL 7723-T/H), 7 K/min (EX |

ESS thermal chamber, -80°C to +200°C, up to 20°C/min ramp for on-board electronics reliability testing.
| Temperature Range | -80°C to +200°C (+250°C on request) |
| Volume | Less than 3m³ (E1 Type) |
| Absorbed Dissipative Power | Over 30kW |
| Ventilation | Greater than 2m/s |
| Noise Level | <70 dBA (Energy Saving mode) |

Thermal test chamber for battery safety testing, -90°C to +220°C, with fire/explosion/outgassing protection.
| Temperature Range | -90°C to +220°C |
| Volume | Few m³ to several m³ |
| Display | 15" touchscreen |
| Energy Savings | ≥40% (Energy Saving mode) |
| Safety Features | Nitrogen inerting, O2 analyzer, explosive gas detector, pressure relief, smoke/gas/flame d |

Environmental test chamber built to standard test protocols for photovoltaic module durability and power qualification.
| Application | Photovoltaic (PV) module environmental and power qualification testing |
| Handling system | Adaptive cart system for module loading/storage |
| Power supply integration | Continuity and power-output testing via Spirale Vision control |
| Control system | Spirale Vision, 15-inch touchscreen |

Localized thermal conditioning air generator, -70°C to +200°C, up to 32 Nm³/h, for electronic component testing.
| Temperature Range | -70°C to +200°C |
| Air Flow | up to 32 Nm³/h |
| Temperature Stability | ±0.1°C |
| Average Temperature Variation | >120°C/min |
| Flexible Hose Length | 2200 mm (±100) |

EXCAL³ is a modular climatic test chamber range covering temperatures from -90°C to +180°C with rapid ramp rates up to 25°C/min, used for environmental qualification testing from l
| Available volumes | 150 L / 225 L / 400 L / 540 L / 770 L / 1,000 L / 1,400 L / 1,900 L |
| Minimum accessible temperature | Up to -50°C with fluid R-744 (CO₂); Up to -65°C / -90°C with fluids R-449A / R-469 |
| Maximum accessible temperature | +180°C (+250°C optional) |
| Temperature variation speed | Between 2°C/min and 25°C/min |
| Relative humidity range | 5 to 98%RH at +10°C to +95°C |

Extreme 320 is a climatic test chamber from Climats equipped with the Spirale touchscreen control system, offering multiple user levels and specialized cycle modes for extreme-temp
| Temperature Range | +180°C to -90°C (+200°C to -100°C optional) |
| Temperature Homogeneity | ±0.5°C to ±1.5°C; ±0.3°C stability |
| Chamber Volume | 320 dm³ |
| Useful Dimensions (W×D×H) | 750 × 500 × 850 mm |
| Footprint | Less than 2.5 m² |

Extreme high-temp ESS chamber, -80°C to +265°C, for electronic board qualification in extreme environments.
| Temperature Range | -80°C to +265°C |
| Speed Variation | 10°C/min linear from +200°C to -40°C, with 10 kg of PCBs |

Secure hot-cold chamber for kerosene-filled aviation fuel tank testing, -70°C to +180°C, per MIL-DO-160.
| Temperature Range | -70°C to +180°C |
| Speed Variation | 10°C/min average from +70°C to -55°C (30kg load, 1kW dissipation) |
| Standard | MIL-DO 160 military and civil aeronautical standard |
| Useful Dimensions (W×D×H) | 1000 × 1000 × 1000 mm |

LABCAL is a benchtop temperature and humidity test chamber for rapid climatic cycling to detect defects or determine product shelf life.
| Available Volumes | 20 L, 30 L, 60 L, 100 L |
| Temperature Range | -70°C to +180°C |
| Relative Humidity Range | 10 to 95% RH (for temperatures +10 to +95°C) |
| Temperature Homogeneity | ±0.5 to ±2°C at +180°C |

The Modular Chamber (CM) is a custom-built environmental test chamber with volumes ranging from 8 to 100 m³, capable of temperatures from -70°C to +80°C. It features a modular pane
| Volumes | from 8 to 100 m³ |
| Temperatures | from -70°C to +80°C |
| Working temperatures (max) | +80°C |

Modular burn-in/ESS chamber for electronic control racks, 0°C to +70°C, combines burn-in with environmental testing.
| Temperature Range | 0°C to +70°C |
| Speed Variation | 3°C/min average (300 kg cabinets, 6 kW dissipation) |
| Useful Dimensions (W×D×H) | 3000 × 7000 × 2750 mm |

SCAL CTH2 is a climatic test chamber equipped with the Spirale touchscreen control system for programmable temperature/humidity cycling and shock/VRT reproducibility testing.
| Touchscreen | Extra-large 15″ touchscreen |
| Levels of use | Production, Standard, Laboratory |
| Tracking alarm | Shock or VRT mode to ensure reproducibility of tests |
| Pre-treatment/post-treatment | Programmable on Spirale Vision, to temperature condition or dry samples at the beginning a |
| Automatic defrost | Spirale Vision optimizes the cycle so defrosting is carried out correctly without disturbi |

3-zone thermal shock chamber (hot/cold/ambient transition), 70-1500L, -90°C to +180°C, MIL-STD compliant.
| Temperature Range | -90°C to +180°C (+220°C optional) |
| Test Volume (CTH3 Horizontal) | 70-1500 liters |
| Test Volume (CTY Vertical) | up to 120 liters |
| SCAL 1000CTH3-22 Carrier Volume | 1000 L |
| Standards Compliance | DIN-IEC-60068-2-14, JESD22-A104D, MIL-STD-202G/750E/810G/883H |

A thermal shock/climatic test chamber (SCAL CTK) equipped with the Spirale control system, offering multi-level operation and advanced test cycle management for reproducible enviro
| SCAL 230CTK7.5 Temperature Range | -80/+180°C |
| SCAL 300CTK7.5 Temperature Range | -85/+180°C |
| SCAL 500CTK15 Temperature Range | -90/+180°C |
| Hot Cabinet Range (all models) | +60/+180°C |
| Standards Compliance | DIN, IEC 60068-2-14, JESD22-A104D, MIL-STD-202G, MIL-STD-750E, MIL-STD-810G, MIL-STD-883H |

SCAL-CTR is a vertical thermal shock test chamber controlled via the Spirale touchscreen interface, used to subject samples to rapid temperature cycling for qualification and relia
| Display | Extra-large 15" touchscreen |
| Usage levels | Production, Standard, Laboratory |
| Tracking alarm | CHoc or VRT mode, for reproducibility of tests |
| Pre-treatment/post-treatment | Programmable on Spirale Vision, to temperature condition or dry samples at start/end of cy |
| Automatic defrost function | Spirale Vision optimizes the cycle so defrosting does not disturb sample temperature |

The CLIMATS Type G environmental test chamber offers large test volumes (3 m³ to 100 m³) and a wide temperature range (-70°C to +150°C) for testing large samples.
| Volumes | from 3 m3 to 100 m³ |
| Temperature | from -70°C to +150°C |
| CLIMATS metallic structure enabling to function | up to +150°C (max) |

WINCAL is a rigid-structure walk-in environmental test chamber offering large standard test volumes with wide temperature and humidity ranges for testing voluminous items.
| Chamber type | Walk-in chamber, rigid structure |
| Standard test volumes | 2 m3, 4 m3, 8 m3, 12 m3, 16 m3 and up to 70 m3 |
| Temperature range | -70°C to +150°C |
| Extended temperature range (optional) | -80°C to +200°C |
| Relative humidity | +10% to +98% |
Indian CubeSat developer offering flight-ready 1U–6U satellite structures, subsystem components, environmental testing services, launch integration, and STEM education programs from Ahmedabad.

The 1U CubeSat Vibration Shaker Test Jig is a precision mounting fixture designed for securing 1U CubeSats during sine, random, and shock vibration tests to qualify them for launch
| Supported CubeSat Size | 1U (100 mm × 100 mm × 113.5 mm) |
| Material | CNC-machined Aluminum and Steel (vibration-resistant) |
| Mounting System | Clamping or bolted rail interface with anti-slip surface |
| Mounting System | Multiple base slots for vibration table compatibility |
| Interface Type | Compatible with slip table and vertical shaker configurations |
Vertically integrated Indian defence and aerospace electronics company designing and manufacturing avionics, microelectronics, RF/microwave, radar, test equipment and space systems.

Automated Test Equipment product line built for validating spacecraft, launch vehicle and missile subsystems.

Data Patterns develops Automated Test Equipment (ATE) for critical aerospace and space requirements, including test benches for launch vehicles, power module checkout for space pro
| Initial Product | DP-800 Multi Programmer (1994) |
| Test System Architectures | cPCI, VME, VXI |
| BMU Test System I/O | > 3000 I/O's |
| Second Launch Pad Count Down System I/O | Upto 14000 I/O |
| Strain Data Acquisition System ADC | 24 bit Sigma Delta ADC |

VXI-based redundant launch pad countdown automation system handling up to 14,000 I/O points, in operation since 2001.
Advanced testing and engineering services provider for U.S. space, defense, and government programs.

Element U.S. Space & Defense offers a comprehensive suite of dynamics testing services, including acceleration, acoustic noise, bird impact, vibration, corrosion, thermal shock
| Acceleration Test Centrifuge Diameter | 1ft (0.3m) to 62 ft (16m) |
| Acceleration Test Weight Capacity | a few grams to 7,000 lbs (3,175kg) |
| Acoustic Noise Test Reverb Chamber Volume | 5,000 cubic foot |
| Acoustic Noise Test Clean Room Size | 1,400 square foot High Bay Class 100k |
| Bird Impact Test Bird Weight Range | 2.2 to 8-pound |
Element Defense provides comprehensive EMI/EMC testing and engineering services, including radiated susceptibility, magnetic susceptibility, HIRF, lightning effects, and electrosta
| Radiated Susceptibility | up to 200V/m, 10kHz to 40GHz |
| Magnetic Susceptibility | dc to 100 kHz |
| HIRF Testing | 400 MHz to 18 GHz |
| Indirect Lightning | to 10 kV/10 kA |
| Lightning Waveforms | per SAE ARP 5416, DO-160, Airbus and Boeing specifications |

Environmental simulation testing by Element U.S. Space & Defense focuses on preparing products for their anticipated operational environments by subjecting them to simulated co

Element U.S. Space & Defense offers comprehensive hydraulics testing services for fluid power systems and components, ensuring reliability and longevity under simulated field c

Element U.S. Space & Defense offers mechanical shock testing services, including thermal shock and vibration testing, to assess device response to extreme acceleration, deceler
Element U.S. Space & Defense’s Camden, Arkansas facility is an ITAR-registered, highly responsive advanced ordnance test and evaluation facility. It supports munitions te

Element U.S. Space & Defense offers robust pneumatic testing services at its Santa Clarita, CA facility, designed for air flow, pressure, and temperature management subsystems
Developer of fluid-dynamic attitude control systems, gyroscopes, and air bearings for the space industry.

Custom-designed air bearing platforms for satellite ADCS hardware ground testing and validation.
| Type | Customized air bearing for ADCS ground testing |
| Simulation | Frictionless torque-free environment for 3-axis testing |
| Flight heritage | Used in TU Berlin Technosat ADCS testing campaign |
| Customization | Platform size, load capacity, interface — per customer requirements |

Customized air bearing platforms for ground-based attitude control system testing and ADCS validation in frictionless conditions.
| Type | Air-bearing frictionless ADCS test platform |
| Application | Ground testing of spacecraft attitude control systems |
| Configuration | Customizable to mission requirements |
| Heritage | Used by TU Berlin for TechnoSat ADCS testing |
| Manufacturer | ElmSpace (Germany) |

Customized air bearing systems for satellite ADCS testing — used in ground-test rigs such as TU Berlin's TechnoSat air bearing table.
| Application | Ground-based ADCS testing (frictionless air bearing tables) |
| Example deployment | TechnoSat air bearing, TU Berlin |
Greek space engineering company delivering advanced modeling, simulation, independent software verification, magnetic cleanliness testing, and IOD/IOV mission support. Holder of a €4M ESA Hellenic Space Dawn Mission contract.

Fixed 12-sensor fluxgate array for rapid, high-accuracy spacecraft magnetic signature characterization — full measurement in ~1 minute. Installed at ESA ESTEC since 2017.
| Sensor array | 12 Bartington Mag-13MS fluxgate magnetometers |
| Panel diameter | ~2.3 m (circular) |
| Acquisition channels | 36 |
| ADC resolution | 18 bit |
| Measurement time | ~1 minute (full signature) |

Portable carry-on magnetic cleanliness testing system — DC to 50 kHz, wireless Bluetooth, smartphone Aruco positioning, automated Multi-Dipole Modeling for field deployment.
| Frequency range | DC to 50,000 Hz |
| Portability | Fits in carry-on suitcase |
| Connectivity | Wireless Bluetooth |
| Positioning method | Smartphone camera with Aruco tag image recognition |
| Supported sensors | Sensys and Bartington fluxgates, MEDA search coils |
ETS-Lindgren designs and manufactures electromagnetic and acoustic energy components and systems, including RF shielded chambers and EMC test chambers, for industrial and commercial markets.

Compact GTEM cell for radiated emissions and immunity testing — 10,000-point emissions scan in 15 minutes or less, IEC 61000-4-20 and ANSI C63.4 compliant.
| Compliance standards | IEC 61000-4-20, ANSI C63.4 |
| Typical radiated emissions scan time | 15 minutes or less (10,000-point scan) |
| Industries | Aerospace & Defense, Automotive, Commercial |

GTEM test cell supporting optional high-voltage pulse testing (e.g., MIL-STD RS-105) — fast radiated emissions/immunity testing for aerospace and defense.
| Compliance standards | IEC 61000-4-20, ANSI C63.4 |
| Optional feature | High Voltage (HV) feed for pulse testing (MIL-STD RS-105) |
| Industries | Aerospace & Defense, Automotive, Commercial |

Compact GTEM cell especially suited to small self-contained or battery-powered device testing — 15-minute radiated emissions scans, full compliance to IEC/ANSI standards.
| Compliance standards | IEC 61000-4-20, ANSI C63.4 |
| Industries | Aerospace & Defense, Automotive, Commercial |

Next-generation reverberation chamber tuner reaching 100 RPM continuous rotation — supports both stepped and continuous stirring modes for automotive/aerospace/defense EMC testing.
| Max continuous rotation speed | 100 RPM |
| Supported modes | Stepped (tuned), Continuous (stirred) |
| Standards | ISO 11452-5, ISO 11452-11 |

Compact tabletop 2D antenna measurement system for R&D and university applications — optional 3D roll-axis stage for expanded measurement capability.
| Format | Tabletop, 2D (optional 3D roll-axis stage) |
| Industries | Academia, Wireless |

Walk-in compact antenna test range chamber with 60cm quiet zone — tests smartphones to gNodeB base stations, 3GPP/CTIA/Qualcomm-approved for FR2 bands n257-n262.
| Quiet zone diameter | 60 cm |
| DUT positioning capacity | 50 kg (110 lb) |
| Supported 5G NR bands | n257-n262 |
| Standards | 3GPP, CTIA, Qualcomm-approved (FR2) |

Extra high-performance pyramidal absorber effective from 30MHz to 100GHz — conductive carbon-impregnated urethane foam for chamber wall/floor/ceiling treatment.
| Frequency range | 30 MHz-100 GHz |
| Power handling | 1.0 W/in² |
| Substrate | Non-hygroscopic |
| Fire rating | Fire retardant |
| Optional treatment | FlexSorb (improved durability) |
French SATCOM equipment distributor and integrator; ground station hardware across L to Q band; founded 2003 in Les Ulis.

Portable and rackmount spectrum analyzers and beacon receivers for satellite signal monitoring — compact, portable, rackmount, and OEM module form factors.
| EVO-CLM (Rev B) | L-Band or 400-3000 MHz, compact form factor |
| PSA-2500 | 5 MHz - 2300 MHz, portable form factor |
| EVO-RSA (Rev B) | 70 to 6000 MHz (option), rackmount |
| LBR-2195A | L-Band, OEM form factor |
German manufacturer of reaction wheels, CubeSat picosatellite deployers, and AOCS components for small satellites, based in Berlin-Adlershof.

The ASTROFEIN ACS Test Bed is a comprehensive test stand for verifying the attitude control systems of mini and microsatellites, offering end-to-end testing capabilities including
| Rotation around vertical axis | free 360° |
| Rotation around horizontal axis | 20° – 30° |
| Magnetic field simulation | High-precision in-orbit |
| CoG calibration | Electronic |
| Sun simulation | Adjustable and movable |
Modular nanosatellite platforms and space test equipment using robotics, AI, and advanced materials.

The XO-VAC is a low-cost, desktop thermal vacuum chamber designed for CubeSats, nanosatellites, and small payloads, simulating space environmental conditions through high vacuum an
| Price | From £48,000 (base model) |
| Overall dimensions | 1260 mm x 750 mm x 600 mm |
| Working volume | 8.4L / 3U CubeSat |
| Temperature range | -25 C to 125 C |
| Thermal | radiation via shroud and/or conduction via tray |
Experior Laboratories provides independent design verification and qualification testing services for components and systems across space, aerospace, military, and other industries.
Experior Laboratories offers comprehensive testing, certification, and qualification services for components and systems across various industries, including space, satellite, and
| Vacuum level | 10⁻⁷ torr |
| Temperature range | ±150°C |
| Chamber #1 (Diversified Vacuum 3600) | 36"x54" inner volume |
| Chamber #2 (Nanovac Galaxy TVC225HSM) | 60"x72" inner volume |
| Chamber #3 | 23"x23"x23" inner working volume |

Extreme low-temperature testing down to 4K — liquid nitrogen and liquid helium cycling for simulating cryogenic fuel systems and space thermal environments.
| Minimum test temperature | 4K (-269°C) |
| Coolants | Liquid nitrogen, liquid helium |
| Safety systems | Triple-redundant overpressure relief, shutoff valve, O2 sensors |

High-intensity acoustic launch-simulation testing using the Acoustic Research Systems NEUTRON System — full satellite DFAT process in 4 days or less.
| Process time | Load-in to load-out in ≤4 days for large satellite |
| Control system | DF-ACS (m+p international) |
| Simulation integration | Dassault Systemes Wave6 vibroacoustic platform |
| Standards | Meets/exceeds NASA, SpaceX, Aerospace, Military requirements |

Classical, pyroshock, and high-G shock testing — up to 10,000+ G via Lansmont P30, proprietary KIPS pyroshock simulation system.
| Classical shock | Up to 1,500 G |
| Horizontal shock system | Up to 5,000 G on parts over 500 lb |
| SRS Shaker Shock (T2000) | Up to 5,000 G |
| Lansmont P30 shocks | >10,000 G, max velocity change 600+ in/s |
| Data capture rate | 1 MHz |
American company making the EyasSat nanosatellite simulator, an educational spacecraft kit co-developed with the US Air Force Academy covering all six satellite bus subsystems for university and workforce training.

Light weight, economical air bearing for conducting attitude control studies about a single axis. Studies include center of mass management, testing various control laws, and…
| Manufacturer | EyasSat |
Danish embedded software specialist providing satellite communications protocol stacks, waveforms and test tools for terminals, satellites and networks.
Software emulator for off-air and in-orbit validation of 5G NTN link performance
Digital-twin off-air test tools for validating satellite connectivity on UAVs and unmanned vehicles
GAUSS Instruments manufactures high-performance EMC test equipment and EMI test solutions, including real-time receivers, for various industry standards and applications.

Ultra-high-performance real-time EMI/EMC receiver and measurement system covering DC to 40 GHz with a 685 MHz instantaneous bandwidth, combining spectrum analyzer, real-time spectr
| Frequency range | DC to 40 GHz |
| Instantaneous (real-time) bandwidth | 685 MHz |
| Real-time disturbance power measurement span | up to 300 MHz |
| Quasi-peak parallel frequencies | up to 64,000 frequencies in parallel |
| Quasi-peak characterization range | up to 1 GHz |
GDP Space Systems designs and manufactures telemetry receivers, satellite modems, and range management systems for aerospace and flight test applications.

Rackmount multi-channel PCM bit synchronizer housing up to 4 bit sync channels in a 2U chassis, with built-in BERT/frame sync.
| Channels | Up to 4 per 2U chassis |
| Data rate | 10 bps to 40+ Mbps |
| Sensitivity | Down to -3 dB Eb/No at 100 mVpp |
| Modulation support | QPSK, OQPSK, SOQPSK |
| Form factor | 2U rackmount, or single/dual-channel PCI card |

The GDP Model 2267C Correlating/Diversity Combining Best Source Selector accepts up to 16 input data streams, each from digital data and clock or optional Ethernet output packets.
| Input streams | Up to 16 |
| Output groups | Up to 6 Best Source processing groups |
| Performance gain | Over 5 dB vs. single receive path |
| I/O | Direct Ethernet TMoIP, analog, or digital |
| Data compatibility | Encrypted or clear data |
Swiss opto-electronics company (part of General Atomics since 2021) developing laser-communication beam-pointing systems, optical ground stations, and free-space/fiber optical communication components.

Custom-built metrology and control systems from GA-Synopta for measuring, calibrating and characterising optical and electromechanical systems, including test beds relevant to spac
| Capabilities | Point spread function, focal length, distortion, magnification, spectral transmission meas |
| DIMM systems | Differential Image Motion Measurement for atmospheric turbulence characterization |
| Other systems | Climatic chamber control, electronic autocollimators, motor test beds, beam pointing/stabi |
Glavkosmos coordinates international human spaceflight projects, facilitates satellite launches, develops and supplies rocket components, and provides equipment for space crews.

TERRA is a space flight simulation complex that recreates the orbital environment—including Earth's magnetic field and solar radiation—for conducting experiments with satellite mod
| Year of release | 2017 |
| Guaranteed service life (years) | 1 |
| Estimated production / delivery time (months) | 3 |
| Diameter | no less than 1.2 m |
| Interface | RS-485 |

The SSCVE is a stationary control and verification equipment designed to measure and control the induction of magnetic fields generated by an EMU, proportional to the current flowi
| Year of release | 2017 |
| Guaranteed service life (years) | 3 |
| Estimated production / delivery time (months) | 6 |
| Brief history of flight qualification | Individual production. |
| Possibility to adapt the product to customer requirements | Yes |

The Active Weightlessness System is a ground-based test equipment designed to simulate weightlessness for modal testing of large transformable spacecraft systems, including reflect
| Purpose | Ground modal testing under conditions simulating weightlessness and testing of large trans |
| Year of release | 2014 |
| Guaranteed service life (years) | 3 |
| Estimated production / delivery time (months) | 12 |
| Possibility to adapt the product to customer requirements | Yes |

Rotates through 360° along one axis (vertical), the possibility of rotation in two horizontal axises is limited. Air bearing consists of a pedestal and hemisphere-form bearing. The
| Max carrying capacity, kg | 15 |
| Angle of turn relative to vertical axis | not limited |
| Angle of turn relative to horizontal axes | ±30° |

Rotates through 360° along one axis (vertical), the possibility of rotation in two horizontal axises is limited. Air bearing consists of a pedestal and hemisphere-form bearing. The
| Max carrying capacity, kg | 160 |
| Angle of turn relative to vertical axis | not limited |
| Angle of turn relative to horizontal axes | ±30° |

Rotates through 360° along one axis (vertical), the possibility of rotation in two horizontal axises is limited. Air bearing consists of a pedestal and hemisphere-form bearing. The
| Max carrying capacity, kg | 35 |
| Angle of turn relative to vertical axis | not limited |
| Angle of turn relative to horizontal axes | ±30° |

Rotates through 360° along one axis (vertical), the possibility of rotation in two horizontal axises is limited. Air bearing consists of a pedestal and hemisphere-form bearing. The
| Max carrying capacity, kg | 65 |
| Angle of turn relative to vertical axis | not limited |
| Angle of turn relative to horizontal axes | ±30° |

A ground-based test system that independently verifies the performance of a microsatellite's attitude determination and control system by optically tracking markers on a test mocku
| Purpose | Designed to verify the work of attitude determination and control system |
| Year of release | 2013 |
| Guaranteed service life (years) | _ |
| Estimated production / delivery time (months) | 5 |
| Flight qualification of the product | No |

A programmable real-time control complex for monitoring the shape and dimensional deviations of large-sized product forms (10 m and larger) using a network of compact triangulation
| Purpose | Real time control of large-sized product forms (from 10 m and more) |
| Year of release | 2007 |
| Guaranteed service life (years) | 1 |
| Estimated production / delivery time (months) | 12 |
| Possibility to adapt the product to customer requirements | Yes |

A ground-based test bench for functional testing of the orientation and stabilization (ADCS) system of 3U CubeSats, including an air bearing table, sun and magnetic field simulator
| Purpose | Designed for functional testing of CubeSat 3U orientation and stabilization system |
| Year of release | 2014 |
| Guaranteed service life (years) | _ |
| Estimated production / delivery time (months) | 6 |
| Flight qualification of the product | No |

The DHS 514 Pressure Converter is a piezoelectric transducer designed to measure acoustic pressures of non-aggressive gaseous media affecting rocket and space technology structural
| Estimated production / delivery time | 6 months |
| Flight qualification of the product | Yes |
| Range of measurements of acoustic pressure | 125-185 dB |
| Conversion coefficient | 110±15, 140±45, 155±15, 170±15 μV / Pa |
| Error | ±1.0 dB |

The DHS 517 Pressure Converter is a flight-qualified piezoelectric transducer designed to measure sound pressure of non-aggressive gaseous media on structural elements of rocket an
| Purpose | Measurement of sound pressure of non-aggressive gaseous media acting on structural element |
| Estimated production / delivery time | 6 months |
| Flight qualification of the product | Yes |
| Range of measurements of sound pressure | 125-185 dB |
| Frequency range | 3-4000 Hz |

The Dynamic Pressure Sensor Vt 206 is a strain gauge sensor designed for measuring static-dynamic pressure in liquid and gaseous aggressive and non-aggressive media, primarily for
| Purpose | Measurement of the static-dynamic pressure of liquid and gaseous aggressive and non-aggres |
| Estimated production / delivery time | 6 months |
| Flight qualification of the product | Yes |
| Possibility to adapt the product to customer requirements | Yes |
| Range of measurements | 0-1; 0-1,4; 0-2; 0-2,8; 0-4; 0-5,6; 0-8; 0-11; 0-16; 0-22; 0-30; 0-40; 0-60 Mpa |

Ground-based measurement equipment for determining the center-of-mass position and axial moments of inertia of nanosatellites up to 10 kg.
| Inaccuracy of the center-of-mass position determining | not more then 1 mm |
| Accuracy of axial moments of inertia determination | not less then 1.5% |
| Year of release | 2017 |
| Guaranteed service life (years) | 3 years |
| Estimated production / delivery time (months) | 12 |

The Force Sensor Vt 114 is a strain gage sensor designed for measuring compressive, tensile, and alternating forces in structures of space rocket and aviation equipment. It works i
| Estimated production / delivery time | 6 months |
| Flight qualification of the product | Yes |
| Range of measurements | ±130 kN |
| The basic error,%, not more | 1 |
| Rated output signal | 1,5+0,22-0,15 mV / V |

The Magnetic Field Simulator is a Helmholtz cage system designed to simulate the Earth's magnetic field along a satellite's orbital trajectory for testing purposes.
| Purpose | Designed for magnetic field simulation along the orbital trajectory of a satellite. |
| Year of release | 2009 |
| Guaranteed service life (years) | _ |
| Estimated production / delivery time (months) | 5 |
| Flight qualification of the product | No |

A highly sensitive magnetic mass-spectrometer leak detector used to test the leaktightness of systems and facilities by detecting and localising helium tracer gas leaks.
| Year of release | 2011 |
| Guaranteed service life (years) | 10 |
| Estimated production / delivery time (months) | 3 |
| Flight qualification of the product | No |
| Possibility to adapt the product to customer requirements | Yes |

The T-406Н КС tester is a compact portable device for checking the technical characteristics of signals emitted by radio beacons and verifying the validity of encoded data during s
| Purpose | T-406N KS tester is intended to control technical characteristics of the signals emitted b |
| Year of release | 2012 |
| Estimated production / delivery time (months) | 6 |
| Flight qualification of the product | No |
| Possibility to adapt the product to customer requirements | Yes |

A debug board designed to facilitate the testing and debugging of any onboard system or a full nanosatellite, featuring multiple debugger interfaces and onboard system emulation.
| Purpose | Board designed to allow debugging of any onboard system or full nanosatellite. |
| Year of release | 2016 |
| Guaranteed service life | 1 year |
| Estimated production / delivery time | 6 months |
| Flight qualification of the product | No |

The LH 604 is a piezoelectric sensor designed to measure pressure pulsations in liquid and gaseous media within rocket and space technology power plants, working with a charge or v
| Estimated production / delivery time | 6 months |
| Flight qualification of the product | Yes |
| Range of measurements of pressure pulsations | 0,05-5,0 Mpa |
| The range of exposure to static pressures | 3,0-60 Mpa |
| Conversion coefficient | (40±25)⋅10-5 mV / Pa |

The LH 608 is a piezoelectric pressure pulsation sensor designed for measuring pressure pulsations in liquid and gaseous media in rocket and space technology power plants, working
| Range of measurements of pressure pulsations, Mpa | 0,05-5,0 |
| The range of exposure to static pressures, Mpa | 3,0-60 |
| Conversion coefficient, mV / Pa | (40±25)⋅10-5 |
| Error,% | ±10 |
| Weight, kg | 0.19 |

A ground test platform designed to hold and balance a 3U CubeSat with ADCS for testing on an air-bearing test bench.
| Purpose | Designed for CubeSat 3U satellite with ADCS installation to test on air-bearing |
| Year of release | 2014 |
| Guaranteed service life (years) | _ |
| Estimated production / delivery time (months) | 5 |
| Flight qualification of the product | No |

A ground test platform for mounting "TabletSat" small-satellite devices to test them on an air-bearing test bench.
| Purpose | Designed for "TabletSat" satellite devices installation to test on air-bearing |
| Year of release | 2009 |
| Guaranteed service life (years) | _ |
| Estimated production / delivery time (months) | 5 |
| Flight qualification of the product | No |

A ground test platform designed for installing the TabletSat satellite for testing on an air-bearing test bench.
| Purpose | Designed for "TabletSat" satellite installation to test on air-bearing |
| Year of release | 2013 |
| Guaranteed service life (years) | _ |
| Estimated production / delivery time (months) | 5 |
| Flight qualification of the product | No |

The VT-718 is a primary linear displacement transducer designed for measuring linear displacements of objects in rocket and space technology control systems, featuring high reliabi
| Purpose | Measurement of linear displacements of objects in rocket and space technology product cont |
| Estimated production / delivery time | 6 months |
| Flight qualification of the product | Yes |
| Possibility to adapt the product to customer requirements | Yes |
| Range of measurements | 0-16; 0-22; 0-30; 0-45; 0-60; 0-90; 0-125; 0-180;0-250; 0-350; 0-500;0-700; 0-750 mm |

The 612M is a flight-qualified, high-temperature piezoelectric sensor designed for measuring rapidly varying pressures in liquid and gaseous aggressive and non-aggressive media wit
| Estimated production / delivery time | 6 months |
| Flight qualification of the product | Yes |
| Range of measurements of rapidly varying pressures | 0,045-5,6 Mpa |
| Range of influence of slowly varying pressures | 2,8-63 Mpa |
| Sensitivity, not less | 16⋅10-5 mV / Pa |

A set of fixing devices designed to secure a nanosatellite on the desktop of equipment used for measuring its center-of-mass position and inertia characteristics.
| Purpose | Designed for fixing of the nanosatellite at the desktop of the equipment for measurement t |
| Flight qualification of the product | No |
| Possibility to adapt the product to customer requirements | Yes |

The Solar Panel Check Stand is a ground support equipment designed for weight relief and opening-out testing of small-size solar panels for space applications.
| Purpose | Provides weight relief and opening-out testing of small-size Product solar panels. |
| Year of release | 2014 |
| Guaranteed service life | 15 years |
| Estimated production / delivery time | 9 months |
| Flight qualification of the product | No |

An automated ground-based system that simulates weightlessness for testing large-sized spacecraft elements such as solar panels.
| Purpose | Designed for ground testing (weightlessness) of spacecraft equipment, solar panels |
| Year of release | 2016 |
| Guaranteed service life (years) | 10 |
| Estimated production / delivery time (months) | 12 |
| Possibility to adapt the product to customer requirements | Yes |

A ground-based test device that displays simulated star field imagery on a screen to test star trackers alongside other ADCS components.
| Purpose | Designed for star trackers testing together with other ADCS components |
| Year of release | 2017 |
| Guaranteed service life (years) | _ |
| Estimated production / delivery time (months) | 9 |
| Flight qualification of the product | No |

A halogen-lamp based sun simulator designed for ground testing of spacecraft ADCS Sun orientation capability.
| Purpose | Designed for testing of ADCS Sun orientation capability |
| Year of release | 2009 |
| Guaranteed service life (years) | _ |
| Estimated production / delivery time (months) | 1 |
| Flight qualification of the product | No |

The Synthesis System of IR Images is a test equipment designed to generate dynamic infrared images for evaluating photodetectors, utilizing independent object and background illumi
| Purpose | Designed to create dynamic infrared images of arbitrary topology in the plane of the locat |
| Year of release | 2018 |
| Guaranteed service life (years) | 10 |
| Estimated production / delivery time (months) | 12 |
| Flight qualification of the product | No |

A ground-based monitoring system that provides wide-angle and close-up video surveillance plus sensor-based tracking of oxygen, propellant, temperature and humidity levels during s
| Year of release | 2014 |
| Guaranteed service life | 5 years |
| Estimated production / delivery time | 18 months |
| Flight qualification of the product | No |
| Possibility to adapt the product to customer requirements | Yes |

An aerodynamic (air-bearing) test table that lets scale mock-ups of spacecraft move freely in the horizontal plane with minimal friction, enabling study of their mutual/relative mo
| Dimensions, mm | 5000kh6000kh3000 |
| Active area size | 1860kh2480 |
| Disk (w/ control system electronics) carrying capacity, kg, up to | 10 |
| Gap between disk and table, mm, up to | 0.5 |
| Working medium | air |

A ground-based magnetic test stand for validating CubeSat attitude determination and control algorithms and for training students.
| Purpose | Conducting testing of control algorithms. Training of students and stuff. |
| Year of release | 2017 |
| Guaranteed service life (years) | 1 year |
| Estimated production / delivery time (months) | 4 |
| Flight qualification of the product | No |

A six-degree-of-freedom precision positioning mechanism (hexapod) used as a component of a testbed for examining the radio-technical performance of antennas under ground conditions
| Purpose | High precision transfer and rotation of the target object in the 3 linear and 3 angle dire |
| Year of release | 2012 |
| Guaranteed service life (years) | 10 |
| Estimated production / delivery time (months) | 4 |
| Flight qualification of the product | No |

The Thermoelectric Converter DT 27 is a flight-qualified sensor designed for temperature measurement of aggressive (liquid oxygen) and non-aggressive liquids and gases in rocket an
| Purpose | Temperature measurement of aggressive (liquid oxygen) and non-aggressive liquids and gases |
| Estimated production / delivery time | 6 months |
| Flight qualification of the product | Yes |
| Range of measurements | -196/+600 °C |
| Limits of permissible deviations of TEDS from NSKHK (L), ° S, (for tolerance classes 2, 3 according to GOST R 8.585-2000) in the temperature measurement range: 1. -196 / -100 °C; 2. St. -100 / + 100 °C; 3. -40 / + 360 °C; 4. St. + 360 / + 600 °C | 1. ±(1,5+0,01 |t|); 2. ±2,5; 3. ±2,5; 4. ±(0,7+0,005 |t|) |

An automated weightlessness (zero-gravity offloading) suspension system used for ground testing of spacecraft equipment and transformable/deployable reflectors.
| Year of release | 2016 |
| Guaranteed service life (years) | 10 |
| Estimated production / delivery time (months) | 12 |
| Possibility to adapt the product to customer requirements | Yes |
| Number of suspension points weightless elements | 36 pcs |

Weight-measuring platform devices designed for static weighing of transport fuelling containers and for weighing liquid fuel and fuel charges.
| Purpose | Weighing of transport fuelling containers in the static weighing mode; weighing of liquid |
| Year of release | 2015 |
| Guaranteed service life (years) | 3 |
| Estimated production / delivery time (months) | 8 |
| Flight qualification of the product | No |
System integrator and manufacturer of CubeSat structures, buses, and MyPOD test/transport pods, with space environment test equipment services.

The 12U MyPOD2 is a versatile tool for CubeSat qualification, testing, fit-checks, storage, and transportation, supporting various CubeSat configurations.
| Temperature range | -50°C to +100°C |
| External Size (L x W x H) | 268 x 266 x 442.1 mm |
| Rail Size (L x W x H) | 227 x 227 mm |
| CubeSat Size (L x W x H) | 226.3 x 226.3 x 366.0 mm |
| Empty Mass | 15 kg |

A 3U CubeSat test pod used for qualification, acceptance testing, dimensional fit-check, storage, and transportation of 1U to 3U CubeSats.
| Temperature range | -50°C to +100°C |
| External Size (L x W x H) | 144 x 148.1 x 470 mm |
| Rail Size (L x W x H) | 100.8 x 100.8 mm |
| CubeSat Size (L x W x H) | 100 x 100 x 340.5 mm |
| Empty Mass | 7.9 kg |

The 3U MyPOD2 is a versatile tool for qualification, acceptance testing, dimensional fit-check, and storage and transportation of CubeSats, supporting various 1U, 1.5U, 2U, and 3U
| Temperature range | -50°C to +100°C |
| External Size (L x W x H) | 137 x 137 x 415 mm |
| Rail Size (L x W x H) | 100.8 x 100.8 mm |
| CubeSat Size (L x W x H) | 100 x 100 x 340.5 mm |
| Empty Mass | 4.8 kg |
India-based space EdTech platform offering CubeSat and CanSat educational kits, high-altitude balloon hardware, and online space science courses for students worldwide.

All-in-one CanSat educational kit simulating a real satellite mission with LoRa telemetry and live web dashboard.
| Sensors | Temperature, humidity, barometric pressure, altitude, GPS, acceleration, gyroscope |
| Communication | LoRa 433 MHz module, long-range |
| Dashboard | Web-based live UI: GPS position, altitude, pressure, acceleration, orientation |
| Payload Capacity | Up to 1 kg |
| Compatibility | Parachute-compatible for recovery |

Educational 1U CubeSat build kit with 20+ sensors, 433 MHz RF comms, GPS, and live AI-powered web dashboard.
| Dimensions | 10 × 10 × 10 cm (1U) |
| Weight | 300 g |
| Sensors | 20+ types: humidity, temperature, barometric pressure, altitude, gyroscope, accelerometer, |
| Communication | 433 MHz RF module |
| Range | 100 m – 1 km |

Weather balloon reaching ~24,000 m altitude for radiosondes and light scientific payloads.
| Mass | 300 g |
| Max Altitude | ~24,000 m |
| Suitable Payloads | Radiosondes, light instruments, amateur radio |
| Not Recommended For | Heavy camera payloads |
Indian small satellite manufacturer offering flight-proven platforms, subsystems, and mission-as-a-service solutions.

Ground-based hardware-in-the-loop test rig for validating satellite payloads and subsystems before flight — 6 PC-104 slots, ground-station simulator included.
| PC-104 slots | 6 (CDH, EPS, COMMs, Interface Card, 2 spares) |
| Bus-probing connectors | 2 |
| Antenna pass-throughs | 2x SMA-SMA with 30dB attenuator (VHF/UHF) |
| Battery boards | 1 (4x battery holder), extendable to 2 |
SPACE COTAN Co., Ltd. is a Japanese company developing and operating the Hokkaido Spaceport at Taiki-cho (Taiki Town) in Hokkaido, Japan's northernmost main island, as a commercial launch site for small orbital rockets and sounding rockets.

Dedicated rocket engine firing test facility at Launch Complex 0 in Taiki, Hokkaido, supporting propulsion development and qualification for orbital and suborbital launch vehicles.
| Location | Launch Complex 0 (LC0), Bisei, Taiki-cho, Hiroo-gun, Hokkaido, Japan |
| Facility type | Static fire / rocket engine firing test |
| Propellants available | LNG (CH4), LOX, GHe, LN2, GN2, GOX, Water, Electrical Power |
| Known users | Interstellar Technologies Inc., Innovative Space Carrier Inc. |
| Applications | Engine development, qualification, hot-fire testing for orbital and suborbital vehicles |
South Africa-based space hardware company developing the Lumen thermal vacuum testing system and providing TVAC test services for the aerospace industry.
Space-environment qualification TVAC testing service from Cape Town — high vacuum + thermal cycling for small satellite components and subsystems, operated by Hypernova Space Techn
| Facility location | Cape Town, South Africa |
| Service type | Thermal vacuum testing as a service |
| Test environment | High vacuum + thermal cycling |
| Target hardware | Small satellite components, subsystems, CubeSat-class assemblies |
| In-house heritage | Qualified Hypernova vacuum arc thruster hardware (Transporter-6, Jan 2023) |
German technology company providing testing, simulation, and engineering services for aerospace, defense, and space systems.

Europe's foremost independent space test centre — thermal-vacuum, vibration, acoustic, EMC, optical, and structural qualification for satellites and spacecraft, operating at IABG O
| Thermal vacuum chamber (Phenix, ESTEC/ETS) | 4 m diameter × 10 m length, <10⁻⁵ mbar |
| Acoustic test facility max SPL | 156 dB |
| Vibration table mass capacity (Hydra, ESTEC) | 20 tonnes |
| Vibration actuators (Hydra) | 8 × 680 kN hydraulic, 6 DOF |
| Test types | Thermal-vacuum, solar simulation, vibration, shock, acoustic, EMC, modal analysis, optical |
CubeSat deployers, antennas, EPS and small-satellite systems.

This cost-effective Training Platform can support hands-on training and education for small satellite design and engineering, perfect to kickstart your small satellite program.…
| Manufacturer | ISISPACE |
Jena-Optronik designs and manufactures sensors, space optics, and electronics for satellites and spacecraft, supporting communication, navigation, and Earth observation.

Advanced dynamic closed-loop star sensor test system: projects real sky scenery (stars, planets, SEUs) on micro-display through collimating optics, >20deg FOV, up to 3deg/s moti
| Function | Dynamic closed-loop end-to-end star sensor testing |
| FOV | >20 deg circular |
| Simulated Objects | Stars (2.0-6.5 mi), solar system bodies, protons (>5000/image), extended objects |
| Single Star Accuracy | <0.0075 deg (3-sigma) |
| Star Diameter | <0.1 deg (99%) |

Compact, cost-efficient Ground Support Equipment for static star pattern simulation and functional testing of ASTRO APS and ASTRO CL star trackers. Available in ambient and TVAC va
| Function | Static star pattern simulation (open-loop) |
| Compatibility | ASTRO APS (plug & play); ASTRO CL (extended version) |
| Variants | OSPS-Standard (ambient), OSPS-TV (TVAC), OSPS-PEEK (reduced shielding) |
| Operating Temperature | +10 to +30 deg C (Standard/PEEK); TVAC range for -TV variant |
| ASTRO CL capability | Alignment and measurement during satellite integration |
KRYTAR designs and manufactures ultra-broadband microwave, mmWave, and RF components and test equipment for commercial and military applications, covering DC to 110 GHz.

Rugged mechanical-design coaxial terminations rated for space use — models spanning DC to 40 GHz, low VSWR, 3.5mm connectors.
| Model T1M-SQ | DC-20.0 GHz, 1.05 max VSWR, 3.5mm male |
| Model T2M-SQ | To 26.5 GHz |
| Model T3M-SQ | To 40.0 GHz |

The KRYTAR 203 Series Zero Bias Schottky Detectors are inline coaxial barrel connector packages designed for high-performance microwave instrumentation and systems, offering broad
| Minimum Frequency | 10 MHz |
| Maximum Frequency | 40 GHz |
| Frequency Response | ±0.5 dB to 20 GHz |
| Frequency Response | ±0.8 dB to 26.5 GHz |
| Frequency Response | ±1.5 dB to 40 GHz |
LabSat, a brand of Racelogic, provides compact GNSS record and replay simulators enabling reliable, repeatable testing of GNSS-enabled devices across automotive, aerospace, and industrial applications.

Compact, portable multi-constellation GNSS record-and-replay simulator for testing and developing products with satellite navigation chipsets.
| Constellations | GPS/Galileo/SBAS/QZSS, GLONASS, or BeiDou |
| Output Signal Level | Adjustable -73 dBm to -103 dBm |
| RF Channels | 1, 2 or 3 (model dependent*) |
| RF Constellation Centre Frequencies | 1575.420 MHz (GPS L1, Galileo E1, SBAS and QZSS); 1602.00 MHz (GLONASS L1); 1561.098 MHz ( |
| Number of Satellites Observed | All in view |

The LabSat 3 Wideband is a multi-constellation and multi-frequency GNSS record and replay system designed for testing GNSS devices in various applications, including aerospace and
| Constellations | GPS L1, L2, L5; Galileo E1, E5a/b, E6; GLONASS G1, G2, G3; BeiDou B1, B2a/b, B3; QZSS L1, |
| Nominal Output Signal Level | -93dBm/MHz @ 0dB, variable attenuator provides between +20 dB and –69 dB of adjustment dur |
| RF Channels | 3 |
| RF Channel Centre Frequencies | Selectable |
| Number of Satellites Observed | All in view |

The LabSat 4 is a compact, portable, and cost-efficient GNSS Record & Replay simulator offering multi-constellation and multi-frequency capabilities with up to 12-bit quantisat
| Constellations | GPS L1, L2, L5; Galileo E1, E5a/b, E6; GLONASS G1, G2, G3; BeiDou B1, B2a/b, B3; QZSS L1, |
| Nominal Output Signal Level | -73dBm/MHz @ 0dB Variable attenuator provides between +20 dB and –69 dB of adjustment duri |
| RF Channels | 3 |
| RF Channel Centre Frequencies | Selectable |
| Number of Satellites Observed | All in view |
Dutch developer of SmallSat and CubeSat separation systems providing smart, lightweight, cost-effective satellite deployers for launch mission management.

Fully assembled CubeSat test fixture (TPOD-L) from Launch42, supporting 12U/16U CubeSats for integration and pre-launch test campaigns.
| Size | TPOD-L |
| Supported CubeSat Size | 12U / 16U |
| Lead time | 4 weeks |
| Price | €15,800 |

Fully assembled CubeSat test fixture (TPOD-M) from Launch42, supporting 6U/8U CubeSats for integration and pre-launch test campaigns.
| Size | TPOD-M |
| Supported CubeSat Size | 6U / 8U |
| Lead time | 4 weeks |
| Price | €11,500 |
Dutch manufacturer of precision optical components and sun sensors for space missions, with flight heritage on ESA programs including LISA.

The Single Sampler is a universal analogue Sunsensor interface box that can be used to readout four (photo) currents simultaneously as well as a 10kOhm nominal thermistor. As such…
| Manufacturer | Lens R&D |
Madrid-based aerospace engineering company specialising in opto-mechanical systems, flexible thermal straps, and cryogenic units for space missions.

Custom-built research-grade cryostats offering precise cryogenic temperature control, compatible with liquid helium or liquid nitrogen, for space-technology research.
| Operating temperature | In-house test asset: 20 to 300 K |
| Interface | Optical windows (in-house asset: 2 windows); compatible with liquid helium or liquid nitro |
| Dimensions | In-house test asset volume: 300 x 300 mm |

Custom-designed thermal vacuum chambers reproducing space environmental conditions (extreme temperature and high vacuum) for qualification testing of space hardware.
| Interface | Custom-configured size, temperature range, vacuum level, and optical window options per pr |
| Operating temperature | Configurable extreme-temperature range (project-specific) |
| Interface | ISO 5 / ISO 7 clean rooms compliant with ISO 14644 for integration |
| Interface | In-house test types: sine/random vibration, shock, TVAC, TVTB |
Total liquid immersion cooling technology for servers and electronics, using patented Directed-Flow cooling in standard 19-inch racks for data center, edge, and rugged industrial applications.

The LCS MiniNODE is a compact, fully sealed (IP67) industrial computer built on the Thin Mini-ITX standard, cooled entirely by roughly one gallon of non-hazardous, eco-friendly die
| Ingress protection | IP67 |
| CPU | AMD Ryzen Embedded R2000/5000-series, up to 6-core/12-thread, 4.4 GHz |
| Memory | up to 64 GB DDR4 |
| Storage | NVMe M.2 SSD |
| Power | 180 W external supply |

Self-contained, plug-and-play 24U mobile server room housing 4-6 ZPServers for rapid edge deployment.
| Power range | 1.1 - 8 kW |
| Storage | up to 16 TB |
| Cooling PUE | < 1.04 |
| Noise level | < 55 dBA |
| Rack size | 24U |

Immersion-cooled 2U rack server delivering up to 4kW per rack unit for data centers and AI workloads.
| Cooling capacity | up to 4 kW per 2U |
| Dimensions | 18 x 33 x 3.5 in (2U) |
| Fluid volume | ~5 gallons per 2U |
| Wet weight | ~75 lb per 2U |
| Cooling PUE | < 1.03 |
Redwire is an integrated aerospace and defense company providing advanced technologies, space infrastructure, and autonomous systems for government agencies and defense programs.

The LoadPath 3U CubeSat Mass Simulator is designed to simulate the mass and center of mass of a 3U CubeSat for ground fit checks, testing, and integration studies.
| Design simulates | mass and center of mass of a 3U CubeSat |
| Mass range | 3-5 kg |
| Suitability | ground fit checks, ground testing and integration studies |
| Nominal structural material | Delrin polymer |
| Material properties | low-outgassing materials acceptable in flight |

The LoadPath 6U CubeSat Mass Simulator is designed to simulate the mass and center of mass of a 6U CubeSat for ground testing, integration studies, and fit checks.
| Design simulates | mass and center of mass of a 6U CubeSat |
| Mass range | 6-10 kg |
| Suitability | ground fit checks, ground testing and integration studies |
| Nominal structural material | Delrin polymer |
| Material properties | constructed of low-outgassing materials acceptable in flight |
Lunar Research Service (LRS) is a Ukrainian space technology company specializing in hardware and materials testing for space applications, nanosatellite development, and extreme-environment testing.

Structural dynamics testing service from Lunar Research Service (LRS) for qualifying hardware intended for extreme, space-relevant environments.

Lunar Research Service offers structural dynamics testing of hardware for extreme environments, covering vibration, shock, and acoustic qualification relevant to space missions.
| Test capabilities | Vibration testing, vibroacoustics, modal characteristics testing, sound transmission loss |

Lunar Research Service (LRS) is a Ukrainian NewSpace company offering satellite mission services, near-space/stratospheric and orbital launch campaigns, and environmental hardware

Lunar Research Service (LRS) provides structural and environmental testing for hardware destined for extreme environments, alongside satellite mission design, in-house deployment s
| Flight heritage | LRS 3U satellite launch agreement with Rocket Factory Augsburg AG (RFA), planned for Decem |
Lúnasa is a London-based space technology company building navigation, autonomy, and rendezvous and proximity operations (RPO) systems for the in-orbit servicing and manufacturing (ISAM) market.

The Lúnasa Robotic Testbed is an advanced ground-based simulation environment for testing and validating vision-based Guidance, Navigation, and Control (GNC) systems for satellite
| Arm Payload capacity | Upto 30 kg |
| Degrees of Freedom | 6 DoF arms + extra DoF from the axis |
| Accuracy | 0.05 mm |
| Length of testbed | 7 m |
| Arm reach | Up to 1.3 m |
Magson GmbH is a Berlin-based manufacturer of high-performance digital fluxgate magnetometers for terrestrial and space applications, including spacecraft attitude control systems.

Linux-based multi-channel data logger for fast low-voltage and E-field measurements, including seafloor deployments.
| Channels | 3 channels |
| Sample rate | Up to 10 kHz |
| Measurement type | Fast E-field / low-voltage measurements |
| Time synchronization | Optional atomic clock for multi-unit sync without cabling |
| Operating system | Linux-based |

Dual-sensor fluxgate gradiometer for detecting small-scale magnetic field anomalies and spacecraft magnetic moment testing.
| Sensor configuration | Two independent fluxgate sensors in spatial gradient arrangement |
| Measurement type | Magnetic field gradient / anomaly detection |
| Primary use | Spacecraft magnetic moment determination, magnetic cleanliness testing |
| Known users | ESTEC (ESA), Thales Alenia Space |
| Base sensor noise | < 15 pT/sqrt(Hz) @ 1 Hz (per Magson fluxgate sensor design) |

Configurable industrial-grade tri-axial fluxgate magnetometer for terrestrial geophysical and field survey applications.
| Sensor type | Tri-axial fluxgate, single or dual sensor configuration |
| Noise level | < 15 pT/sqrt(Hz) @ 1 Hz |
| Long-term stability | Offset drift < 3 nT/year |
| Data storage | Optional integrated flash memory for stand-alone operation |
| Optional sensors | Tilt meter, angular encoder, external GPS receiver |
Chinese commercial satellite manufacturer building Earth observation, communications, and remote sensing satellites, plus payloads, components, and ground terminal systems.

The Changchun Optical Payload Manufacturing AIT Center specializes in the design, development, testing, and validation of large-aperture optical remote sensing satellite payloads,
| Integrating Sphere Diameter | 3-meter |
| Three-axis Toolmaker's Microscope Standard | JS B7153 |

The MinoSpace Advanced Equipment Manufacturing Laboratory is a comprehensive facility in Beijing for commercial satellite testing and development, integrating testing, experimentat
| Total area | nearly 5,000 square meters |
| Vibration table capacity | up to 1000 kg |
| EMC chamber dimensions | 14m (L) x 12m (W) x 10m (H) |
| Thermal vacuum chamber effective temperature range | ±200°C |
| Thermal vacuum chamber effective test diameter | 3.6 meters |
UK national measurement institute providing precision timing, frequency standards, and calibration services critical for satellite navigation and space systems.

UK National Physical Laboratory provides precision metrology and calibration services for satellite instrument validation and Earth observation calibration.
| Services | Precision metrology, sensor calibration |
| Applications | Satellite instrument validation, EO calibration |
| Country | United Kingdom |
Nautilus Navigation in Space designs autonomous Guidance, Navigation, and Control (GNC) sub-systems, provides Flight Dynamics as a Service, and develops ground testing equipment for space missions.

Ground testing equipment for CubeSat ADCS closed-loop testing.
| Supported platforms | 1U to 12U CubeSats |
| Test mode | Closed-loop ADCS testing |
Polish smallsat hardware company designing and manufacturing components and subsystems for CubeSats and small satellites, serving commercial and institutional space customers across Europe.

Space environmental qualification testing for CubeSats and components — thermal vacuum (TVAC), vibration, shock, and EMC/EMI testing services with reporting.
| Test types | TVAC, vibration, shock, EMC/EMI |
| Facility | In-house test equipment |
| Output | Full test reports for mission assurance |
| Customers | Other satellite developers and component suppliers |
NOFFZ Technologies is a German manufacturer of universal test and automation systems, including RF test platforms and GNSS signal simulators for aerospace, defense, and automotive applications.

Fully automated, multi-station rotary/indexing end-of-line test system for high-volume electronics production.
| Handling | Automatic rotary/indexing table through multiple test/inspection stations |
| DUT capacity | Dual-DUT or multi-nest configurations |
| Optional modules | Optical pin/connector inspection, label printing and application, automated sorting |
| Instrumentation | Modular UTP instrumentation for various signal types and power requirements |
| Software | UTP Software Suite (sequencing, variant management, data logging, traceability, MES/IT con |

Quad-DUT board-level RF functional tester with shielded RF chamber and interchangeable adapters for connected-car components.
| DUT capacity | Up to 4 DUTs tested in parallel |
| RF chamber attenuation | Up to 60 dB |
| Adapters | Interchangeable adapters for different DUT variants |
| Instrumentation | Integrable Universal Wireless Tester (UWT) or third-party RF instrumentation |
| Signal conditioning | Integrable Signal Conditioning Unit (SCU) |

Compact Antenna Test Range (CATR) radar test system for calibrating large 4D and imaging radar sensors in a small footprint.
| Test technology | CATR (Compact Antenna Test Range) with integrated parabolic reflector |
| Footprint | < 3.5 m2 base area |
| Frequency range (target simulator) | 75 GHz - 82 GHz |
| Bandwidth | Up to 5 GHz |
| Target simulation | One or multiple targets |

Compact low-channel-count RF functional and end-of-line test system for automotive and IoT modules.
| Test type | RF functional test, end-of-line / board-level (FKT/EOL) |
| DUT capacity | Single DUT (Single Device Under Test) |
| Typical DUTs | eCall modules, NAD modules, connected gateways, TCUs, IAMs |
| RF chamber | Integrated NOFFZ RF chamber UTP 5070 |
| Automation | Manual or robot-operated adapter |

Scalable dual/multi-DUT RF functional test system with shielded RF chambers for infotainment and connected-car modules.
| Test type | Parallel RF functional test, EOL |
| DUT capacity | Two or more DUTs in parallel |
| Signal types tested | 5G, BT, WLAN, V2X, BroadR-Reach, CAN, A2B audio |
| RF chamber | UTP 5070, up to 60 dB RF attenuation, for over-the-air (OTA) test |
| Voltage/current range | Up to 1 kV / up to 1 kA |

Highly parallel, scalable UTP test system for long-term functional testing, environmental screening, and burn-in of electronic assemblies.
| Test type | Multi-DUT burn-in, screening, long-term functional test |
| Environmental range | Approx. -40 degC to +85 degC in climate chamber |
| Parallelization | Multiple DUTs tested simultaneously (example configs up to 8 DUTs parallel) |
| Software | UTP Software Suite (sequencing, variant management, data logging, MES/IT connectivity) |
| Example configuration | Two drawers with 28 modules, flexible interfaces, RF tests, PXI-based automation |

Compact near-field radar sensor test system with low-reflection absorber chamber for automotive radar validation and end-of-line test.
| Test type | Direct near-field radar sensor test |
| Frequency range (target simulator) | 75 GHz - 82 GHz |
| Bandwidth | Up to 5 GHz |
| Target simulation | One or multiple targets |
| Motion axes | 2 axes (azimuth and elevation), optional goniometer or robot |

The Universal Wireless Tester (UWT), jointly developed by NOFFZ and National Instruments (NI), is a flexible, cost-effective non-signaling RF test platform addressing the growing n
| Standards supported | 5G NR, LTE, WCDMA, GSM, V2X, 802.11 a/b/g/n/ac/ax/p, BT, BLE, UWB |
| Platform | NI PXI-based, open and software-centric |
| RF switch | NOFFZ UMX universal RF switch, 32 bidirectional DUT ports, integrated signal conditioning |
| Scalability | Up to 128 RF channels using up to four NI vector signal transceivers and four UMXs |
| Additional capability | Waveform generation for GNSS and broadcast radio |
Italian electric propulsion startup developing water-propelled resistojet thruster systems for nanosatellites and microsatellites, offering a safe, low-cost, and high-performance propulsion solution.

Specialized vacuum chamber testing service available to external customers, achieving pressures down to 1×10⁻⁶ mbar for space component qualification and thruster characterization.
| Minimum pressure | 1×10⁻⁶ mbar |
| Facility type | High vacuum chamber |
| Use cases | Thruster testing, component qualification, outgassing, functional vacuum testing |
US defense and technology prime contractor providing space systems engineering, missile defense integration, space domain awareness, and ground system development for US government programs.

DYSE® is an RF channel emulator that simulates realistic RF environments, including congested and contested conditions, for testing and evaluation of RF systems.
| Tuning range | up to 20 GHz |
| IBW | >1 GHz |
| Path delay | >1 sec |
| RF paths | Up to 1024 |
| Interconnection | Full-mesh |
San Francisco-based manufacturer of flight-proven CubeSat kits, SUPERNOVA nanosatellite buses, and spacecraft power/electronics components, with over 150 kits delivered and dozens of successful space missions since 2003.

A CubeSat Kit test module that simulates one Remove-Before-Flight switch and up to three separation switches, electrically compatible with common CubeSat EPS designs.
| Simulated RBF switches | 1 |
| Simulated Separation switches | Up to 3 |
| Switch logic combination | AND / OR via user-settable jumpers |
| Bus compatibility | 104-pin CubeSat Kit Bus standard |
| Includes | One fully assembled Flight Switch Simulator Module |

A programming/debug adapter cable that connects a Silicon Labs USB Debug Adapter to a Pluggable Processor Module (PPM) B1 in a CubeSat Kit.
| SKU | 710-00488 |
| Connector A | 2x5 0.100" pitch header (10-pin JTAG, mates with Silicon Labs USB Debug Adapter) |
| Connector B | 8-pin flat printed circuit cable (FPC) |
| Hardware Class | Development Hardware |
| Used With | Pluggable Processor Module (PPM) B1 / Silicon Labs USB Debug Adapter |

A programming/debug adapter cable that connects a TI MSP430 Flash Emulation Tool (FET) to a Pluggable Processor Module (PPM) A1/A2/A3 in a CubeSat Kit.
| SKU | 634-00334 |
| Connector A | 2x7 0.100" pitch header (14-pin JTAG, mates with TI MSP430 FET) |
| Connector B | 8-pin flat printed circuit cable (FPC) |
| Hardware Class | Development Hardware |
| Used With | Pluggable Processor Module (PPM) A1 / A2 / A3 |

A programming/debug adapter used to connect a Microchip In-Circuit Debugger (ICD 3) or PICkit programmer to a CubeSat Kit Pluggable Processor Module (PPM D1/D2/E1).
| SKU | 710-00540 |
| Price | $50.00 per item |
| Hardware classification | Development Hardware |
| Connector 1 | 6-pin RJ-11 jack (for ICD 3 phone-style cable) |
| Connector 2 | 6-pin flat printed circuit (FPC) cable |

A CubeSat Kit Accessories module (Load Board A) sold by Pumpkin for use during CubeSat integration and test.
| SKU | 711-00651 |
| Price | $255.00 |
| Category (site breadcrumb) | CubeSat Kit Accessories |
| CAD/Datasheet file name (no link provided) | Load Board A |

A CubeSat Kit accessory module that exposes VBATT, +5V_SYS and VCC_SYS power buses on banana jacks and connectors for drawing or injecting test power.
| VCC_SYS | +3.3V |
| +5V_SYS | +5.0V |
| VBATT | 8-28V depending on application |
| Connectors | Banana jacks (x3 pairs); two 8-pin Harwin M80 connectors (J391, J390) |
| Configurable resistors | R1 (routes H2 pins 39/40 to J390), R2 (routes H2 pins 51/52 to J390) -- one fitted at fact |

A low-cost, portable 2U rackmount satellite simulator hosting a SUPERNOVA-based satellite simulator electronics stack running a stripped-down version of Pumpkin's flight-proven GUT
| Form factor | 2U rackmount unit |
| Flight software | Stripped-down version of Pumpkin's flight-proven GUTS FSW, option /O1 included at no charg |
| Expansion | Up to three additional compatible 104-pin modules with I2C, SPI, RS232 or GPIO interfaces |
| Optional power supply | 150 W power supply option to stand in for an EPSM1 |
| Optional GNSS receiver | Available as additional-cost option |

A USB-based JTAG debug adapter for programming and debugging Silicon Labs C8051-family microcontrollers used in Pumpkin's CubeSat Kit development hardware.
| SKU | 633-00489 |
| Hardware Class | Development Hardware |
| Compatible With | Silicon Labs C8051F120 (PSPM B / PPM B1); JFPC-C8051 Programming Adapter |

A Total Phase Beagle I2C/SPI Protocol Analyzer offered by Pumpkin Space as a CubeSat Kit accessory for bus-level debugging.
| SKU | 634-00522 |
| Price | $495.00 |

A USB-to-serial debug adapter that provides a debugging terminal interface and optional power to Pumpkin CubeSat Kit modules via a 4-pin FPC connector.
| Connector | 4-pin FPC serial terminal/debug connector |
| I/O logic level | Selectable 3.3V (default) or 5V |
| Power output | 3.3V or 5V to connected device |
| Interface type | USB serial (USB-to-serial) |
| Product type | Development Hardware |
German manufacturer of miniature optoelectronic ADCS components for small satellites and CubeSats.

The Pyxis Space EGSE Box & Software package provides a complete Electrical Ground Support Equipment solution for testing, characterizing, and qualifying Pyxis Space ADCS compon
| PC Interface | USB |
| Software functions | Control, visualization, measurement analysis, firmware updates |
| Compatible products | All Pyxis Space ADCS sensors and actuators |
| Price | €5,000 |
Danish pioneer of drone-based RF testing and antenna measurement solutions for satellite antennas and electronic warfare, enabling cost-effective SATCOM ground segment testing without satellite access.

Drone-based RF direction-finding system that locates sources of RF interference, RFI, and signal degradation on ground station antennas in real time.
| Function | Drone-based RF interference localization |
| Platform | Autonomous UAV (drone) |
| Capability | Spatial triangulation of RFI sources |
| Use Case | Interference diagnosis at satellite ground stations |
| Integration | Quadsat cloud analytics platform |

UAV-based RF antenna measurement system for satellite ground stations, covering 1–18 GHz (downlink), providing far-field pattern data without shutting down live links.
| Frequency Range | 1–18 GHz |
| Link Direction | Downlink (DL) |
| Measurement Method | UAV-based far-field pattern measurement |
| Platform | Autonomous UAV (drone) |
| Applicable Bands | L, S, Ku-band |

Drone-based satellite antenna test and calibration system supporting the full antenna lifecycle, tailored for LEO and multi-orbit terminals.
| Measurement capabilities | Pointing accuracy, tracking and handover, radiation pattern raster and cut, cross-polar di |
| Antenna types supported | Multi-beam, flat-panel, electronically steerable (LEO and multi-orbit) |
| Lifecycle coverage | Manufacturing QC, vendor type approval, factory/site acceptance testing, in-situ deploymen |
| Test platform | Drone-mounted satellite signal emulator |

UAV-based satellite pass emulator that flies real orbital trajectories for LEO/MEO satellites, enabling end-to-end RF link testing and autotracking validation against live-equivale
| Function | Orbital trajectory emulation via UAV |
| Supported Orbits | LEO and MEO |
| Trajectory Input | TLE-based or custom pass definition |
| Test Capabilities | Autotracking, Doppler compensation, link budget, scheduling |
| Link Directions | Uplink and downlink |
Radian Aerospace designs and manufactures fully-reusable orbital mission platforms and reentry vehicles for routine and affordable space access.

The Radian Reusable Reentry Vehicle (R3V) is a modular, aerodynamically controlled, and recoverable vehicle designed to test advanced materials, sensors, avionics, and thermal prot
| Flight profiles | High-speed, high-stress (launch through hypersonic transition, reentry, and targeted landi |
| Maximum speed | Exceeding Mach 5 |
| Thermal Protection System | Radian’s patent pending Dur-E-Therm |
Robinson Aerospace Systems provides hands-on educational CubeSat kits and STEM solutions for schools, universities, and businesses globally, aiming to inspire and educate students in space technology.

The CubeSat Test Bench allows for easy testing and prototyping of RASCube modules by laying them out like a 'flatsat'. It connects modules as if they were stacked, and is available
| Compatibility | RASCube V1, V2 and LB |
Swiss-Swedish space components manufacturer providing satellite structures, thermal control products, payload electronics, and antennas for commercial and institutional programs.

Ground support equipment clampband connecting spacecraft interface rings to test adapters during AIT, in PAS 937 S, 1194 VS and 1666 MVS sizes.
| Clampband PAS 937 S | Manufactured per Ariane 5 User's Manual (Issue 5 Rev 2), Soyuz User's Manual (Issue 2 Rev |
| Clampband PAS 1194 VS | Manufactured per Ariane 5 User's Manual (Issue 5 Rev 2) and Soyuz User's Manual (Issue 2 R |
| Clampband PAS 1666 MVS | Manufactured per Ariane 5 User's Manual (Issue 5 Rev 2) and Soyuz User's Manual (Issue 2 R |
| Units delivered | More than 50 GSE clampbands |
| Services | In-house proof load testing without dummy equipment |

Tiltable and rotatable MGSE trolley supporting spacecraft during horizontal or vertical integration, with a full set of EC safety interlocks.
| Motion | Table tilts and rotates to any attitude between spin axis vertical and horizontal |
| Spacecraft interface | Transport and Handling Adapter (THA) or other test adapters |
| Materials | Aluminium alloy or carbon steel |
| Safety | EC-compliant interlocks: no rotating while tilting, no tilting while rotating, key-switch |
| Units delivered | Over 80 Multi-Purpose Trolleys in Europe and the USA |

Pressurized and non-pressurized spacecraft containers with thermal control, dynamic damping and air filtering, certified for air transportation.
| Container types | Hat-off, tilt-lid, door-type roll-in, large An124-compatible, constellation-type |
| Thermal control | Full active and passive thermal control |
| Environmental control | Air filtering and drying or N2 purging |
| Constellation container temperature | 19-25 degrees C during operation, -40 to 45 degrees C during transport |
| Constellation container humidity | Below 65% relH during operation, up to 100% relH during transport |

Large-format spacecraft transport container from Beyond Gravity's spacecraft container line, for the biggest geosatellites and deep space spacecraft.
| Product line | Beyond Gravity spacecraft containers (SCO) |
| Thermal control | Full active and passive thermal control |
| Environmental control | Air filtering and drying or N2 purging |
| Transport modes | Road, air, long-term storage; certified for air transportation on a wide range of aircraft |

Electrical or manual lifting devices for instruments and spacecraft of all sizes, with fixed or convertible hoisting axis and optional CoG adjustment.
| Actuation | Electrical or manual |
| Hoisting axis | Fixed, or convertible between horizontal and vertical configuration |
| Options | Remote control for lifting, centre-of-gravity adjustment |
| Range | From small instruments to very large spacecraft |
German manufacturer (Wuerzburg) of pico/nanosatellite subsystems and tailored small satellite systems, with flight heritage tracing back to the first German pico-satellite UWE-1.

Development kit for the standardized UNISEC Europe CubeSat bus, providing a satellite development board, subsystem prototype, and software starter kit for rapid CubeSat prototyping
| Satellite bus connector | Compact/robust backplane, redundant power + high/low-speed digital buses, dedicated reset/ |
| External debug interface | UART via USB bridge; JTAG, SBW, SWD programming/debugging; USB power supply (5V, 3.3V, unr |
| Power control circuit | OBC-controlled via redundant I2C, power switch, voltage/current monitoring, over/under-vol |
| Interface control circuit | Selective bus isolation, prevents current leakage during partial power down, OBC-controlle |
SERENUM Space is a CubeSat component and BUS manufacturer, integrator, and service provider based in Brno, Czech Republic, and a commercially oriented subsidiary of VZLU AEROSPACE.

Integration jigs, vibration test pods, transport boxes, and display cases for 1U-8U CubeSats.
| Vertical/Horizontal Support Jig material | Aluminium 2025, PA/PEEK clamps, Anodized/Alodine 1200 surface |
| Vertical Support Jig mass | 1.170 kg |
| Vertical Support Jig size | 220 x 220 x 87 mm |
| Vibration Jig sizes supported | 1U, 2U, 3U, 6U, 8U |
| Vibration Jig material | Aluminium 7075, no treatment or anodized |

Full-spectrum spacecraft environmental qualification and acceptance testing: vibration, shock, thermal-vacuum, and cleanroom services.
| Mechanical test types | Resonance search, quasistatic, sine, random, shock |
| TV chamber volume | 1000 x 1000 x 1000 mm |
| TV tunnel extension | 10 m x 200 mm diameter |
| Max part dimensions (TV chamber) | 950 x 870 x 780 mm |
| Vacuum level | < 10⁻³ Pa |
Indian spacetech company building the world's highest resolution L & P band Synthetic Aperture Radar (SAR) payloads for satellites, aircraft and drones, plus Ground Penetrating Radar and hyperspectral imaging systems.
Portable horizontal far-field antenna measurement facility delivering real-time 3D antenna radiation pattern and gain measurements.
| Angular Precision | 0.45 deg |
| Frequency Range | Customisable |
| Measurement Time (Per Plane) | 5 minutes |
| Standard Dimension (L x W x H) | 14 ft x 2 ft x 3 ft (customisable) |

Fully automated near-field antenna measurement system with anechoic chamber, 5 mm scan spacing and far-field projection.
| Maximum Scanning Area | 1.5 m x 1.5 m |
| Scan Speed | 100 scan points, 5 cm spacing (10x10), in 4 minutes |
| Scanning System | Horizontal Planar Measurement System |
| Provided Antenna RF Cable Length | 5-8 m |
| Height | Adjustable as required |
Vertical far-field antenna measurement facility for real-time antenna radiation pattern and gain measurement over the full frequency range.
| Angular Precision | 0.45 deg |
| Frequency Range | Customisable |
| Measurement Time (Per Plane) | 5 minutes |
| Standard Dimension (L x W x H) | 9 ft x 9 ft x 12 ft (customisable) |
SkyLabs is a Slovenian space-technology company that designs and manufactures miniaturized, fault-tolerant on-board data handling, communications, power, ADCS/GNC and EGSE equipment for small satellites.

Ground station equipment for CCSDS-compliant, full-duplex communication over S-band RF link with NANOlink-2 equipment.
| Type | CCSDS-compliant SDR ground station equipment |
| Frequency range | S-band |
| Error correction | Convolutional and Reed-Solomon codes |
| Compatible with | NANOlink-2, skyEGSE-GUI, NANOsky CMM SDK |

Ground station equipment for CCSDS-compliant, full-duplex communication over UHF/VHF RF link with NANOcomm-2 equipment.
| Type | CCSDS-compliant SDR ground station equipment |
| Frequency range | UHF/VHF |
| Error correction | Convolutional and Reed-Solomon codes |
| Compatible with | NANOcomm-2, skyEGSE-GUI, NANOsky CMM SDK |

USB interface dongle for high-speed, low-latency communication over CAN/LVDS/RS422 interfaces.
| Standard | IPC Class 3+ |
| MAIT | In-house |
| Interfaces | Two CAN buses, two high-speed LVDS (TIA/EIA-644), two RS422 (TIA/EIA-422) |
| Connectivity | USB Plug-n-Play |
San Jose, CA company pioneering plasma jet printing for direct-write conformal electronics manufacturing on complex 3D surfaces, with applications in space, aerospace, and in-space manufacturing.

Plasma jet printer for direct-write electronics on curved and complex 3D surfaces -- antennas, frequency-selective surfaces, and RF structures.
| Process | Single-step atmospheric-pressure plasma jet printing, no pre- or post-treatment |
| Substrate type | Curved, vertical, and complex 3D surfaces |
| Applications | Printed antennas, frequency selective surfaces, IML/OML printing, sensors and RF structure |
| Target markets | Aerospace & defense, automotive |

Compact plasma jet printing platform for R&D, process development, and proof-of-concept multi-material printing on planar surfaces.
| Process | Single-step atmospheric-pressure plasma jet printing, no pre- or post-treatment |
| Target use | Corporate R&D, university research, process development |
| Substrate type | Planar surfaces |
| Materials | Copper, silver, and dielectric inks |

Plasma jet print head integrated onto a robotic arm for conformal printing on complex 3D aerospace parts, including upside-down and OEM-integrated printing.
| Process | Single-step atmospheric-pressure plasma jet printing, orientation independent |
| Integration | Robotic arm-mounted print head, OEM integration supported |
| Applications | Complex 3D parts, upside-down printing, aerospace manufacturing |
SPiN (Space Products and Innovation) develops MA61C, a plug-and-play intelligent Command and Data Handling (C&DH) node that lets satellite manufacturers integrate subsystems from different suppliers without custom engineering, cutting desig

Plug-and-play Electronic Ground Support Equipment for monitoring and commanding satellite subsystems directly from a PC over USB.
| Interfaces supported | SpaceWire, I2C, CAN, UART, MIL-STD-1553, GPIO |
| Host interface | USB |
| Software | Integrated API and Windows GUI for commanding and monitoring |
Czech company (Brno) developing non-explosive, rapidly resettable hold-down and release actuators and initiation electronics for ground testing and qualification of spacecraft mechanisms.

PC-controlled current-pulse generator and control electronics for synchronized initiation of release actuators in ground testing.
| Actuation steps | Activation, arming, fire |
| Power source | 50 A / 12 V / 600 W |
| Number of actuators | Up to 5 actuators (10 power lines) |
| Arming current | 0.125 A |
| Status monitoring | LED and software |
Developer of smart habitats and life support systems for human exploration in space and extreme environments.

Precision artificial sun simulator for the ESA-DLR LUNA Analog Facility in Cologne, replicating the grazing-angle, high-contrast lighting conditions of the lunar south pole over a
| System type | Artificial sun simulator / precision lighting array |
| Simulated environment | Lunar south pole lighting conditions |
| Coverage area | 30 × 20 m |
| Lighting characteristics | Grazing incidence angles, tunable intensity, deep polar shadow patterns |
| Control system | Advanced programmable, tunable illumination |
SpinLaunch develops a kinetic (non-combustion) launch system that uses a rotating vacuum-sealed accelerator to hurl launch vehicles toward space, and operates Meridian Space, a low-cost LEO satellite communications constellation business.

A 33-meter vacuum-chamber test and qualification system at Spaceport America that launches payloads at 800-5,000 mph, serving as SpinLaunch's development platform and as a satellit
| Vacuum chamber span | 33 meters |
| Test payload velocity range | 800-5,000 mph |
| Location | Spaceport America, New Mexico, USA |
| Use cases | Development test flights, customer payload testing, satellite qualification, lunar-environ |
SPUTNIX is a Russian manufacturer of nanosatellite and microsatellite platforms, onboard subsystems and ground infrastructure, operating as a subsidiary brand of Sitronics Group.

A frictionless air-bearing table for testing relative-motion, docking, and multi-satellite GNC algorithms.
| Overall dimensions | 5000x4000x3000 mm |
| Active area dimensions | 1860x2480 mm |
| Platform carrying capacity | up to 10 kg |
| Working clearance between table surface and platforms | up to 0.5 mm |
| Working body | atmospheric air |

A modular, on-site-assembled anechoic chamber (200 MHz-45 GHz) for antenna pattern and EMC testing.
| Working volume | not less than 2x2x2 m |
| Anechoic volume | 0.7x0.7x0.7 m |
| Doorway dimensions | at least 1.9x1.9 m |
| Anechoic level | at least 20 dB (400-440 MHz range) |
| Shielding level | at least 40 dB (400-440 MHz range) |
SSBV Aerospace & Technology Group was a Dutch-led, technology-driven group of companies providing space and defence hardware, including smallsat subsystems, ground station equipment, and precision airdrop systems.

Telemetry and telecommand interface unit for satellite Electrical Ground Support Equipment (EGSE).
US manufacturer of optical measurement instruments, hyperspectral imaging systems, and thermal control coatings, founded 1977 in San Diego by former Apollo-program aerospace engineers.

A portable directional-hemispherical reflectometer that measures the integrated infrared surface reflectance of large objects in the field at two angles of incidence across six wav
| Measurement type | Integrated directional-hemispherical reflectance |
| Angles of incidence | 20° and 60° |
| Wavelength bands | Six bands |
| Spectral range | 0.9 to 12 μm |
| Interface | SOC410-DHR touchscreen interface with guided calibration, sample identification, and measu |

The SOC-100 HDR is an automated reflectometer that measures polarized, angular diffuse reflectance, transmittance, and directional emittance in the 2.0 to 25.0 μm spectral range, o
| Spectral Range | 2.0 – 25.0 λ (μm) / 5000 – 400 cm-1 Range can be modified based on FTIR optics. |
| Method | Automated reflectometer 18″ electroformed hemiellipsoid mated to Thermo Scientific™ Nicole |
| Calibration | Comparison of scans of the specimen sample and calibrated specular gold standard at each a |
| Source | A custom heated cavity provides uniform 2π steradian radiation into the subtended hemielli |
| Resolution | Depending on data requirement: 2, 4, 8, 16, or 32 cm-1 resolution may be employed. |

The SOC-210 BDR is an automated goniometer designed for precise and comprehensive measurement of Bidirectional Reflectance Distribution Function (BRDF) and Bidirectional Transmitta
| Spectral range | 0.35-14 micron |
| Incident polar angle | 0-85 degrees |
| Incident azimuth angle | 0-360 degrees |
| Reflected polar angle | 0-85 degrees |
| Reflected azimuth angle | 0-360 degrees |
The world's first incubator dedicated exclusively to the Moon, backed by CNES, supporting entrepreneurs developing solutions for sustainable human presence on the lunar surface.
Fieldisplay, developed by Anyfields and incubated through TechTheMoon, is a system for visualizing electromagnetic radiation and measuring antenna performance. As connected systems
| Function | Electromagnetic radiation visualization and antenna performance measurement |
| Applications | Satellites, drones, IoT devices, connected/autonomous machines |
| Measurement type | Radiation pattern, antenna gain, performance metrics |
Czech mission integrator and space hardware builder behind the CAVE CubeSat deployer, TRONE/CRUSOE EGSE, and the TRACE/TROLL NG/TRULY satellite missions.

Test Space is a comprehensive environmental testing facility offering thermal vacuum, electrodynamic shaker, and cleanroom services for hardware qualification, particularly suited
| shaker force | 45 kN (90 kN Shock) |
| shaker Max dynamic payload | 100 kg |
| shaker MAX frequency | 2000 Hz (on 1050×1050 mm slip table) |
| TVAC TEMPERATURE RANGE | -70 to +200 °C |
| tvac ULTIMATE VACUUM | < 10⁻⁶ mbar |

TILT is a two-axis rotation integration stand designed for CubeSats ranging from 6U to 16U, facilitating assembly, integration, and testing (AIT) with features for reduced handling
| Integrate CubeSats of sizes from | 6-16 U |
| Price of your Integration Stand | 6,990 EUR |
| Axes controlled rotation | 2 axis |
| TRL Level | 9+ |
Chinese manufacturer of high-precision star trackers, sun sensors, star simulators, and attitude control modules for satellites, with over 1,000 units flown on-orbit.

Ultra-compact TY-Space Dynamic Star Simulator (DSS-25) designed for all function and performance testing of star trackers mounted on satellites.
| Field Of View | 20x20 deg |
| Magnitude | 2 to 6.5 Mv |
| Accuracy | 30" [3sigma] |
| Update Rate | >= 40 Hz |
| Resolution | 2560x2560 |

The TY-Space Dynamic Star Simulators (DSS-14) is an instrument designed for function and performance testing of star trackers, offering adaptability to various star tracker brands.
| Field Of View | 20°×20° |
| Magnitude | 2 ~ 6.5 Mv |
| Accuracy | 30"[3σ] |
| Update Rate | ≥ 40Hz |
| Resolution | 1440 × 1440 |

TY-Space Dynamic Testing System (DTS) is mainly formed by a star tracker, a Dynamic Star Simulator (DSS), and an image acquisition system for satellite semi-physical simulation tes
| Dynamic Star Simulator | Receives quaternion from simulator computer; outputs real-time star field for satellite se |
| Star Tracker - Attitude Accuracy (pointing/rolling) | 3"/50" [3sigma] |
| Image Acquisition System | Image acquisition, real-time display and storage |

The TY-Space Optical Star Pattern Simulator (OSPS) is a static star simulator designed for testing the function and performance of star trackers, including in environmental experim
| Field Of View | 15°×15° |
| Number of Stars | >15 |
| Sky District | North Pole Area / Customization |
| Optics / Illumination | Collimating / LED |
| Dimension | Φ65mm×73mm |

TY-Space Static Star Testing System (SSTS) is mainly formed by a star tracker, an Optical Star Pattern Simulator (OSPS), and an image acquisition system.
| Optical Star Pattern Simulator | Static star simulator, North Pole Area/Customization |
| Star Tracker - Attitude Accuracy (pointing/rolling) | 3"/50" [3sigma] |
| Image acquisition system | Image acquisition, real-time display and storage |
US manufacturer of precision fluid control components and integrated propulsion systems for spacecraft, with 70+ years of heritage. Products include micro propulsion systems, valves, pressure regulators, and CubeSat propulsion modules.

A differential pressure indicator that provides visual or remote warning when a filter element is nearing the end of its service life, designed for reliability and high G-load tran
| Material | Aluminum (std), Corrosion Resistant Steel (optional) |
| Seals (Electrometric) | Buna “N” (std), Viton (std), EPR (std), Others Upon Request |
| Operating Pressure | 5,000 psig |
| Proof Pressure | 7,000 psig |
| Burst Pressure | 12,500 psig |
VORAGO Technologies designs radiation-hardened ARM microcontrollers and processors for space and extreme-environment applications using patented HARDSIL technology.

The VORAGO PEB1 is the primary development and evaluation platform for the VA416X0 family of radiation-hardened ARM Cortex-M4 microcontrollers (VA41620 and VA41630). The kit compri
| Target MCU Options | VA41620 or VA41630 (ARM Cortex-M4, HARDSIL) |
| SBC Dimensions | 3.15 x 3.3 inches |
| Boot NVM (SBC) | 256 KB SPI FRAM |
| Clock Generation | 20 MHz - 80 MHz programmable |
| Crystal Oscillator | 10 MHz |
Polish RF/microwave company in Gdynia, founded 2002; L/S/X/Ku-band components, space-grade diplexers and filters, and EMC testing laboratory services.

The WiRan S-Band Test Cap is a precision-engineered accessory for full-duplex testing of S-band antennas on satellites, operating within the 2025–2290 MHz frequency range.
| Frequency range | 2025-2290 MHz |
| Return Loss | >15 dB |
| Gain | Avg. -25 dB |
| Flattness | ±2 dB |
| Power Handling | 10 Watt |
PocketQube deployer and vibration test equipment maker, plus mechanical engineering consultancy for small-satellite developers.

The 1.5P VibePOD is a test fixture designed for random vibration testing of 1.5P Pocketqubes, qualified to NASA GEVS7000 standards.
| Dimensions w/o plate | 98mm x 96mm x 117mm |
| Dimension of adapter plate | 230mm x 230mm x 14mm |
| Mass (Dry) | 1.1kg |
| First mission | 2020 EASAT-2 1.5P |
| Qualification | NASA GEVS7000 in 2020 |

An open-source 2P CubeSat-format vibration test pod used to mechanically qualify a Payload Qualification (PQ) unit during vibration testing.
| Dimensions w/o plate | 147mm x 98mm x 96mm |
| Dimension of adapter plate | 230mm x 230mm x 10mm |
| Mass (Dry) | 1.3kg |
| First mission | Awaiting to be qualified. |

The 3P Vibe POD is an open-source vibration testing fixture designed to qualify 3-unit CubeSat Payloads (3P PQ) by simulating launch environment vibrations.
| Dimensions w/o plate | 211mm x 98mm x 96mm |
| Dimension of adapter plate | 330mm x 330mm x 10mm |
| Mass (Dry) | 1.6kg |
| First mission | Awaiting to be qualified. |
XCAM designs space-qualified CubeSat cameras, scientific X-ray detectors, in-vacuum cameras, and particle fallout monitors for space and scientific research applications.

Customisable CCD/EMCCD vacuum camera system for UHV/XHV environments, available in flange-mounted or hermetically sealed immersible configurations.
| Vacuum Compatibility | UHV / XHV / UCV |
| Detector Types | CCD, EMCCD |
| Illumination | Front-illuminated (FI) and back-illuminated (BI) |
| Readout Speed | Up to 3 MHz |
| Readout Channels | Up to 4 |

Imager Control Systems for evaluating Teledyne e2v CIS120, CIS125, CIS300, and ChromaD scientific imaging sensors with Camera Link, Ethernet, and USB 3 interfaces.
| CIS 120 Sensor Format | 2048 x 2048 pixels |
| CIS 120 Pixel Size | 10 um |
| CIS 120 Illumination | Back-illuminated (visible, UV, EUV) |
| CIS 120 Noise | 3 e- RMS |
| CIS 120 Data Interface | Camera Link |

The Imager Control System (ICS) is an electronic interface for managing and operating imaging sensors, providing precise power, current, and voltages for reliable function and enab
| Sensor | Teledyne e2v 'Capella', 2k x 2k back-illuminated, 10 µm pixels |
| Applications | Visible, UV, and EUV |
| Noise | 3 e⁻ rms |
| Data Interface | Camera Link |
| Software | Python code included |

The Imager Control System (ICS) is an electronic interface for managing and operating imaging sensors, providing precise power, current, and voltages for reliable function and enab
| Sensor | Teledyne e2v CIS 300 |
| Format | Up to 9k x 9k pixels |
| Data Lines | 12 |
| Thermal | Temperature sensing, thermal control connectivity |
| Data Interface | USB 3 |

Real-time particle fallout monitor for cleanrooms using Direct Particle Detection (DPD) technology, sampling 4 cm2 at up to 10 samples per hour.
| Total Detection Area | 4 cm2 |
| Sample Rate | 10 per hour |
| Particle Detection Range | 5 to >750 um |
| Operating Temperature | +20 to +35 deg C |
| Housing Material | Aluminium |

ESA-funded autonomous particulate contamination monitor for space launch vehicle fairings, detecting particles from 5 um during ascent.
| Total Detection Area | 4 cm2 |
| Sample Rate | Every 10 seconds (minimum) |
| Minimum Detectable Particle Size | 5 um (100% detection) |
| Maximum Detectable Particle Size | >750 um |
| Data Acquisition Lifetime | >=254 seconds |

Compact USB in-vacuum video camera for monitoring processes inside vacuum chambers, rated to 10e-6 mbar with built-in LED illumination.
| Dimensions | 50 x 50 x 60 mm (excl. lens and USB connector) |
| Image Sensor | 1.3 MP CMOS, 1/1.8 inch format, RGB or B&W |
| Pixel Size | 5.5 um |
| Lens Mount | C-mount, wide-angle fixed focus |
| Wavelength Range | 400-1000 nm |
Chinese Academy of Sciences research institute in Xi'an developing space optics, precision photonic instruments, and optical remote sensing payloads for China's satellite and space programs.

Compact space environment simulation chamber for thermal-vacuum testing of optical instruments and payloads.
| Type | Thermal-vacuum space environment simulation chamber |
| Conditions | Vacuum + thermal cycling (cryogenic to elevated temperature) |
| Application | Component and subsystem-level space qualification testing |
| Optional | UV/radiation exposure capability (configuration-dependent) |
| Purpose | Pre-launch environmental verification of optical payloads |

Ultra-high-speed streak cameras for transient optical phenomena, laser diagnostics, and space instrument characterization by XIOPM.
| Technology | Photoelectric streak tube with CCD/CMOS readout |
| Time resolution | Picosecond to nanosecond range |
| Spectral range | UV to near-IR (model-dependent) |
| Application | Laser diagnostics, ICF, plasma physics, space instrument testing |
| Division | Streak Camera and Electro-optical Conversion (SCEC), XIOPM |
US passive microwave and RF components manufacturer in Manchester, NH; TVAC-rated space hardware, cryogenic components, attenuators, adapters, power dividers for satellite and defence.

A cryogenic-compatible SMA male RF termination rated to 26.5 GHz and 1 Watt average power.
| Item # | 2001-61XX-0X-CRYO |
| Description | Term, SMA-m, 26.5GHz, 1W |
| Add-ons | Chain |
| Materials | SS or Gold-plated |
| Types | Terminations |
Zero-G Solutions provides FAA-approved commercial parabolic flights for astronaut training, scientific research, and public experiences in zero, Lunar, and Martian gravity.

Parabolic microgravity/lunar/Martian-gravity flights for testing space technology payloads before launch.
| Parabolas per research flight | 30 (double standard flight) |
| Total weightlessness duration | Up to 15 minutes |
| Gravity levels available | Microgravity, lunar gravity, Martian gravity (customizable) |
| Aircraft | G-Force One (modified Boeing 727) |
| Handheld mixed payload seat | $10,300 (1 person, 90+ day advance booking) |
Directory
R&D company providing miniaturized radiation dosimeters and EMC filters for space and ground applications. TRL-9 flight heritage.
AAA Engineering & Test Lab provides precision electronic component testing, upscreening, failure analysis, and counterfeit mitigation services for aerospace, space, defense, medical, and ind
Aaronia AG develops and manufactures spectrum analyzers, spectrum analysis software, and drone detection and defense systems, all produced in Germany.
Accord Software & Systems designs and manufactures customized GPS/GNSS receivers for space applications and GPS/GNSS semiconductor chips for defense and commercial markets.
Redwire is an integrated aerospace and defense company providing advanced technologies for space infrastructure, autonomous systems, and multi-domain operations to government agencies and de
Alba Orbital manufactures PocketQube satellites, provides launch and ground station services, and operates a fleet of nighttime imaging satellites for government and commercial clients.
AVCOM of Virginia is a satellite communications equipment manufacturer founded in 1976, specializing in spectrum analyzers, satellite beacon receivers, and RF signal monitoring products.
Huali Chuangtong (华力创通, Hwacreate) is a Chinese satellite navigation and IoT technology company listed on the Shenzhen Stock Exchange, headquartered in Beijing, developing GNSS (GPS/BeiDou)
Celestia Satellite Test & Simulation provides ground-based solutions for satellite simulation, testing, communication, and data processing, including EGSE, TT&C, and Optical Modems.
Climats is a French manufacturer of high-precision environmental and climatic test chambers, including customized thermal-vacuum chambers for space qualification testing.
Indian CubeSat developer offering flight-ready 1U–6U satellite structures, subsystem components, environmental testing services, launch integration, and STEM education programs from Ahmedaba
Vertically integrated Indian defence and aerospace electronics company designing and manufacturing avionics, microelectronics, RF/microwave, radar, test equipment and space systems.
Advanced testing and engineering services provider for U.S. space, defense, and government programs.
Developer of fluid-dynamic attitude control systems, gyroscopes, and air bearings for the space industry.
Greek space engineering company delivering advanced modeling, simulation, independent software verification, magnetic cleanliness testing, and IOD/IOV mission support. Holder of a €4M ESA He
ETS-Lindgren designs and manufactures electromagnetic and acoustic energy components and systems, including RF shielded chambers and EMC test chambers, for industrial and commercial markets.
French SATCOM equipment distributor and integrator; ground station hardware across L to Q band; founded 2003 in Les Ulis.
German manufacturer of reaction wheels, CubeSat picosatellite deployers, and AOCS components for small satellites, based in Berlin-Adlershof.
Modular nanosatellite platforms and space test equipment using robotics, AI, and advanced materials.
Experior Laboratories provides independent design verification and qualification testing services for components and systems across space, aerospace, military, and other industries.
American company making the EyasSat nanosatellite simulator, an educational spacecraft kit co-developed with the US Air Force Academy covering all six satellite bus subsystems for university
Danish embedded software specialist providing satellite communications protocol stacks, waveforms and test tools for terminals, satellites and networks.
GAUSS Instruments manufactures high-performance EMC test equipment and EMI test solutions, including real-time receivers, for various industry standards and applications.
GDP Space Systems designs and manufactures telemetry receivers, satellite modems, and range management systems for aerospace and flight test applications.
Swiss opto-electronics company (part of General Atomics since 2021) developing laser-communication beam-pointing systems, optical ground stations, and free-space/fiber optical communication
Glavkosmos coordinates international human spaceflight projects, facilitates satellite launches, develops and supplies rocket components, and provides equipment for space crews.
System integrator and manufacturer of CubeSat structures, buses, and MyPOD test/transport pods, with space environment test equipment services.
India-based space EdTech platform offering CubeSat and CanSat educational kits, high-altitude balloon hardware, and online space science courses for students worldwide.
Indian small satellite manufacturer offering flight-proven platforms, subsystems, and mission-as-a-service solutions.
SPACE COTAN Co., Ltd. is a Japanese company developing and operating the Hokkaido Spaceport at Taiki-cho (Taiki Town) in Hokkaido, Japan's northernmost main island, as a commercial launch si
South Africa-based space hardware company developing the Lumen thermal vacuum testing system and providing TVAC test services for the aerospace industry.
German technology company providing testing, simulation, and engineering services for aerospace, defense, and space systems.
CubeSat deployers, antennas, EPS and small-satellite systems.
Jena-Optronik designs and manufactures sensors, space optics, and electronics for satellites and spacecraft, supporting communication, navigation, and Earth observation.
KRYTAR designs and manufactures ultra-broadband microwave, mmWave, and RF components and test equipment for commercial and military applications, covering DC to 110 GHz.
LabSat, a brand of Racelogic, provides compact GNSS record and replay simulators enabling reliable, repeatable testing of GNSS-enabled devices across automotive, aerospace, and industrial ap
Dutch developer of SmallSat and CubeSat separation systems providing smart, lightweight, cost-effective satellite deployers for launch mission management.
Dutch manufacturer of precision optical components and sun sensors for space missions, with flight heritage on ESA programs including LISA.
Madrid-based aerospace engineering company specialising in opto-mechanical systems, flexible thermal straps, and cryogenic units for space missions.
Total liquid immersion cooling technology for servers and electronics, using patented Directed-Flow cooling in standard 19-inch racks for data center, edge, and rugged industrial application
Redwire is an integrated aerospace and defense company providing advanced technologies, space infrastructure, and autonomous systems for government agencies and defense programs.
Lunar Research Service (LRS) is a Ukrainian space technology company specializing in hardware and materials testing for space applications, nanosatellite development, and extreme-environment
Lúnasa is a London-based space technology company building navigation, autonomy, and rendezvous and proximity operations (RPO) systems for the in-orbit servicing and manufacturing (ISAM) mar
Magson GmbH is a Berlin-based manufacturer of high-performance digital fluxgate magnetometers for terrestrial and space applications, including spacecraft attitude control systems.
Chinese commercial satellite manufacturer building Earth observation, communications, and remote sensing satellites, plus payloads, components, and ground terminal systems.
UK national measurement institute providing precision timing, frequency standards, and calibration services critical for satellite navigation and space systems.
Nautilus Navigation in Space designs autonomous Guidance, Navigation, and Control (GNC) sub-systems, provides Flight Dynamics as a Service, and develops ground testing equipment for space mi
Polish smallsat hardware company designing and manufacturing components and subsystems for CubeSats and small satellites, serving commercial and institutional space customers across Europe.
NOFFZ Technologies is a German manufacturer of universal test and automation systems, including RF test platforms and GNSS signal simulators for aerospace, defense, and automotive applicatio
Italian electric propulsion startup developing water-propelled resistojet thruster systems for nanosatellites and microsatellites, offering a safe, low-cost, and high-performance propulsion
US defense and technology prime contractor providing space systems engineering, missile defense integration, space domain awareness, and ground system development for US government programs.
San Francisco-based manufacturer of flight-proven CubeSat kits, SUPERNOVA nanosatellite buses, and spacecraft power/electronics components, with over 150 kits delivered and dozens of success
German manufacturer of miniature optoelectronic ADCS components for small satellites and CubeSats.
Danish pioneer of drone-based RF testing and antenna measurement solutions for satellite antennas and electronic warfare, enabling cost-effective SATCOM ground segment testing without satell
Radian Aerospace designs and manufactures fully-reusable orbital mission platforms and reentry vehicles for routine and affordable space access.
Robinson Aerospace Systems provides hands-on educational CubeSat kits and STEM solutions for schools, universities, and businesses globally, aiming to inspire and educate students in space t
Swiss-Swedish space components manufacturer providing satellite structures, thermal control products, payload electronics, and antennas for commercial and institutional programs.
German manufacturer (Wuerzburg) of pico/nanosatellite subsystems and tailored small satellite systems, with flight heritage tracing back to the first German pico-satellite UWE-1.
SERENUM Space is a CubeSat component and BUS manufacturer, integrator, and service provider based in Brno, Czech Republic, and a commercially oriented subsidiary of VZLU AEROSPACE.
Indian spacetech company building the world's highest resolution L & P band Synthetic Aperture Radar (SAR) payloads for satellites, aircraft and drones, plus Ground Penetrating Radar and hyp
SkyLabs is a Slovenian space-technology company that designs and manufactures miniaturized, fault-tolerant on-board data handling, communications, power, ADCS/GNC and EGSE equipment for smal
San Jose, CA company pioneering plasma jet printing for direct-write conformal electronics manufacturing on complex 3D surfaces, with applications in space, aerospace, and in-space manufactu
SPiN (Space Products and Innovation) develops MA61C, a plug-and-play intelligent Command and Data Handling (C&DH) node that lets satellite manufacturers integrate subsystems from different s
Czech company (Brno) developing non-explosive, rapidly resettable hold-down and release actuators and initiation electronics for ground testing and qualification of spacecraft mechanisms.
Developer of smart habitats and life support systems for human exploration in space and extreme environments.
SpinLaunch develops a kinetic (non-combustion) launch system that uses a rotating vacuum-sealed accelerator to hurl launch vehicles toward space, and operates Meridian Space, a low-cost LEO
SPUTNIX is a Russian manufacturer of nanosatellite and microsatellite platforms, onboard subsystems and ground infrastructure, operating as a subsidiary brand of Sitronics Group.
SSBV Aerospace & Technology Group was a Dutch-led, technology-driven group of companies providing space and defence hardware, including smallsat subsystems, ground station equipment, and pre
US manufacturer of optical measurement instruments, hyperspectral imaging systems, and thermal control coatings, founded 1977 in San Diego by former Apollo-program aerospace engineers.
The world's first incubator dedicated exclusively to the Moon, backed by CNES, supporting entrepreneurs developing solutions for sustainable human presence on the lunar surface.
Czech mission integrator and space hardware builder behind the CAVE CubeSat deployer, TRONE/CRUSOE EGSE, and the TRACE/TROLL NG/TRULY satellite missions.
Chinese manufacturer of high-precision star trackers, sun sensors, star simulators, and attitude control modules for satellites, with over 1,000 units flown on-orbit.
US manufacturer of precision fluid control components and integrated propulsion systems for spacecraft, with 70+ years of heritage. Products include micro propulsion systems, valves, pressur
VORAGO Technologies designs radiation-hardened ARM microcontrollers and processors for space and extreme-environment applications using patented HARDSIL technology.
Polish RF/microwave company in Gdynia, founded 2002; L/S/X/Ku-band components, space-grade diplexers and filters, and EMC testing laboratory services.
PocketQube deployer and vibration test equipment maker, plus mechanical engineering consultancy for small-satellite developers.
XCAM designs space-qualified CubeSat cameras, scientific X-ray detectors, in-vacuum cameras, and particle fallout monitors for space and scientific research applications.
Chinese Academy of Sciences research institute in Xi'an developing space optics, precision photonic instruments, and optical remote sensing payloads for China's satellite and space programs.
US passive microwave and RF components manufacturer in Manchester, NH; TVAC-rated space hardware, cryogenic components, attenuators, adapters, power dividers for satellite and defence.
Zero-G Solutions provides FAA-approved commercial parabolic flights for astronaut training, scientific research, and public experiences in zero, Lunar, and Martian gravity.
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