NewSpace Market · Sector Catalogue
OBC & Avionics
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
What is inside
This catalogue lists 267 obc & avionics products offered by 103 manufacturers across 33 countries. Of those, 119 carry a manufacturer datasheet and 18 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 14 October 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.
Manufacturers by country
Overview
All products at a glance
| Product | Manufacturer | Country | Key specification | Price |
|---|---|---|---|---|
| A445 IBOX Radiation Tolerant Engine Controller | Aitech Systems | United States | Control logic: FPGA (radiation-tolerant, user-reprogrammable) | on request |
| A664 FPGA IP Core | Beijing Huali Chuangtong Technology Co., Ltd. | China | — | on request |
| A664 Network Analyzer | Beijing Huali Chuangtong Technology Co., Ltd. | China | — | on request |
| A664 Signal Switch | Beijing Huali Chuangtong Technology Co., Ltd. | China | — | on request |
| A664 Stimulus/Acquisition Card | Beijing Huali Chuangtong Technology Co., Ltd. | China | — | on request |
| A664 Switch (100 Mbps) | Beijing Huali Chuangtong Technology Co., Ltd. | China | — | on request |
| A664 Switch (Gigabit) | Beijing Huali Chuangtong Technology Co., Ltd. | China | — | on request |
| ABACUS On-Board Computer | GAUSS Srl | Italy | Cores: Two cores (MCU MSP430 and FPGA Spartan-3E) directly interconnected w… | on request |
| ADS | Unibap Space Solutions AB | Sweden | Ix10 ads-x2 cpu: AMD Ryzen V1000 | on request |
| Aether Software Platform | Aethero | United States | Deployment: Cloud + Edge (cloud.aethero.com) | on request |
| AMATDT | Aethero | United States | Deployment target: Aethero Edge Computing Modules (NxA-ECM, NxN-ECM) | on request |
| Andromeda: Guidance, Navigation & Control (GNC) Software | Saturn Space | United States | Compatible orbits: GEO, MEO, LEO | on request |
| Andromeda: Guidance, Navigation & Control (GNC) Software | Saturn Satellite Networks | United States | Compatible orbits: GEO, MEO, LEO | on request |
| Antartix – Computadora OBC | VENG S.A. | Argentina | Factor de forma: PCI/104-Express totalmente compatible | on request |
| Antelope | KP Labs | Poland | Size: 13.24 x 95.9 x 90.1 mm | on request |
| Antelope Advanced Data Processing Unit | KP Labs | Poland | Processor: AMD Zynq UltraScale+ MPSoC (ZU2/3/4/5 variants) | on request |
| Aptos | Aptos Orbital | United States | Years in space: 5.5 | on request |
| ASTROFEIN GPS receiver unit- ARGO | EXA (Astro-und Feinwerktechnik) | Germany | Frequency: GPS L1 Band, C/A code | on request |
| Aurora 1000 Satellite-Borne Intelligent Computer | Zhongke Tiansuan (Comospace) | China | On-orbit operation: 1,000+ cumulative days (multiple satellites) | on request |
| Avionic Systems | Data Patterns (India) Ltd. | India | — | on request |
| Baize Integrated Electronics System | Hongqing Technology (鸿擎科技) | China | Functions: Attitude control, power management, thermal control, telemetry/t… | on request |
| BRAVO-II Motor Controller | Motiv Space Systems | United States | Axis: Dual Axis Motor Controller Card | on request |
| Breakout Board Module | Pumpkin, Inc. | United States | SKU: 711-00380 | $255 |
| Catalyst – Unibap Collaboration | Unibap Space Solutions AB | Sweden | — | on request |
| CAVU CDH-FS | CAVU Aerospace | United Kingdom | Key system features: Dual Cold/Hot Redundant OBC Modules | on request |
| CAVU OBC-1 | CAVU Aerospace | United Kingdom | Expected life-time: 3-5 years in LEO | on request |
| CCM3012 3U OpenVPX I/O Carrier Board | Mercury Systems | United States | PMC-X sites: 1 | on request |
| CCM6020 6U OpenVPX I/O Carrier Board | Mercury Systems | United States | PMC/XMC sites: 2 | on request |
| CDH-110 | Berlin Space Technologies | Germany | Data interfaces: RS422, SPI, PWM | on request |
| CDH-FS | CAVU Aerospace | United Kingdom | Memory (RAM): 160Mbits MRAM 40 bits width (128Mbits+32Mbits ECC) | on request |
| CELESTE GNSS Receiver | Spacemanic s.r.o. | Slovakia | Operating temperature: -40°C to +85°C | on request |
| CFC-400XS Compact Flight Computer | Innoflight | United States | Processor board: Defense-grade Xilinx UltraScale+ MPSoC (GPP + FPGA) | on request |
| CFC-405XP / CFC-450XP Compact Flight Computer | Innoflight | United States | Processor board: Defense-grade Xilinx UltraScale+ MPSoC (GPP + FPGA) | on request |
| CFC-510P Compact Flight Computer | Innoflight | United States | Processor board: AMD Ryzen GPU | on request |
| CFC-600P Compact Flight Computer (AI/ML) | Innoflight | United States | Processor board: Defense-grade AMD Versal AI Edge adaptive SoC | on request |
| CM950 PMC Carrier Card for 3U CompactPCI SBCs | Aitech Systems | United States | Form factor: Single-slot 3U CompactPCI | on request |
| CM951 PMC Carrier Card with Integrated MIL-STD-1553B | Aitech Systems | United States | Form factor: Single-slot 3U CompactPCI | on request |
| Cockpit & Rugged Displays | Data Patterns (India) Ltd. | India | Display size: 3" to 20" | on request |
| CODE+ Software Defined Drive Electronics | Beyond Gravity (ex-RUAG Space) | Switzerland | Architecture: Fully software-defined, radiation-tolerant microcontroller | on request |
| COMBO – Space-Grade Configuration Memory Boot Manager | 3D Plus (HEICO) | France | Part number: 3DCO0849 / 3DMCO0849 | on request |
| Command and Data Handling (C&DH) System | Tyvak International S.r.l. | Italy | — | on request |
| Comospace Satellite Edge Computing Platform | Zhongke Tiansuan (Comospace) | China | Technology: In-orbit edge computing and AI processing | on request |
| Constellation On Board Computer (cOBC) | Beyond Gravity (ex-RUAG Space) | Switzerland | Architecture: Complete subsystem based entirely on commercial components | on request |
| Constellation Remote Terminal Unit (cRTU) | Beyond Gravity (ex-RUAG Space) | Switzerland | Function: Bridge between On-Board Computer and platform electronic interfaces | on request |
| Core Drive Electronics (CODE) | Beyond Gravity (ex-RUAG Space) | Switzerland | Type: Two-axis stepper motor controller, modular and stackable | on request |
| COTS Boards | Data Patterns (India) Ltd. | India | — | on request |
| CP400.85 | AAC Clyde Space | Sweden | TRL: 9 | on request |
| CryptoSWIFT FIPS140-2 | Tethers Unlimited, Inc. (AMERGINT) | United States | Built for: LEO small satellite missions | on request |
| CubeSat Kit Upgrade to C8051 | Pumpkin, Inc. | United States | SKU: 711-00717 | on request |
| CubeSat Kit Upgrade to dsPIC33 | Pumpkin, Inc. | United States | SKU: 711-00719 | $5 455 |
| CubeSat Kit Upgrade to MSP430 | Pumpkin, Inc. | United States | SKU: 711-00716 | on request |
| CubeSat Kit Upgrade to PIC24 (PIC24FJ256GA110) | Pumpkin, Inc. | United States | SKU: 711-00718 | $5 455 |
| CubeSat Kit Upgrade to PIC24 (PIC24FJ256GB210) | Pumpkin, Inc. | United States | SKU: 711-00795 | $5 455 |
| CubeSat OBC / ADCS Motherboard SXC-MB-04-ADC | SPUTNIX | Russia | Form factor: PC/104 | on request |
| CubeSat Payload Controller | NanoAvionics | Lithuania | Type: Payload data / control unit | on request |
| Custom Embedded Solutions and Modified COTS Products | Alpha Data Parallel Systems | United Kingdom | Operating temperature: 0 to +55 °C | on request |
| DARA OBC | Alén Space | Spain | — | on request |
| DARA OBC — On-Board Computer | Alén Space | Spain | TRL: TRL-9 (Flight Heritage) | on request |
| Data Processing Units | DSI Aerospace Technology | Austria | — | on request |
| Deep Thought | Spacemanic s.r.o. | Slovakia | Operating temperature: -40°C to +85°C | on request |
| Development Board (DB) | Pumpkin, Inc. | United States | SKU: 710-00297 | $1 710 |
| Development Board 2 (DB2) | Pumpkin, Inc. | United States | Bus connectors: Two interconnected 104-pin CubeSat bus connectors with M3 s… | $375 |
| DP-OBC-0402 On Board Computer | Data Patterns (India) Ltd. | India | Processor: e200 core processor, dual core | on request |
| E-Series: Orbital DPUs | Edge Aerospace | Luxembourg | Function: Command & control, data handling, AI-enabled autonomy | on request |
| E193 1/2-ATR 3U VPX & CompactPCI Rugged Enclosure | Aitech Systems | United States | Form factor: 1/2-ATR, 3U | on request |
| E900 8-Slot 3U CompactPCI Space Enclosure | Aitech Systems | United States | Slot configuration: 8-slot 3U CompactPCI backplane | on request |
| E905 1/2 ATR 3U CompactPCI Space Enclosure | Aitech Systems | United States | Slot configuration: 3-slot 3U CompactPCI | on request |
| EDDIE | Spacemanic s.r.o. | Slovakia | Operating temperature: -40°C to +85°C | on request |
| EDGE-1100 | ibeos | — | Processing Power: 1.1 TFLOPS (2 TFLOPS single precision) | on request |
| EDGX Sterna DPU — Onboard AI Compute powered by NVIDIA | EDGX | Belgium | Compute architecture: NVIDIA Orin GPU | on request |
| EIDEL Remote Interface Unit (ERIU) | Eidel | Norway | Interfaces supported: SpaceWire, CAN bus, RS-422 | on request |
| Electronic Design Services | ALTER Technology | Spain | PCB substrate types: FR4, IMS, flexible, rigid-flex | on request |
| Embedded Computing and OBC for Smallsats | CONTEC | South Korea | Products: Embedded SBCs, OBC modules, industrial IoT, data acquisition for … | on request |
| Emtech AstroCore-R Onboard Computing Platform | Emtech Space | Greece | Radiation tolerance: Radiation-supervised design | on request |
| ESCC3503001 Space Clock Oscillator (XO) | Rakon Limited | New Zealand | Frequency range: 4–100 MHz | on request |
| EXObox | Exolaunch | Germany | Maximum satellites managed per unit: 50 | on request |
| FERMI OBC&DH Miniaturized Rad-Hard On-Board Computer | Argotec Srl | Italy | Type: On-Board Computer and Data Handling unit (OBC&DH) | on request |
| FG-1 | CAVU Aerospace | United Kingdom | Supply voltage: Single 12 V or 5 V and 12 V | on request |
| FLOTONE ONE | Cosmoleap | China | — | on request |
| Fortis™ VPX | Sidus Space, Inc. | United States | System components: SSBC (Quad-Core ARM, rad-hard PolarFire FPGA, 8 GB DDR4)… | on request |
| FoX Electronics Platform | Beyond Gravity (ex-RUAG Space) | Switzerland | Form factor: 3U SpaceVPX modular platform | on request |
| FoX Payload Processor | Beyond Gravity (ex-RUAG Space) | Switzerland | Function: Control and data processing for payloads, instruments and robotics | on request |
| Fusio RT Space Computer Core | 3D Plus (HEICO) | France | FPGA resources: 550k ASIC gate equivalents (4,400,000 system gates) | on request |
| G-200 / G-510 Gyroscopes | ElmSpace | Germany | Models: G-200, G-510 | on request |
| GR740 | Gaisler | Sweden | TRL: 9 | on request |
| GR740 Module (ICU CPU Module) | EREMS | France | Processor: GR740 | on request |
| GSC6203 6U OpenVPX GPGPU Coprocessing Board | Mercury Systems | United States | GPU: Dual NVIDIA Pascal P5200E MXM | on request |
| HDS6603B 6U OpenVPX, SOSA-aligned, Multiprocessing Board | Mercury Systems | United States | Processors: Dual Intel 2.2 GHz 10-core or 1.8 GHz 14-core Xeon (Broadwell) … | on request |
| I/O LED Module | Pumpkin, Inc. | United States | SKU: 710-00521 | $360 |
| IARE Aerospace Systems Laboratory | Institute of Aeronautical Engineering | India | Type: Research Laboratory | on request |
| ICE Cube — On-Board Computer Unit (OBCU) | N7 Space | — | Processor: LEON3 SPARC V8 | on request |
| ICE-Lok Thermally Enhanced Wedge Locks | ACT (Advanced Cooling Technologies) | United States | Thermal resistance reduction vs. COTS: > 33% | on request |
| Insight4EO On-Board AI Processing | Deimos Space (Indra) | Spain | Processing type: On-board AI / edge processing | on request |
| Instrument Control Unit (ICU) | Kayser Space | Italy | Functions: Power distribution, command handling, data acquisition, communic… | on request |
| Instrument Control Units | DSI Aerospace Technology | Austria | Reliability: > 0.99 | on request |
| Integrated Circuit 1879 VM8Y | NTC Module | — | Package type: HFCBGA-1444 | on request |
| Integrated Electronics Module (IEM) | Tiger Innovations, Inc. | United States | Power consumption: 24 Watts | on request |
| Integrated EPS/OBC Bus Module | Aphelion Orbitals | United States | Mppt inputs: 5 with 40 W input capacity | on request |
| IOI-8 Input/Output Interfaces Module | Innoflight | United States | Interfaces: 4x 2.5GBase-T (2.5 GbE), 4x 1000Base-T (GbE) | on request |
| IP & MM (Industry Pack and M-Module Modules) | Data Patterns (India) Ltd. | India | Dp-IP-3039: 48 Channel Digital I/O IP Module | on request |
| iX20 | Unibap Space Solutions AB | Sweden | CPU: AMD Ryzen V8000 | on request |
| iX5 | Unibap Space Solutions AB | Sweden | Flight heritage: 5 missions launched | on request |
| iX5-100 | Unibap Space Solutions AB | Sweden | — | on request |
| KAM/CSB/12U Smart Backplane Chassis | Curtiss-Wright Defense Solutions | United States | Slots: 12 | on request |
| Kryten-M3 & Kryten-M3 PLUS | AAC Clyde Space | Sweden | Design life: 5 years in LEO | on request |
| LCS MiniNODE Industrial Computing System | LiquidCool Solutions | United States | Cpu: AMD Ryzen 5 5600G (6C/12T, 4.4 GHz boost) | on request |
| LDS3517 3U OpenVPX Single Board Computer | Mercury Systems | United States | Main processor: Intel 8-core, 64 bit, Xeon D-1539 | on request |
| LDS6525 6U OpenVPX Single Board Computer | Mercury Systems | United States | Processor: 4th Generation Intel® Core™ i7, quad-core processor (Haswell mob… | on request |
| LDS6527 6U OpenVPX Single Board Computer | Mercury Systems | United States | Processor: Intel Xeon D 12-core server-class SoC processor with AVX2 | on request |
| Leopard | KP Labs | Poland | Processing cores: AMD Zynq UltraScale+ MPSoC ZU6EG | ZU9EG | ZU15EG | on request |
| Lion | KP Labs | Poland | Processing Cores: Kintex Ultrascale KU060 | on request |
| MA61C cPCI | Space Products and Innovation (SPiN) | Italy | Interfaces supported: SpaceWire, I2C, CAN, RS422, RS232, MIL-STD-1553B, GPIO | on request |
| MA61C CubeSat | Space Products and Innovation (SPiN) | Italy | Interfaces supported: SpaceWire, I2C, SPI, CAN, RS422, RS485, RS232, GPIO | on request |
| MA61C SmallSat | Space Products and Innovation (SPiN) | Italy | Interfaces supported: SpaceWire, MIL-STD-1553, I2C, SPI, CAN, RS422, RS485,… | on request |
| MASTER Cubesat On-Board Computer | 2NDSpace Srl | Italy | Processor: Dual core: Cortex M7 480 MHz + Cortex M4 240 MHz | on request |
| MASTER II Next Generation Satellite OBC | 2NDSpace Srl | Italy | Architecture: Modular, separated control and computing layers | on request |
| MASTER-CHIEF Extended On-Board Computer | 2NDSpace Srl | Italy | Processor: Dual core: Cortex M7 480 MHz + Cortex M4 240 MHz | on request |
| MASTER, MASTER-CHIEF, MASTER-II Cubesat On-Board Computers | 2NDSpace Srl | Italy | Processor (MASTER): Dual core (Cortex M7 480 MHz, Cortex M4 240 MHz) | on request |
| MFCC-8558 XMC Single Board Computer with BuiltSAFE | Mercury Systems | United States | Processor: NXP QorIQ T2080 four dual threaded e6500 cores | on request |
| Mission Systems and Avionics | Tata Advanced Systems (Space) | India | — | on request |
| Modular ICU (On-Board Computer Architecture) | EREMS | France | FPGA: NG-MEDIUM | on request |
| Motherboard | SPUTNIX | Russia | Purpose: Designed for satellite control. Provides satellite stabilization. | on request |
| Motherboard (w/Raspberry-Pi, Soft, and ADCS-controller) | SPUTNIX | Russia | Purpose: Satellite control with ADCS — stabilization and target algorithm e… | on request |
| Motherboard (w/set of Sensors, Raspberry-Pi and Soft) | SPUTNIX | Russia | Purpose: Designed for satellite control. Provides satellite stabilization a… | on request |
| Motherboard Module (MBM) | Pumpkin, Inc. | United States | Price: $1,575.00 | $1 575 |
| Motherboard Module 2 (MBM2) | Pumpkin, Inc. | United States | Processor: 1 GHz ARM Cortex-A8 (BeagleBone Black) | $7 225 |
| MTE-110 Mission Timing Electronics | Innoflight | United States | Clock: Embedded Chip Scale Atomic Clock (CSAC) | on request |
| MuCore | Muon Space | United States | Architecture: Software-defined Network-on-Chip (NoC) | on request |
| Multi-Purpose Drive Electronics (MPDE) | Beyond Gravity (ex-RUAG Space) | Switzerland | Type: Two-axis stepper motor controller | on request |
| Multiband GNSS Module with Antenna M-GNSSB-ANT-RX | Arralis | Ireland | GNSS bands: GPS L1, BeiDou B1 (1560-1610 MHz) | on request |
| Multiband GNSS OEM Receiver Board M-GNSSB-RX | Arralis | Ireland | GNSS bands: GPS L1, BeiDou B1 (1560-1610 MHz) | on request |
| NanoDock DMC-3 | GomSpace | Denmark | Operating temperature: -40…+85 °C | on request |
| NanoDock SDR (MK2) | GomSpace | Denmark | Operating temperature: -20°C to +85°C | on request |
| NANOhpc-AI | SkyLabs d.o.o. | Slovenia | Standard: ISO 19683, IPC Class 3+ | on request |
| NANOhpc-DPU | SkyLabs d.o.o. | Slovenia | Standard: ISO 19683, IPC Class 3+ | on request |
| NANOhpc-obc | SkyLabs d.o.o. | Slovenia | Standard: ISO 19683, IPC Class 3+ | on request |
| NANOhpm-obc | SkyLabs d.o.o. | Slovenia | Standard: ISO 19683, IPC Class 3+ | on request |
| NANOif-2 | SkyLabs d.o.o. | Slovenia | Standard: ISO 19683, IPC Class 3+ | on request |
| NanoMind A3200 | GomSpace | Denmark | Form factor: PC104 (9.0 cm x 9.6 cm) | on request |
| NanoMind A3200 On-Board Computer | GomSpace | Denmark | Type: On-board computer (C&DH) | on request |
| NanoMind HP MK3 | GomSpace | Denmark | SoC: Xilinx Zynq 7030/7045 Programmable SoC | on request |
| NanoMind Z7000 | GomSpace | Denmark | Processor: Dual ARM Cortex A9 MPCore up to 800 MHz | on request |
| NANOobc-2 | SkyLabs d.o.o. | Slovenia | Standard: ISO 19683, IPC Class 3+ | on request |
| Nanosatellite Onboard Computer | SPUTNIX | Russia | Year of release: 2016 | on request |
| NewSpace Compact Master Reference Oscillator | Rakon Limited | New Zealand | Output frequency: 100 MHz/200 MHz | on request |
| Next Generation On Board Computer (OBC NG) | Beyond Gravity (ex-RUAG Space) | Switzerland | Core ASIC: Radiation-hardened CREOLE chip developed by Beyond Gravity | on request |
| Nexus-01 Edge-AI Onboard Computer | Akula Tech | Australia | Compute module: NVIDIA Jetson TX2i | on request |
| NOVI Space Compute and AI Infrastructure | Novi | United States | Flight heritage: Supported missions for the U.S. Air Force and the Missile … | on request |
| NxA-ECM | Aethero | United States | Processor: Nvidia AGX Thor or Orin | on request |
| NxN-ECM | Aethero | United States | Processor: Nvidia Orin NX or Nano | on request |
| NxN-ECM (Nvidia-NX/Nano Edge Computing Module) | Aethero | United States | Base processor: Nvidia Orin NX or Nano | on request |
| OBC | Space Inventor ApS | Denmark | Msrp: €9,000 | $9 000 |
| OBC PolarFire VPX | CAVU Aerospace | United Kingdom | Processor: Microchip MPFS460T-1FCG1152I / MPFS460TS-1FCG1152I (with security) | on request |
| OBC-104 | CAVU Aerospace | United Kingdom | Processor: ARM Cortex-M3 on FPGA | on request |
| OBC-64 | CAVU Aerospace | United Kingdom | Processor: PIC64-HPSC1000 / PIC64-HPSC1100 family (RISC-V vector compute) | on request |
| OBC-Cube-Polar | CAVU Aerospace | United Kingdom | Processor: Microchip PolarFire SoC Flash Based FPGA SoC | on request |
| OBC-Hyper-Polar | CAVU Aerospace | United Kingdom | Processor: RISC-V MSS: 4× 64-bit U54 application cores + 1× E51 monitor core | on request |
| OBCU-500-NS | Airbus Defence and Space | France | Integrated functions: OBC, TM/TC, GPS receiver, AOCS interfaces | on request |
| OCEOS (single core) & OCEOSmp (multicore) RTOS | O.C.E. Technology | — | Code Footprint: <10 kB (core functionality) | on request |
| ODALISS DIPP | Emxys | Spain | Connectors: 80-pins high-speed interface backplane connector. | on request |
| OmniEye | Omnipresent Robot Technologies | India | — | on request |
| On Board Computer | Alba Orbital | United Kingdom | Manufacturer: Alba Orbital | on request |
| On-board computer | SPUTNIX | Russia | Dimensions: 171 x 111 x 51 (without fasteners) mm | on request |
| On-board Computer | DSI Aerospace Technology | Austria | CPU Performance: 160 MIPS/FLOPS | on request |
| On-Board Computer (OBC) | Terma | Denmark | Processor: LEON2/3/4 (SPARC V8/V9 ISA) | on request |
| On-board computer (with a set of sensors and ADC controller) | SPUTNIX | Russia | Model: SPUTNIX SXC-MB-04-ADC | on request |
| On-Board Computers | DSI Aerospace Technology | Austria | — | on request |
| On-Board Data Handling | VECTRONIC Aerospace GmbH | Germany | Power consumption: around 1.5 W | on request |
| Onboard Computer (OBC) | EnduroSat | Bulgaria | Processor: ARM Cortex M7 | on request |
| Onboard Computer (OBC) | Dragonfly Aerospace | South Africa | Operating temperature: -10 °C to +50 °C | on request |
| Onboard Flight Computers | ZeroG Lab | China | — | on request |
| OrbitsEdge Orbital Edge Platforms and Ground-Based Development Boards | OrbitsEdge | United States | — | on request |
| ORC3990 — Space-Grade Processing SoC for Satellite Avionics | Totum Labs | United States | Device type: Radiation-tolerant System-on-Chip (SoC) | on request |
| Payload Baseboard | SPUTNIX | Russia | Purpose: Can be used for development of payload and other systems compatibl… | on request |
| Payload baseboard for platforms SXC1/3 | SPUTNIX | Russia | Model: SPUTNIX SXC-MBB-03 | on request |
| Payload Data Handling System VPDHS | VECTRONIC Aerospace GmbH | Germany | Dimensions: 290 mm x 192 mm x 34 mm | on request |
| Payload Data Handling Units | DSI Aerospace Technology | Austria | Storage Capacity: 1–8 Tbit | on request |
| Payload Electronics | Tsd-space | Italy | Pilot-d cdiu mission: Luna-25 (Luna-Glob) mission | on request |
| picoRTU system | SkyLabs d.o.o. | Slovenia | Standard: ISO 19683, IPC Class 3+ | on request |
| Pluggable Processor Module A1 (PPM A1), with TI’s MSP430F1612 | Pumpkin, Inc. | United States | SKU: 710-00485 | on request |
| Pluggable Processor Module A1 (PPM A1), with TI’s MSP430F1612 | Pumpkin, Inc. | United States | — | $655 |
| Pluggable Processor Module A2 (PPM A2), with TI’s MSP430F1611 | Pumpkin, Inc. | United States | SKU: 710-00486 | on request |
| Pluggable Processor Module A3 (PPM A3), with TI’s MSP430F2618 | Pumpkin, Inc. | United States | SKU: 710-00516 | on request |
| Pluggable Processor Module B1 (PPM B1) | Pumpkin, Inc. | United States | SKU: 710-00487 | on request |
| Pluggable Processor Module D1 (PPM D1) | Pumpkin, Inc. | United States | SKU: 710-00527 | $655 |
| Pluggable Processor Module D2 (PPM D2) | Pumpkin, Inc. | United States | SKU: 710-00528 | $655 |
| Pluggable Processor Module E1 (PPM E1) | Pumpkin, Inc. | United States | SKU: 710-00748 | $655 |
| Pluggable Socketed Processor Module B (PSPM B) | Pumpkin, Inc. | United States | SKU: 710-00607 | on request |
| Pluggable Socketed Processor Module D (PSPM D) | Pumpkin, Inc. | United States | SKU: 710-00608 | $855 |
| Pluggable Socketed Processor Module E (PSPM E) | Pumpkin, Inc. | United States | SKU: 710-00711 | $855 |
| Protoboard Module Kit | Pumpkin, Inc. | United States | SKU: 711-00303 | $100 |
| Proton2X-Box | ZIN Technologies | United States | Processor: Dual-core PowerPC | on request |
| Proton600K Multi-Core Processor | ZIN Technologies | United States | Form factor: 3U OpenVPX Single Board Computer | on request |
| ProtonVPX-Box | ZIN Technologies | United States | Backplane: High-speed 3U VPX mesh backplane, no separate SRIO switches/SpW … | on request |
| Pumpkin CubeSat Kit Motherboard Module 2 (MBM2) | Pumpkin, Inc. | United States | Hardware revision: F | on request |
| Pumpkin Motherboard Module (MBM) 2 Rev. F | Pumpkin, Inc. | United States | Operating temperature: -40 to +85 ºC | on request |
| PyCubed Plus–based Avionics Board | CubeSat Aerospace | India | Processor: STM32F765 ARM Cortex-M7, 216 MHz | on request |
| Q7 Processor | Xiphos Technologies | Canada | Processor: Xilinx Zynq SoC includes ARM dual-core Cortex-A9 MPCore processo… | on request |
| Q7S | AAC Clyde Space | Sweden | Processor: Xilinx Zynq-7000 (dual ARM Cortex-A9 + FPGA) | on request |
| Q7S Command & Data Handling Unit | AAC SpaceQuest (AAC Clyde Space subsidiary) | United States | Type: Command & Data Handling / OBC | on request |
| Q8 Computer-on-Module | Xiphos Technologies | Canada | Mpsoc: Xilinx Zynq UltraScale+ | on request |
| Q8 Low SWaP Computer-on-Module | Xiphos Technologies | Canada | Processor: Xilinx Zynq UltraScale+ Multi-Processor System-on-Chip (MPSoC) P… | on request |
| Q8 On-Board Computer | Xiphos Technologies | Canada | Processor: Xilinx Zynq SoC (ARM dual-core Cortex-A9 MPCore) | on request |
| Q8J Computer-on-Module | Xiphos Technologies | Canada | Mpsoc: Xilinx Zynq UltraScale+ | on request |
| Q8J Data Storage and Interface Board | Xiphos Technologies | Canada | Storage: 2x 1 TB SSD | on request |
| Q8J Low SWaP with GTH Computer-on-Module | Xiphos Technologies | Canada | Processor: Xilinx Zynq UltraScale+ Multi-Processor System-on-Chip (MPSoC) P… | on request |
| Q8RFG3 Gen 3 RFSoC Processor | Xiphos Technologies | Canada | Mpsoc: Xilinx Zynq UltraScale+ ZU48DR | on request |
| Q9 Versal Computer-on-Module | Xiphos Technologies | Canada | Mpsoc: AMD Versal SoC | on request |
| Remote Terminal Unit (RTU) | Beyond Gravity (ex-RUAG Space) | Switzerland | Redundancy: Fully redundant | on request |
| Resilient Space Computing Systems (NuStream, NuPod, NuComm) | Ramon.Space | Israel | Operating orbits: LEO, MEO, GEO and deep space | on request |
| RK300 Space TCXO | Rakon Limited | New Zealand | Frequency range: 10–100 MHz | on request |
| RK300NS NewSpace TCXO | Rakon Limited | New Zealand | Frequency: 80 MHz / 100 MHz | on request |
| RK409AV Ultra-Stable Space OCXO | Rakon Limited | New Zealand | Frequency: 10 MHz / 10.23 MHz / 10.24 MHz | on request |
| RK409NS NewSpace OCXO | Rakon Limited | New Zealand | Frequency range: 10–125 MHz | on request |
| RK410 High Reliability Space OCXO | Rakon Limited | New Zealand | Package size (LxWxH): 99 x 88 x 54 mm | on request |
| RK410 Space OCXO | Rakon Limited | New Zealand | Frequency range: 5–10 MHz | on request |
| RLT-ETH-x | Réaltra Space Systems Engineering | Ireland | Number of ethernet ports: Up to 4, 12, and 20 | on request |
| Robust On-Board Data Handling Unit | S4 - Smart Small Satellite Systems GmbH | Germany | Radiation protection approach: Software-based, using advanced FDIR and redu… | on request |
| Robust On-Board Data Handling Unit (OBC) | S4 - Smart Small Satellite Systems GmbH | Germany | Power consumption: < 15 mW | on request |
| ROCK-2 3U OpenVPX Mission Computer, BUILTSAFE™ | Mercury Systems | United States | Form Factor: 3U OpenVPX | on request |
| Rugged Embedded Computing for Space | Curtiss-Wright Defense Solutions | United States | Products: SBCs (VPX/VME), data acquisition, solid-state recorders, mission … | on request |
| S-A1760 Venus Space GPGPU | Aitech Systems | United States | Gpu: NVIDIA Jetson TX2i, Pascal Architecture | on request |
| S-A2300 Radiation Tolerant COTS AI Supercomputer | Aitech Systems | United States | Som: NVIDIA Jetson AGX Orin Industrial | on request |
| S930 Radiation Tolerant 3U CompactPCI Analog I/O Board | Aitech Systems | United States | ADC resolution: 12-bit | on request |
| S940 Radiation Tolerant 3U CompactPCI Digital I/O Board | Aitech Systems | United States | RS-422 output channels: 12 | on request |
| S950 | Aitech Systems | United States | Processor: High Performance PowerPC® 750FX Processor | on request |
| S992 Radiation-Tolerant 3U CompactPCI Non-Volatile Memory Board | Aitech Systems | United States | Storage capacity: 8 to 64 GB (scalable) | on request |
| S993 Radiation-Tolerant 3U CompactPCI Non-Volatile Memory Board | Aitech Systems | United States | Storage capacity: 256 GB base / up to 1 TB (8 NAND modules) | on request |
| Satellite Attitude Control Computer | MinoSpace | China | Board card size: Standard 3U | on request |
| Satellite Avionics & Power Systems | Redwire Space Belgium (ex-QinetiQ Space) | Belgium | Product family: On-board computers (OBC) | on request |
| Satellite Electronics & Avionics | BAE Systems | United Kingdom | — | on request |
| SBC-1461 | CesiumAstro | United States | TRL: 9 | on request |
| SBCFA1000 Single-Board Computer | ZIN Technologies | United States | Type: Radiation-tolerant single-board computer (OBC) | on request |
| SC-OBC Module A1 | Space Cubics Inc. | Japan | Main processor: Xilinx Artix-7 FPGA | on request |
| SC-OBC Module V1 | Space Cubics Inc. | Japan | Main processor: AMD Versal AI Edge Series VE2302 | on request |
| Scalable Compute Platform | Rogue Space Systems Corp. | United States | Flight heritage: Flight-demonstrated on OTP-2 | on request |
| SE-1 Space Edge Computer | Spiral Blue | Australia | Processing module: NVIDIA Jetson Xavier NX | on request |
| Sirius OBC LEON3FT Development Kit | AAC Clyde Space | Sweden | Processor: 32-bit LEON3FT SPARC v8 @ 50 MHz | on request |
| Sirius QuadCore | AAC Clyde Space | Sweden | TRL: 8 | on request |
| SIRIUS TCM LEON3FT DEVELOPMENT KIT | AAC Clyde Space | Sweden | Expected life: 5 years in LEO | on request |
| SIRIUS-OBC-LEON3FT | AAC Clyde Space | Sweden | Expected lifespan: 5 years in LEO | on request |
| SKAIDOCK | Zaitra | Czech Republic | Processor: AMD UltraScale+ XCZU7EG with ProASIC3 supervisor (Xiphos Q8J) | on request |
| Solid-State Recorders, Mass Memories and Payload Data Processing | Airbus Defence and Space | France | Coreci 2 flight heritage: in flight since 2021 | on request |
| SP0 Rad-Tolerant 3U CompactPCI SBC | Aitech Systems | United States | Processor: PowerQUICC-III MPC8548E @ 833 MHz, 1.0 or 1.2 GHz | on request |
| SP0-S Radiation Tolerant 3U CompactPCI SBC | Aitech Systems | United States | Processor: NXP PowerQUICC III MPC8548E | on request |
| SP1-S Aquarius™ Radiation Tolerant 3U SpaceVPX SBC | Aitech Systems | United States | Processor: NXP Layerscape LS1046A SoC | on request |
| SP240 On-Board Computer | Novi | United States | TRL: 9 (flight-proven, operational on orbit) | on request |
| Space Avionics: Payload Controller/Sequencer and Layer-3 Ethernet Switch | Arquimea | Spain | Product 1: Payload Controller/Sequencer | on request |
| SpaceTech Remote Terminal Unit (RTU) | SpaceTech GmbH | Germany | Processor: Dual Core LEON3 processor, also usable for data pre-processing | on request |
| SpaceWire-router and on-board storage device of the on-board computer complex | SPUTNIX | Russia | Dimensions: 117 x 111 x 51 (without fasteners) mm | on request |
| Sparrow OBC Node | Needronix | Poland | Type: Distributed OBC node | on request |
| SSD-2000 Solid-State Drive | Innoflight | United States | Capacity: Up to 2 TB | on request |
| SSMM | Dragonfly Aerospace | South Africa | Operating temperature: -10 °C to +50 °C | on request |
| SSTL Core | SSTL (Surrey Satellite Technology) | United Kingdom | — | on request |
| ST Engineering Spacecraft On-Board Computer (OBC) | ST Engineering Satellite Systems | Singapore | Processor: Dual-Core LEON3-FT Sparc V8 | on request |
| Sterna | EDGX | Belgium | Computational power: Up to 157 TOPS (NVIDIA Jetson Orin NX 16 GB) | on request |
| SX-SBOX Onboard Computing (Microsatellite) | SPUTNIX | Russia | Family: Onboard computing (SX-SBOX line) | on request |
| TetraPLEX | TelePIX | South Korea | Space heritage: 2024 | on request |
| TPPRE (Thruster Pointing and Pressure Regulation Electronics) | Kayser Space | Italy | Function: Xenon valve actuation and thruster pointing control | on request |
| TR-2S LEO | JAVAD GNSS | United States | Channels: 874 | on request |
| Typhoon Edge | CAVU Aerospace | United Kingdom | Processor: NVIDIA JETSON ORIN AGX Industrial & Microchip PolarFire SoC MPFS… | on request |
| Unibap iX10 Space Computer | Unibap Space Solutions AB | Sweden | Cpu: AMD Ryzen V1000 | on request |
| VVDN Aerospace & Defence Electronics Engineering | VVDN Technologies | India | Engineering disciplines: FPGA, RF, embedded SW/HW, silicon, mechanical | on request |
| Xiphos Q8RF Family | Xiphos Technologies | Canada | Operating temperature: -40 to +60 °C | on request |
| Xiphos Q9 Versal Computer-on-Module | Xiphos Technologies | Canada | Operating temperature: -40 to +60 °C | on request |
| Z7000-P4 | Space Inventor ApS | Denmark | Msrp: €18,000 | $18 000 |
| ZHP Payload Computer | Serenum Space | Czech Republic | Processor: Zynq 7015, dual-core Cortex-A9 up to 766 MHz, with FPGA | on request |
Products
Products by manufacturer
2NDSpace Srl
Italy · 2023 · 4 productsNew Space company designing modular nanosatellite/CubeSat hardware: structures, solar panels, EPS, antennas, OBCs, and deployers/separation systems.

MASTER Cubesat On-Board Computer
Dual-core CubeSat OBC with Cortex M7/M4 processors, OTA updates, FreeRTOS compatibility and rich I/O.
| Processor | Dual core: Cortex M7 480 MHz + Cortex M4 240 MHz |
| Software | OTA update, FreeRTOS-compatible architecture |
| Communication interfaces | 13x: CAN, RS422, RS485, UART, USART, I2C, SPI |
| Gpio | 8x |
| ADC inputs | 6x |

MASTER II Next Generation Satellite OBC
Next-generation modular OBC with dual-section hardware redundancy, PolarFire SoC, FPGA guardian supervision and on-demand edge AI.
| Architecture | Modular, separated control and computing layers |
| Redundancy | Dual-section (A/B), active/standby or dual-active modes |
| Failover | Hardware-driven, deterministic, no software boot required |
| Supervision | Always-on Guardian FPGA: health monitoring, watchdog, reset, power-cycling |
| Processor | PolarFire SoC with integrated FPGA fabric |

MASTER-CHIEF Extended On-Board Computer
Extended CubeSat OBC adding an independent critical-data-management core with ECC RAM to the MASTER architecture.
| Processor | Dual core: Cortex M7 480 MHz + Cortex M4 240 MHz |
| Critical data core | Independent Cortex M7 400 MHz |
| Critical data ram | 1 MB with ECC |
| Critical data program memory | 2 MB |
| Software | OTA update, FreeRTOS-compatible architecture |

MASTER, MASTER-CHIEF, MASTER-II Cubesat On-Board Computers
The MASTER series offers a range of On-Board Computers (OBCs) for CubeSats, featuring dual-core processors, various communication interfaces, and memory options. The MASTER-CHIEF p
| Processor (MASTER) | Dual core (Cortex M7 480 MHz, Cortex M4 240 MHz) |
| Ota update (MASTER) | Yes |
| Os compatibility (MASTER) | FreeRTOS compatible |
| Communication interfaces (MASTER) | 13 (CAN, RS422, RS485, UART, USART, I2C, SPI) |
| Gpio / ADC inputs (MASTER) | 8x GPIO / 6x ADC inputs |
3D Plus (HEICO)
France · 1995 · 2 productsWorld-leading manufacturer of space electronic components using proprietary 3D interconnect technology for extreme miniaturization.

COMBO – Space-Grade Configuration Memory Boot Manager
Space-grade configuration memory boot manager (3DCO0849) for AMD XQR Versal FPGAs, integrating 16 Gb RT NAND Flash for multiple large bitstreams in a 32×32 mm BGA package with on-o
| Part number | 3DCO0849 / 3DMCO0849 |
| Compatible FPGA | AMD XQR Versal |
| Nand flash capacity | 16 Gb |
| Power supply voltages | 1.2 V, 2.5 V, 3.3 V |
| Operating temperature | -40°C to +105°C |

Fusio RT Space Computer Core
Rad-hard-by-design SRAM-based FPGA computer core family with 4.4 million system gates, 128 Mbit TMR configuration memory, and optional NAND Flash and SDRAM in a single 32×32 mm BGA
| FPGA resources | 550k ASIC gate equivalents (4,400,000 system gates) |
| User i/os | 263 |
| I/o speed | Up to 800 Mbps |
| Configuration memory | 128 Mbit TMR NOR Flash |
| Nand flash (NAND/FULL) | 64 Gb |
AAC Clyde Space
Sweden · 1999 · 7 productsAAC Clyde Space provides small satellite technologies and space-based data services, offering end-to-end solutions from satellite components to data analytics for various applications.

CP400.85
The CP400.85 is a miniaturized, flight-proven processing platform with high computing power and low energy consumption, designed for CubeSat missions as a payload processor or gene
| TRL | 9 |
| Lead time | 16 Week |
| Flown since | 2018 |
| Processor | ARMv7-A |
| Clock frequency | 500 MHz |

Kryten-M3 & Kryten-M3 PLUS
The Kryten-M3 and Kryten-M3 PLUS are command and data handling solutions designed for price-sensitive commercial missions requiring reliable and qualified solutions.
| Design life | 5 years in LEO |
| Processor | SmartFusion2 SoC ARM Cortex-M3, 62.5 DMIPS |
| Clock | 50 MHz |
| Mram | 16 MB |
| Radiation (TiD) | 20 kRAD |

Q7S
The Q7S is a CubeSat Onboard Computer (OBC) designed for 'always-on' operation, offering advanced error detection and correction.
| Processor | Xilinx Zynq-7000 (dual ARM Cortex-A9 + FPGA) |
| Cpu speed | Up to 866 MHz |
| Ram | 1 GB DDR3 |
| Flash storage | 4 GB NAND |
| Operating system | Linux / FreeRTOS |

Sirius OBC LEON3FT Development Kit
The Sirius OBC LEON3FT Development Kit is designed for advanced satellite constellations in LEO and deep space exploration missions, providing 'always-on' reliable operations with
| Processor | 32-bit LEON3FT SPARC v8 @ 50 MHz |
| Sdram | 64 MB post-EDAC |
| Mass memory storage | 32 GB post-EDAC |
| Power supply | 9-15V (12 V plug included) |
| Spacewire | 50 Mbps, RMAP, 2 interfaces |

Sirius QuadCore
Sirius QuadCore is a next-generation, fault-tolerant Command and Data Handling solution combining an on-board computer, quad-core processing, and mass memory for New Space nanosate
| TRL | 8 |
| Processor | LEON4FT, 250 MHz LEON4 quad core fault-tolerant processor |
| Operating system | Linux or RTEMS real-time operating system compliant to IEEE 1754 SPARCv8 |
| Fault tolerance | TMR (Triple-Modular Redundancy) on boot flash and EDAC (Error Detection and Correction) on |
| SEE tolerance | Tolerant to Single-Event-Effects (SEE) in logic and data storage |

SIRIUS TCM LEON3FT DEVELOPMENT KIT
The SIRIUS TCM LEON3FT Development Kit is a smallsat Telemetry, Tracking and Command Control Module (TCM) designed for reliable, 'always-on' operations in LEO and deep space missio
| Expected life | 5 years in LEO |
| Processor | 32-bit LEON3FT SPARC v8 @ 50 MHz |
| Sdram | 64 MB post-EDAC |
| Mass memory storage | 32 GB post-EDAC |
| Operating temperature | -30 to +60 C |

SIRIUS-OBC-LEON3FT
The SIRIUS-OBC-LEON3FT is a flight-proven CubeSat Onboard Computer (OBC) designed for 'always-on' reliable operations in advanced satellite constellations and deep space exploratio
| Expected lifespan | 5 years in LEO |
| Processor | 32-bit LEON3FT SPARC v8 @ 50 MHz |
| Sdram | 64 MB post-EDAC |
| Nvram | 16 kB post-EDAC |
| Nand flash | 2 GB post-EDAC |
AAC SpaceQuest (AAC Clyde Space subsidiary)
United States · 1 productAAC Clyde Space provides small satellite technologies and space-based data services, offering end-to-end solutions from components to data analytics.

Q7S Command & Data Handling Unit
Compact, low-mass OBC/CDH solution for price-sensitive commercial CubeSat and SmallSat missions. Space-qualified with small size, low power.
| Type | Command & Data Handling / OBC |
| Design | Small size, low mass, low power |
| Target market | Price-sensitive commercial missions |
| Target platform | CubeSat, SmallSat (aerospace) |
| Functions | Command, telemetry, data storage, scheduling |
ACT (Advanced Cooling Technologies)
United States · 2003 · 1 productPremier thermal management solutions company specializing in custom two-phase heat transfer technology for aerospace, defense, and industrial applications.

ICE-Lok Thermally Enhanced Wedge Locks
Patented Isothermal Card Edge wedge locks that reduce card-to-chassis thermal resistance by over 33% vs. standard wedge locks, VITA 48.2 compliant with spaceflight heritage for Spa
| Thermal resistance reduction vs. COTS | > 33% |
| Temperature reduction (100 W system) | > 10°C vs. standard 3/8" wedge locks |
| Standard compliance | VITA 48.2 |
| Compatible card formats | VITA 3U, 6U, 9U |
| Ice-lok 250 series | 7, 9, 11 wedges (1/4" width) |
Aethero
United States · 5 productsAethero designs and manufactures high-performance, space-rated computers and offers compute-as-a-service for various space platforms, from CubeSats to Space Stations.

Aether Software Platform
Aethero's cloud-based fleet management and OTA software platform for managing distributed edge computing modules in space, supporting multi-modal AI/ML workloads and real-time oper
| Deployment | Cloud + Edge (cloud.aethero.com) |
| Update mechanism | OTA (Over-the-Air) |
| Os: edge | ECM-OS (headless, hypervisor/containerized) |
| Os: mcu | MCU-RTOS (real-time, minimal footprint) |
| Communication protocol | CSP (CubeSat Space Protocol) |

AMATDT
Aethero's Automated Model Annotation, Training and Deployment Tool — a software platform for customizing, training, and deploying AI/ML models onto Aethero edge computing modules,
| Deployment target | Aethero Edge Computing Modules (NxA-ECM, NxN-ECM) |
| Supported imagery types | RGB, Multispectral, Hyperspectral |
| Model customization | Flag-based configuration for detection outputs |
| Annotation | Built-in imagery annotation tool |
| Training | Automated model training pipeline |

NxA-ECM
Aethero's most powerful edge computing module based on the Nvidia AGX Thor or Orin processors, designed for high-performance spacecraft computing with 4000+ TFLOPS/TOPS and 50+ kRa
| Processor | Nvidia AGX Thor or Orin |
| Compute power | 4000+ TFLOPS/TOPS |
| Expected lifespan | 7+ years |
| Radiation tolerance | 50+ kRad TID |
| Expansion modules | 4+ available options |

NxN-ECM
Aethero's TRL-9 space-grade edge computing module based on the Nvidia Orin NX or Nano processors, supporting modular, redundant, and distributed spacecraft computing configurations
| Processor | Nvidia Orin NX or Nano |
| Compute power | 4000+ TFLOPS/TOPS |
| Expected lifespan | 7+ years |
| Radiation tolerance | 50+ kRad TID |
| Expansion modules | 4+ available options |

NxN-ECM (Nvidia-NX/Nano Edge Computing Module)
The NxN-ECM is a space-rated Edge Computing Module based on the Nvidia Orin NX or Nano, available in modular, multiple redundant, or distributed configurations for spacecraft and s
| Base processor | Nvidia Orin NX or Nano |
| Configuration options | Modular, Multiple Redundant, Distributed Computing Modules |
| Distributed computing support | Stackable or server rack format through Kubernetes clustering |
| Applications | Spacecraft, Space Data Centers, Supercomputer use cases |
| TRL | 9 |
Airbus Defence and Space
France · 2014 · 2 productsAirbus Defence and Space designs and manufactures satellites, spacecraft equipment, and provides related services for telecommunications, navigation, Earth observation, and space exploration.

OBCU-500-NS
The OBCU-500-NS is a high-performance On-Board Computer developed by Airbus Defence and Space to serve next generation LEO constellations and beyond.
| Integrated functions | OBC, TM/TC, GPS receiver, AOCS interfaces |
| Mission life | 10-year LEO rating |
| Product line | PureLine |

Solid-State Recorders, Mass Memories and Payload Data Processing
This page describes a suite of digital payload equipment for space applications, including the CORECI 2 compression, recording, and ciphering equipment, the NEMO-2 2041 compact sol
| Coreci 2 flight heritage | in flight since 2021 |
| Nemo-2 2041 heritage | over 30 years of strong flight heritage on solid-state technologies |
| User capacity | 4Tb to 12Tb |
| Input rate | 1.8 Gb/s with 6 slices |
| Real time image compression | 350 MPixels/s to 1050 MPixels/s |
Aitech Systems
United States · 16 productsDesigner and manufacturer of rugged, high-performance embedded computing solutions for aerospace, defense, and space applications.

A445 IBOX Radiation Tolerant Engine Controller
A space-qualified radiation-tolerant integrated control subsystem managing spacecraft power switching, peripheral control, engine interfaces, cameras, RF transmitters, and sensor I
| Control logic | FPGA (radiation-tolerant, user-reprogrammable) |
| Storage | Flash memory |
| Cards | Switch Card (SWC) + 2 × High Power Distribution Unit (HPDU) |
| Analog inputs | Yes |
| Thermistor inputs | Yes |

CM950 PMC Carrier Card for 3U CompactPCI SBCs
A radiation-tolerant single-slot 3U CompactPCI carrier card enabling direct connection of single-wide conduction-cooled PMC I/O modules to the SP0-S SBC, consuming less than 2 W an
| Form factor | Single-slot 3U CompactPCI |
| Power consumption | < 2 W |
| TID (Standard Flight) | 45 krad (Si) unshielded |
| TID (Optional) | 100 krad (Si) |
| Pmc accommodation | Single-wide conduction-cooled PMC |

CM951 PMC Carrier Card with Integrated MIL-STD-1553B
A radiation-tolerant single-slot 3U CompactPCI PMC carrier card combining an additional PMC site with integrated dual-redundant MIL-STD-1553B interface, consuming less than 7 W and
| Form factor | Single-slot 3U CompactPCI |
| Mil-std-1553b | Dual redundant BC/RT/MT (STANAG 3838) |
| Power consumption | < 7 W (dependent on 1553 traffic) |
| TID (Standard Flight) | 45 krad (Si) unshielded |
| TID (Optional) | 100 krad (Si) |

E193 1/2-ATR 3U VPX & CompactPCI Rugged Enclosure
A standard 1/2-ATR sealed aluminum enclosure accommodating up to four 3U OpenVPX or CompactPCI boards with internal conduction cooling, 28 Vdc MIL-STD-704 power input, and MIL-DTL-
| Form factor | 1/2-ATR, 3U |
| Board capacity | 4 × 3U boards (OpenVPX or CompactPCI) |
| Dimensions | 5" W × 6.5" L × 7" H (127 × 165 × 178 mm) |
| Power standard | MIL-STD-704 compliant |
| Connectors | MIL-DTL-38999 circular connectors |

E900 8-Slot 3U CompactPCI Space Enclosure
A cold-plate-cooled 8-slot 3U CompactPCI space enclosure with dual 28V/140W radiation-tolerant power supplies, up to 9 high-speed I/O interfaces tested to 400 Mbps, and Faraday cag
| Slot configuration | 8-slot 3U CompactPCI backplane |
| Power supplies | Dual 28V/140 W, radiation-tolerant, latch-up immune |
| Auxiliary outputs | +15 VDC, -15 VDC, +12 VDC dedicated |
| High-speed i/o | Up to 9 interfaces, tested at 400 Mbps |
| Cooling | Cold plate conduction cooling |

E905 1/2 ATR 3U CompactPCI Space Enclosure
A cold-plate-cooled 3-slot 3U CompactPCI space enclosure with a radiation-tolerant 28 Vdc/140 W power supply (>25 krad TID, >37 MeV-cm²/mg latch-up immunity), Faraday cage EM
| Slot configuration | 3-slot 3U CompactPCI |
| Power supply input | 28 Vdc / 140 W |
| Power supply efficiency | > 80% |
| Total ionizing dose (Power Supply) | > 25 krad (Si) |
| Latch-up immunity (Power Supply) | > 37 MeV-cm²/mg |

S-A1760 Venus Space GPGPU
The S-A1760 Venus is a radiation-characterized small form factor space GPGPU based on the NVIDIA Jetson TX2i with Pascal architecture, offering 256 CUDA cores, 1 TFLOPS, and 8 GB L
| Gpu | NVIDIA Jetson TX2i, Pascal Architecture |
| Cuda cores | 256 |
| Cpu | NVIDIA Denver 2 Dual-Core ARM + Cortex A57 Quad-Core ARM |
| Performance | 1 TFLOPS |
| Energy efficiency | 60 GFLOPS/W |

S-A2300 Radiation Tolerant COTS AI Supercomputer
The S-A2300 is a radiation-tolerant small form factor AI supercomputer based on the NVIDIA Jetson AGX Orin Industrial SoM with 2048 CUDA Ampere cores, 248 TOPS AI performance, and
| Som | NVIDIA Jetson AGX Orin Industrial |
| Ai performance | 248 TOPS |
| Cuda cores | 2048 (Ampere Architecture) |
| Tensor cores | 64 |
| Cpu | 12-core ARM v8.2 64-bit |

S930 Radiation Tolerant 3U CompactPCI Analog I/O Board
A radiation-hardened 3U CompactPCI analog I/O board providing 51 12-bit ADC input channels (±10V), 2 DAC output channels, 11 bus voltage monitors, and triple-voted SRAM buffers for
| ADC resolution | 12-bit |
| Analog input channels | 51 |
| ADC input range | -10 V to +10 V |
| Analog output channels | 2 × 12-bit DAC, -10 V to +10 V |
| Bus voltage monitors | 11 channels |

S940 Radiation Tolerant 3U CompactPCI Digital I/O Board
A radiation-tolerant 3U CompactPCI digital I/O board providing 12 RS-422 outputs, 4 RS-422 inputs, 2 RS-232 UART ports, 3 H-bridge torque rod interfaces, and opto-isolated discrete
| RS-422 output channels | 12 |
| RS-422 input channels | 4 |
| RS-232 UART ports | 2 |
| H-bridge torque rod interfaces | 3 (2 A rated) |
| Discrete output drivers | 2 opto-isolated |

S950
The S950 is a rugged 3U CompactPCI single board computer designed for harsh space radiation environments, offering low power consumption and high radiation tolerance for mission-cr
| Processor | High Performance PowerPC® 750FX Processor |
| Board type | Single-Slot Conduction-Cooled 3U CompactPCI Single Board Computer (SBC) |
| Operating frequency | 1 GHz |
| Power consumption | Less than 10 W |
| Total ionization dose (TID) | Greater than 15 krad (Si) (unshielded) |

S992 Radiation-Tolerant 3U CompactPCI Non-Volatile Memory Board
A radiation-tolerant 3U CompactPCI non-volatile Flash memory board providing scalable 8 to 64 GB NAND storage with hardware EDAC and PCI DMA engine, consuming less than 2 W for spa
| Storage capacity | 8 to 64 GB (scalable) |
| Memory type | Non-volatile NAND Flash |
| Nand modules | 1 to 8 individually addressable (3D-Plus) |
| Pci interface | 32-bit CompactPCI, 33.333 MHz |
| Power consumption | < 2 W nominal |

S993 Radiation-Tolerant 3U CompactPCI Non-Volatile Memory Board
A radiation-tolerant 3U CompactPCI non-volatile storage board providing 256 GB to 1 TB NAND Flash with hardware EDAC and POSIX-compliant Flash File Driver with wear leveling for hi
| Storage capacity | 256 GB base / up to 1 TB (8 NAND modules) |
| Memory type | Non-volatile NAND Flash |
| Nand modules | Up to 8 individually addressable (3D-Plus) |
| Pci interface | 32-bit CompactPCI, 33 MHz or 66 MHz |
| Error correction | Hardware EDAC (single-bit correction, double-bit detection) |

SP0 Rad-Tolerant 3U CompactPCI SBC
The SP0 is a radiation-tolerant 3U CompactPCI Single Board Computer (SBC) designed for space applications, featuring a PowerQUICC-III MPC8548E processor and low power consumption.
| Processor | PowerQUICC-III MPC8548E @ 833 MHz, 1.0 or 1.2 GHz |
| Core complex bus (ccb) speed | 333 MHz |
| Form factor | Rugged 3U CompactPCI SBC |
| Pmc site | One Standard PMC Site |
| Compliance | PICMG 2.0, Rev. 3.0 Compliant |

SP0-S Radiation Tolerant 3U CompactPCI SBC
The SP0-S is a radiation-hardened 3U CompactPCI single-board computer using the NXP PowerQUICC III MPC8548E processor at 1.0 GHz with 1 GB DDR2 ECC memory, rated to >100 krad (S
| Processor | NXP PowerQUICC III MPC8548E |
| Clock speed | 1.0 GHz |
| Core complex bus | 400 MHz |
| Memory | 1 GB DDR2 @ 400 MHz with ECC |
| User flash | 1 GB with ECC |

SP1-S Aquarius™ Radiation Tolerant 3U SpaceVPX SBC
The SP1-S Aquarius™ is a radiation-tolerant 3U SpaceVPX single-board computer powered by NXP Layerscape LS1046A (four 64-bit ARM Cortex-A72 cores at 1.8 GHz) designed for LEO, GEO,
| Processor | NXP Layerscape LS1046A SoC |
| Cpu cores | Four 64-bit ARM Cortex-A72 |
| Clock speed | 1.8 GHz |
| Memory | 4/8 GB DDR4 @ 1050 MHz with ECC |
| FPGA | Radiation-tolerant Polarfire FPGA |
Akula Tech
Australia · 2022 · 1 productMelbourne-based deep-tech startup building AI-powered smart satellites with onboard hyperspectral data processing and in-orbit AI model execution.

Nexus-01 Edge-AI Onboard Computer
Space-qualified Edge-AI onboard computer flying on the Nexus-01 mission, processing hyperspectral imagery and running AI/ML models in orbit.
| Compute module | NVIDIA Jetson TX2i |
| Cuda cores | 256 |
| Peak performance | 1.3 TFLOPS |
| Hyperspectral payload compatibility | Esper OTR-2 (250+ spectral bands) |
| Onboard ai processing | Level 0 to Level 3 hyperspectral data processing, parallel multi-model execution |
Alba Orbital
United Kingdom · 2012 · 1 productAlba Orbital manufactures PocketQube satellites, provides launch and ground station services, and operates a fleet of nighttime imaging satellites for government and commercial clients.

On Board Computer
The Alba Orbital On Board Computer (OBC) is an entry-level control hub for satellites, featuring a TI MSP430 microcontroller for low power consumption and flexibility.
| Manufacturer | Alba Orbital |
| Expected shipping time | 12-16 Weeks |
| Meets | PQ60 v1.0 Specifications |
| Dimensions | 42 mm x 42 mm |
| Mass | 8.5 grams (without memory card) |
Alpha Data Parallel Systems
United Kingdom · 1 productAlpha Data Parallel Systems manufactures FPGA cards, I/O adaptors, carrier cards, and development kits. They provide custom solutions and legacy products for various markets, including space and high-reliability development. Their products

Custom Embedded Solutions and Modified COTS Products
Alpha Data offers Modified-Commercial-Off-The-Shelf (MCOTS) services, reusing existing products and designs to provide customized solutions that meet specific customer needs with r
| Operating temperature | 0 to +55 °C |
| Storage temperature | -40 to +85 °C |
| Humidity | Up to 95% (non-condensing) |
| Altitude | Down to 1,500 feet (460 meters) below sea level Up to 60,000 feet (18,300 meters) above se |
| Vibration | Class V3 |
ALTER Technology
Spain · 1986 · 1 productALTER Technology provides laboratory and engineering services for high-reliability EEE components, specializing in microelectronics and optoelectronics engineering, procurement, assembly, and testing

Electronic Design Services
ALTER Technology provides comprehensive electronic design services from concept to manufacturing, including PCB design (FR4, IMS, flex), FPGA design, RF design, power electronics,
| PCB substrate types | FR4, IMS, flexible, rigid-flex |
| Assembly methods | Through-hole and surface-mount, selective and reflow soldering |
| Design capabilities | Analog, mixed-signal, digital, RF, high-frequency, power electronics |
| Power electronics | DC/DC and DC/AC converters |
| FPGA design | Advanced processing for automotive and aerospace |
Alén Space
Spain · 2008 · 2 productsAlén Space designs, manufactures, and operates small satellites, providing end-to-end mission development services and advanced communication platforms, subsystems, and components for space and ground

DARA OBC
Alén Space provides the DARA OBC, an essential system for the control and management of all satellite activities, designed for room optimization in small satellites.

DARA OBC — On-Board Computer
Low-power ARM Cortex-M7 OBC (TRL-9) for nanosatellites. 280 mW typical power, integrated IMU (mag + gyro + accel), GNSS, and FreeRTOS with PC/104 form factor.
| TRL | TRL-9 (Flight Heritage) |
| Processor | ARM Cortex-M7, up to 280 MHz |
| Rtos | FreeRTOS (CSP compatible) |
| Typical power | 280 mW |
| IMU — magnetometer | 3-axis digital |
Aphelion Orbitals
United States · 2017 · 1 productAphelion Orbitals is a New Jersey-based launch vehicle company developing the Helios nanosatellite launch system for regular, scheduled orbital access at low cost.

Integrated EPS/OBC Bus Module
The Aphelion Cubesat Bus Module is an integrated electrical power system and on-board computer solution designed for mission-critical, volume constrained environments.
| Mppt inputs | 5 with 40 W input capacity |
| Output rails | 7 independently controlled and monitored |
| Output capacity (5V) | 3 A |
| Output capacity (3.3V) | 4 A |
| Deployment mechanism channels | 4 dedicated for high current |
Aptos Orbital
United States · 2024 · 1 productSpace-hardened compute and communications terminal connecting satellites directly to the cloud (AWS, Azure) with 99% global coverage.

Aptos
Aptos is a space-hardened device that integrates compute, persistent communications, and cloud services into any satellite or spacecraft, enabling powerful AI onboard and 99% globa
| Years in space | 5.5 |
| Data coverage | 99% |
| TRL | 9 For LEO |
| Dimensions | 10x24x7 cm |
| Mass | 1600 g |
Argotec Srl
Italy · 2008 · 1 productArgotec is an Italian spacecraft manufacturer that designed and operates the ArgoMoon CubeSat and develops satellite platforms and subsystems for ESA and commercial missions.

FERMI OBC&DH Miniaturized Rad-Hard On-Board Computer
Miniaturized radiation-hardened on-board computer and data handling unit for microsatellite platforms, for spacecraft management and computationally intensive algorithms.
| Type | On-Board Computer and Data Handling unit (OBC&DH) |
| Radiation | Rad-hard, described by the vendor as best-in-class radiation hardening assurance |
| Target platforms | Microsatellite platforms; fitted to Argotec HAWK LITE |
| Functions | Spacecraft management, computationally intensive algorithms, data handling |
| Operating domains | Deep space and LEO |
Arquimea
Spain · 2007 · 1 productSpanish space technology company founded 2007 in Leganes, developing MEMS relay switches, SiC power devices, and miniaturized power conditioning units for satellite applications.
Space Avionics: Payload Controller/Sequencer and Layer-3 Ethernet Switch
Space-qualified payload controllers, sequencers, and a 16-port Gigabit Ethernet Layer-3 switch, developed in partnership with Ecliptic and validated in over 160 missions including
| Product 1 | Payload Controller/Sequencer |
| Product 2 | Layer-3 Gigabit Ethernet Switch (16-port GbE) |
| Flight heritage (missions) | >160 successful missions |
| Contracts since 2001 | >400 |
| Reference missions | Artemis (NASA), ISS, LEO/MEO/GEO/cislunar/lunar platforms |
Arralis
Ireland · 2 productsIrish developer of mmWave and RF/microwave MMICs, modules, phased-array antennas, and radar/comms front-end systems for satellite, aerospace and defense markets.

Multiband GNSS Module with Antenna M-GNSSB-ANT-RX
The M-GNSSB-ANT-RX is a compact integrated multiband GNSS antenna and receiver module supporting GPS L1 and BeiDou B1 with 2-3 dB antenna gain, RTK capability, UART and RS-485 inte
| GNSS bands | GPS L1, BeiDou B1 (1560-1610 MHz) |
| Antenna gain | 2-3 dB |
| Correction technology | RTK (Real-Time Kinematic) |
| Supply voltage | 3.3-5 V |
| Current consumption | 25 mA |

Multiband GNSS OEM Receiver Board M-GNSSB-RX
The M-GNSSB-RX is a compact multiband GNSS OEM receiver board supporting GPS L1 and BeiDou B1 with RTK correction capability, UART and RS-485 interfaces, and 3.3-5 V supply for def
| GNSS bands | GPS L1, BeiDou B1 (1560-1610 MHz) |
| Correction technology | RTK (Real-Time Kinematic) |
| Supply voltage | 3.3-5 V |
| Current consumption | 25 mA |
| Data interfaces | UART (3.3 V), RS-485 (5 V) |
BAE Systems
United Kingdom · 1999 · 1 productUK defense and aerospace prime with a dedicated space division; develops Azalea radar satellites and offers Space-as-a-Service payload hosting.

Satellite Electronics & Avionics
BAE Systems manufactures radiation-hardened electronics, processors, and avionics for space applications. Products include single-board computers, data processing units, inertial m
Beijing Huali Chuangtong Technology Co., Ltd.
China · 1999 · 6 productsHuali 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

A664 FPGA IP Core
The A664 IP Core is an FPGA IP unit compliant with the ARINC 664 specification, supporting 2 ARINC 664 ports with configurable 10/100/1000 Mbps port speeds. It enables fast impleme

A664 Network Analyzer
The A664 Network Analyzer is an ARINC 664 (AFDX) network data acquisition and analysis tool. It adopts a portable ruggedized laptop form factor with 4 acquisition ports supporting

A664 Signal Switch
The A664 Signal Switch is a high-performance, multi-channel, low-power real-time multi-path signal switching device. It supports switching of 8 channels of 10/100/1000 Mbps ARINC 6

A664 Stimulus/Acquisition Card
The A664 Stimulus/Acquisition Card is a high-performance ARINC 664 protocol simulation test terminal network card providing 24 ARINC 664 ports with configurable 10/100 Mbps port sp

A664 Switch (100 Mbps)
The A664 100 Mbps Switch is an 8/24-port ARINC 664 switch based on the ARINC 664 avionics bus standard. It features high reliability and real-time determinism with multiple remote

A664 Switch (Gigabit)
The A664 Gigabit Switch is an 8/16/24-port ARINC 664 switch based on the new-generation avionics bus ARINC 664 standard. It provides SFP interfaces supporting optical modules (LC c
Berlin Space Technologies
Germany · 2010 · 1 productBerlin Space Technologies (BST) designs and mass manufactures small satellite systems and technologies, providing end-to-end solutions for space missions.

CDH-110
The CDH-110 is a Command and Data Handling (CDH) system for satellite buses, comprising an On-Board Computer (OBC-110) and an Attitude Control Computer (ACC-110) in a single housin
| Data interfaces | RS422, SPI, PWM |
| Processing power | 2x90 + 400MIPS |
| Tmtc operation | Yes |
| Real time linux | Yes (HP OBC) |
| Communications security | Authentication & Encryption |
Beyond Gravity (ex-RUAG Space)
Switzerland · 1993 · 9 productsSwiss-Swedish space components manufacturer providing satellite structures, thermal control products, payload electronics, and antennas for commercial and institutional programs.

CODE+ Software Defined Drive Electronics
Software-defined drive electronics with a radiation-tolerant microcontroller, expanded sensing and in-orbit software patching.
| Architecture | Fully software-defined, radiation-tolerant microcontroller |
| Command interface | Dual UART; CCSDS command and telemetry packets |
| Optional extension boards | Signal multiplexing, MIL-STD-1553B communication interface |
| Sensing | Direct acquisition of analog and digital sensor inputs (motor current, position indicators |
| Software maintenance | In-orbit software patching |

Constellation On Board Computer (cOBC)
Fully redundant on-board computer subsystem built entirely from commercial components, with integrated GNSS receiver and platform/payload interfaces.
| Architecture | Complete subsystem based entirely on commercial components |
| Redundancy | Fully redundant, flight-proven FDIR |
| Integrated functions | On-board processing, GNSS receiver, ground communication, platform and payload interfaces |
| Optional boards | PDIO (analogue interfaces, magnetorquers, thermistors, stepper motors incl. SADE), PROPE ( |
| Frequency | 800 MHz |

Constellation Remote Terminal Unit (cRTU)
Customizable remote terminal unit bridging the on-board computer and platform electronic interfaces, based on the same COTS I/O boards as the cOBC.
| Function | Bridge between On-Board Computer and platform electronic interfaces |
| Board commonality | Same commercial I/O boards as the cOBC |
| Customization | Additional modifications and new board types available on request |
| Supply voltage | 28 V (22 V – 38 V) |
| Pulse commands number of pulses | 81 |

Core Drive Electronics (CODE)
Compact, lightweight two-axis stepper motor controller for small satellite mechanisms, built as stackable modules.
| Type | Two-axis stepper motor controller, modular and stackable |
| Motors per module | Two bipolar stepper motors, independently controlled |
| Redundancy | Two modules stacked vertically, cold redundancy |
| Power conversion | Isolated DC/DC converter with EMC filters, hardware-adjustable motor drive voltage |
| Mechanism signals | 7 additional signals per motor connector for sensors (switches, thermistors) or heaters up |

FoX Electronics Platform
3U SpaceVPX modular avionics platform (Flexible On-board avioniX) of off-the-shelf modules for LEO, MEO, GEO and cislunar missions.
| Form factor | 3U SpaceVPX modular platform |
| Target orbits | LEO, MEO, GEO and cislunar |
| Communication | Ethernet-based, supporting redundancy and high data rates |
| Applications | Spacecraft control, edge/payload processing, payload and robotics control, GNSS receiver, |
| Operating temperature | -20…+60 °C |

FoX Payload Processor
High-performance processing unit for payloads, instruments and robotics, with scalable software and gateware processing.
| Function | Control and data processing for payloads, instruments and robotics |
| Processing | Software and gateware processing, scalable to processing and storage needs |
| Platform | Part of the FoX Electronics Platform (3U SpaceVPX) |
| Mass | 3.6 kg |
| Dimensions | 148x128x217 mm3 |

Multi-Purpose Drive Electronics (MPDE)
High-performance two-axis stepper motor controller for satellite mechanisms, optimized for low micro-vibration operation.
| Type | Two-axis stepper motor controller |
| Redundancy | Two electrically identical units for cold redundancy |
| Command interface | MIL-STD-1553 TC/TM (replaceable to suit platform concept) |
| Power conversion | Isolated DC/DC converter per unit; available for different power bus voltages |
| Driven mechanisms | Antenna pointing mechanisms, solar arrays, thruster pointing mechanisms |

Next Generation On Board Computer (OBC NG)
Radiation-hardened satellite on-board computer built around the Beyond Gravity CREOLE chip with fault-tolerant SPARC V8 processor.
| Core ASIC | Radiation-hardened CREOLE chip developed by Beyond Gravity |
| Processor | Fault-tolerant SPARC V8 |
| Integrated functions | Communication functions, reconfiguration function, mass memory controller, extension possi |
| Dimensions | 283 x 242 x 278 mm |
| Mass | 9 kg |

Remote Terminal Unit (RTU)
Fully redundant remote terminal unit bridging the on-board computer and platform and payload electronic interfaces.
| Redundancy | Fully redundant |
| Function | Bridge between OBC and platform/payload electronic interfaces |
| Supported functions | Standard I/O, AOCS, propulsion |
| Form factor | 392 x 242 x 277 mm |
| Power consumption | 15 W |
CAVU Aerospace
United Kingdom · 2016 · 10 productsCAVU Aerospace designs and manufactures spacecraft avionics, including radiation-tolerant onboard computers, thermal control units, frame grabbers, and flight-proven satellite cameras for space applications.

CAVU CDH-FS
The CAVU CDH-FS is an advanced, fully redundant FPGA-based on-board computer system designed for critical space missions, offering continuous operation and resilience against sever
| Key system features | Dual Cold/Hot Redundant OBC Modules |
| Key system features (2) | Dual Cold/Hot Redundant ADC/DAC Modules |
| Key system features (3) | Double Hot Redundant ADC Converters |
| Key system features (4) | Advanced Supervisor & Health Monitoring Module |
| Key system features (5) | Efficient Data Synchronization Between OBC Modules |

CAVU OBC-1
The CAVU OBC-1 is a cutting-edge, FPGA-based satellite computing system designed for reliable and efficient operation in space, featuring intelligent redundancy and advanced comman
| Expected life-time | 3-5 years in LEO |
| Processor | Microchip/Microsemi SmartFuion2 Flash Based FPGA |
| Processor core | ARM Cortex-M3 on FPGA |
| Fpu | on FPGA Upon Request |
| Processor speed | 150 DMIPS @ 128 MHz, Max 166 MHz |

CDH-FS
Main OBC for SmallSat platform
| Memory (RAM) | 160Mbits MRAM 40 bits width (128Mbits+32Mbits ECC) |
| Memory (ROM) | 96Mbits MRAM (Configurable as Triple 32Mbits) |
| Memory (Nonvolatile Flash) | Total 24Gbit SLC NAND Flash (Triple 8G), 256K Serial FRAM, 256M Serial NOR |
| Radiation hardness (Total Ionizing Dose) | 30Krad (Si)/yr |
| Operating temperature | -40 C to +85 C |

FG-1
The FG-1 is a state-of-the-art Cubesat satellite board designed for high-quality image capture from CameraLink cameras, featuring a radiation-hardened FPGA and robust environmental
| Supply voltage | Single 12 V or 5 V and 12 V |
| Power consumption | <1 W for FG-1 Board |
| Mass | 75gr |
| Dimensions | Cubesat standard |
| Temperature | -40 C to +85 C @ 10 bar |

OBC PolarFire VPX
OBC based on PolarFire FPGA SoC in 3U VPX
| Processor | Microchip MPFS460T-1FCG1152I / MPFS460TS-1FCG1152I (with security) |
| Risc-v cores | Quad 64-bit U54 application cores + 1× E51 monitor core — >4,000 DMIPS total |
| FPGA fabric | 461k logic elements, 784 DSP blocks — flash-based, no SRAM bitstream |
| Vectorblox™ | Up to 279 GOPs INT8 (V1000 config, no TMR) / 156 GOPs with synthesised TMR |
| Serdes | 20 lanes at up to 12.7 Gbps each |

OBC-104
CubeSat OBC based in SmartFusion2
| Processor | ARM Cortex-M3 on FPGA |
| Processor (2) | Microchip/Microsemi SmartFuion2 Flash Based FPGA |
| Processor (3) | 150 DMIPS @ 128 MHz |
| Memory | 112Mbits MRAM 40 bits width (96Mbits+16Mbits ECC) |
| Memory (2) | 48Mbits MRAM (Configurable as Triple 16Mbits) |

OBC-64
OBC based on PIC-64 SOSA aligned HPSC
| Processor | PIC64-HPSC1000 / PIC64-HPSC1100 family (RISC-V vector compute) |
| Processor cores | 8× RISC-V SiFive® X280 vector cores + S7 system controller |
| Performance | ~26K DMIPS class; up to 2 TOPS (INT8) / 1 TFLOPS (bf16) |
| Memory | DDR4 ECC, up to 16 GB |
| Storage | eMMC / NAND / NOR / QSPI; MRAM/FRAM options |

OBC-Cube-Polar
CubeSat OBC based on PolarFire FPGA
| Processor | Microchip PolarFire SoC Flash Based FPGA SoC |
| Processor (2) | Quad 64-bit RISC-V on FPGA + 1 RISC-V Monitoring Core |
| Memory | RAM: 2 GB or 4 GB with ECC Protection |
| Memory (2) | MRAM: Triple 16 MB or 32 MB MRAM (Total 48 MB or 96 MB) |
| Storage | Nonvolatile Storage: 64 GB Flash via Dual 32 GB eMMC |

OBC-Hyper-Polar
OnBoard Computer based on PolarFire FPGA SoC
| Processor | RISC-V MSS: 4× 64-bit U54 application cores + 1× E51 monitor core |
| FPGA fabric | Microchip PolarFire SoC FPGA — two variants: MPFS250T (254k LE) & MPFS460T (461k LE) |
| Memory (Fabric) | DDR4 SDRAM 8 GB 72-bit ECC Enabled |
| Memory (MSS) | LPDDR4 SDRAM 4 GB 32-bit |
| Storage | Dual 256 GB eMMC |

Typhoon Edge
AI OnBorad Computer- PolarFire FPGA paired with NVIDIA Jetson
| Processor | NVIDIA JETSON ORIN AGX Industrial & Microchip PolarFire SoC MPFS460T |
| Ai performance | 248 TOPS |
| Memory | 64 GB ECC LPDDR5 |
| Memory bandwidth | 204.8 GB/s |
| Interfaces | PCIe x8, PCIe x4, CSI-2, Camera Link HS, Camera Link Base/Medium/Full, 10GbE copper, 1GbE, |
CesiumAstro
United States · 1 productUS manufacturer of software-defined, phased-array communication systems and payloads for satellite constellations, defense, and space applications.

SBC-1461
The SBC-1461 is a compact, TRL 9 single-board computer designed for LEO satellite missions, offering reliable onboard compute, data handling, and system control.
| TRL | 9 |
CONTEC
South Korea · 1 productCONTEC provides an all-in-one solution for satellite data reception, processing, and analysis, supporting space missions through its global ground station network.

Embedded Computing and OBC for Smallsats
CONTEC's compact embedded computing boards and on-board computers (OBCs) for small satellites — applying CONTEC's industrial computing expertise to space-grade satellite avionics.
| Products | Embedded SBCs, OBC modules, industrial IoT, data acquisition for space |
| Interfaces | CAN bus, UART, SPI, I2C (standard satellite protocols) |
| Space program | SSTJ nano-satellite bus (partner program) |
| Customers | JAXA, NICT, Japanese research institutions |
| HQ | Osaka, Japan (TSE Prime Market listed) |
Cosmoleap
China · 1999 · 1 productDahang Transition develops and operates medium and large reusable launch vehicles and their on-board computers, supporting satellite Internet engineering.

FLOTONE ONE
FLOTONE ONE is an on-board computer that integrates flight control, engine thrust control, and telemetry acquisition, designed with a three-mode hot backup redundancy architecture
CubeSat Aerospace
India · 1 productIndian CubeSat developer offering flight-ready 1U–6U satellite structures, subsystem components, environmental testing services, launch integration, and STEM education programs from Ahmedabad.

PyCubed Plus–based Avionics Board
The PyCubed Plus–based Avionics Board by CubeSat Aerospace is a compact, flight-ready control system designed for 1U–3U CubeSats, integrating essential subsystems like power manage
| Processor | STM32F765 ARM Cortex-M7, 216 MHz |
| Memory | 4 MB MRAM (non-volatile, radiation-tolerant) |
| Memory (2) | microSD card slot for data logging |
| Sensors | 9-axis IMU (accelerometer, gyroscope, magnetometer) |
| Sensors (2) | Sun sensor interface via solar panel FFC |
Curtiss-Wright Defense Solutions
United States · 1929 · 2 productsAmerican aerospace and defense electronics company providing rugged computing and data acquisition systems for space and defense platforms.

KAM/CSB/12U Smart Backplane Chassis
A rugged, 12-slot radiation-tolerant chassis that lets standard commercial data acquisition modules operate safely in space radiation environments, reducing the cost of space-grade
| Slots | 12 |
| Family | KAM-500 (Acra KAM-500) |
| Radiation protection | Rad-hard backplane detects and corrects Single Event Latch-Up per module |
| COTS module compatibility | 100+ standard COTS I/O plug-in modules |
| Power feature | Per-module on/off control to minimize power consumption |

Rugged Embedded Computing for Space
Curtiss-Wright Defense Solutions' rugged VPX computing boards, data acquisition systems, and mission computers for space launch vehicles and satellite applications.
| Products | SBCs (VPX/VME), data acquisition, solid-state recorders, mission computers |
| Processor families | Intel Xeon-D, NXP PowerPC (radiation-tolerant variants) |
| Bus standards | VPX (VITA 65), VME, PCIe |
| Certifications | DO-254/DO-178C available for safety-critical airborne/space |
| Applications | Launch vehicle avionics, payload data handling, SAR/EO data processing |
Data Patterns (India) Ltd.
India · 1998 · 5 productsVertically integrated Indian defence and aerospace electronics company designing and manufacturing avionics, microelectronics, RF/microwave, radar, test equipment and space systems.

Avionic Systems
Airborne LRUs and mission computers for manned and unmanned aircraft

Cockpit & Rugged Displays
Multi-function rugged LCD cockpit displays from 3 inch to 20 inch
| Display size | 3" to 20" |
| Video formats | RS170, Stanag 3350, PAL, VGA, DVI, ARINC 708, ARINC 818 |
| Interfaces | ARINC 429, ARINC 708, RS422, MIL-1553B |
| Protocols | AFDX, Ethernet, Fiber Channel, USB |

COTS Boards
Open-standard COTS modules for rugged and ATE platforms
DP-OBC-0402 On Board Computer
A rugged, PC104-form-factor On Board Computer module built around a dual-core e200 processor, providing signal processing and communication interfacing for cube/nano satellite subs
| Processor | e200 core processor, dual core |
| Core configuration | Lock-step mode or decoupled parallel mode |
| Form factor | PC104 compatible |
| Extended memory | 8 GB SD card, 2 MB external flash, 8 MB SRAM |
| Serial interfaces | 4x RS422, 2x SPI, 3x I2C |

IP & MM (Industry Pack and M-Module Modules)
A family of Industry Pack (IP) and M-Module (MM) mezzanine I/O modules compliant with ANSI-VITA 4, providing compact, ruggedised digital, communication, sensing and precision-sourc
| Dp-IP-3039 | 48 Channel Digital I/O IP Module |
| Dp-IP-3084 | 48 Channel TTL I/O IP Module |
| Dp-IP-3113 | 16 Channel Differential Digital I/O Module |
| Dp-IP-4221 | 8 Channel RS422/485 Serial Communication IP Module |
| Dp-IP-4299 | 8 Channel ARINC 429 IP Module |
Deimos Space (Indra)
Spain · 2001 · 1 productSpanish space engineering group (founded as Deimos Space, part of Elecnor 2001-2024) now operating as Indra Space, delivering end-to-end satellite platforms, avionics, ground segment, GNSS and space-surveillance solutions.

Insight4EO On-Board AI Processing
On-board artificial-intelligence processing solution for low-latency Earth observation missions.
| Processing type | On-board AI / edge processing |
| Primary applications | Maritime surveillance, emergency response, rapid Earth observation |
| Output | Autonomous, classified EO products and alerts |
Dragonfly Aerospace
South Africa · 2019 · 2 productsSouth African manufacturer of high-performance electro-optical imaging payloads and satellite platforms for Earth observation.

Onboard Computer (OBC)
High reliability, low-power flight computer with integrated AOCS interface and controller for low Earth orbit spacecraft, available exclusively as part of Dragonfly Aerospace space
| Operating temperature | -10 °C to +50 °C |
| Form factor | EuroCard 3U |
| Dimensions | 160 x 117 x 30.5 mm |
| Mass | 0.35 kg |
| Design life | Up to 8 years LEO |

SSMM
Dragonfly's SSMM is a flight-proven, high-reliability, high-speed solid-state mass memory designed for low Earth orbit spacecraft, featuring a Eurocard 3U form factor and 512 GB st
| Operating temperature | -10 °C to +50 °C |
| Form factor | EuroCard 3U |
| Dimensions | 160 x 107 x 29 mm |
| Mass | 0.35 kg |
| Design life | Up to 8 years LEO |
DSI Aerospace Technology
Austria · 5 productsDSI Aerospace Technology develops dependable electronics for space applications. They offer products such as On-board Computers, Payload Data Handling Units, Data Processing Units, Instrument Control Units, and Ground Support Equipment.

Data Processing Units
DSI Processing Units are based on advanced computing systems, including highly capable FPGAs, to provide a wide range of data processing and compute functions in-orbit.

Instrument Control Units
DSI ICUs are specialized systems designed to interface directly to a spacecraft instrument and provide control and monitoring on complex subsystems.
| Reliability | > 0.99 |
| Configurable Interfaces | SpaceWire, MIL-STD-1553B, RS422, Analogue monitoring, and more |
| Volume | Customizable |
| Power Consumption | Customizable |

On-board Computer
DSI's On-board Computers control and monitor all critical aspects of your spacecraft with a highly reliable, redundant design based on proven radiation-hardened components.
| CPU Performance | 160 MIPS/FLOPS |
| Redundancy | Cold or Hot Redundancy |
| Configurable Interfaces | SpaceWire, MIL-STD-1553B, RS422, Analogue monitoring, and more |
| Volume | from 250 × 170 × 165 mm³ (L×W×H), depending on unit |
| Power Consumption | from 15–25 W peak, depending on unit features |

On-Board Computers
On-Board Computers provide a reliable central computer for your spacecraft, with flexible interfacing and a robust and redundant CPU.

Payload Data Handling Units
DSI's PDHUs provide mass memory for spacecraft data, offering reliable, high-capacity storage and support functions like telemetry encoding and data processing.
| Storage Capacity | 1–8 Tbit |
| Data Rates | Up to 5 Gbps |
| Volume | from 260 x 133 x 224 mm³ |
| Power | from 12 W – 35 W |
Edge Aerospace
Luxembourg · 1 productDeveloper of high-performance orbital Data Processing Units (DPUs) for autonomous space operations.

E-Series: Orbital DPUs
The E-Series Orbital DPUs are high-performance Data Processing Units fully qualified for space operation, designed for reliable command & control, data handling, and AI-enabled
| Function | Command & control, data handling, AI-enabled autonomy |
| Qualification | Qualified and proven for space operation |
EDGX
Belgium · 2023 · 2 productsBelgian NewSpace company developing in-orbit edge AI computing solutions; makes the EDGX Sterna Computer — Europe's first NVIDIA-based onboard payload data processing unit for satellites.

EDGX Sterna DPU — Onboard AI Compute powered by NVIDIA
The EDGX Sterna DPU is a space-qualified, mission-ready data processing unit (DPU) for satellite onboard computing, built on NVIDIA Orin GPU technology. Europe’s first mature
| Compute architecture | NVIDIA Orin GPU |
| Radiation hardening | Mission-ready radiation hardening applied |
| First in-orbit demo | March 2026, SpaceX Transporter-16 |
| Companion software | SpaceFeather Software |
| Target orbit | LEO |

Sterna
Sterna is a flight-proven, space-hardened edge computing platform designed to provide supercomputing capabilities in orbit for ambitious satellite payloads.
| Computational power | Up to 157 TOPS (NVIDIA Jetson Orin NX 16 GB) |
| Baseline computational power | 100 TOPS (NVIDIA Jetson Orin NX 16 GB) |
| Scalable power | 10 W–40 W (Jetson Orin Nano or NX) |
| Power presets | 10 W, 15 W, 25 W, 40 W |
| Launch compatibility | Falcon 9, Ariane 6, Vega-C |
Eidel
Norway · 1966 · 1 productNorwegian space and defence electronics company specializing in telemetry, secure communications, and mission-critical instrumentation since 1966.
EIDEL Remote Interface Unit (ERIU)
Modular, high-performance interface unit bridging spacecraft buses and scientific payloads — SpaceWire/CAN/RS-422 support, FPGA hardware acceleration.
| Interfaces supported | SpaceWire, CAN bus, RS-422 |
| Processing | Dedicated FPGA hardware acceleration |
| Optional features | Encryption, on-board mass storage |
| Architecture | Modular, configurable analog/digital I/O channels |
ElmSpace
Germany · 1 productDeveloper of fluid-dynamic attitude control systems, gyroscopes, and air bearings for the space industry.

G-200 / G-510 Gyroscopes
Gyroscope product line (G-200 and G-510 models) for satellite attitude sensing applications.
| Models | G-200, G-510 |
| Mass | 12 g |
| Dimensions | 34 x 29 x 9 mm |
| Supply voltage | 3.3 V |
| Power | 0.11 W |
Emtech Space
Greece · 1 productGreek 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.

Emtech AstroCore-R Onboard Computing Platform
Radiation-supervised, AI-native onboard computing platform for satellites — processes raw satellite data into real-time in-orbit decisions.
| Radiation tolerance | Radiation-supervised design |
| Processing architecture | AI-native onboard computing |
| Function | Real-time in-orbit data processing and autonomous decision-making |
| Applications | On-orbit data reduction, anomaly detection, payload scheduling, image classification |
Emxys
Spain · 2007 · 1 productEmxys is a Spanish space electronics company specialising in advanced onboard computers, power systems, optical transceivers, and complete nanosatellite platforms for data-intensive space missions.

ODALISS DIPP
The ODALISS DIPP is a compact, high-performance Data-Intensive Payload Processor designed for satellite applications, featuring a dual-core ARM + FPGA architecture running Linux OS
| Connectors | 80-pins high-speed interface backplane connector. |
| Connectors (2) | 10-pin Pogo-style for program and debug without mechanical stress. |
| Connectors (3) | 10-pin Pogo-style for NAND flash data access. |
| Memory | eMMC NAND flash or microSD card configurable from 4 GB up to 256 GB. |
| Memory (2) | 1 GB or 512 GB DDR3L RAM. |
EnduroSat
Bulgaria · 2015 · 1 productSoftware-flexible CubeSat platforms (1U–16U+), shared-satellite hosted-payload service.

Onboard Computer (OBC)
Flight computer for SmallSats and CubeSats with 2x higher radiation resilience and ADCS-ready sensors. Low power consumption with FreeRTOS development environment and an optional i
| Processor | ARM Cortex M7 |
| Program memory | 2 |
| Mass storage | 2x 16 GB |
| Voltage supply | 12 V |
| Mass | 123 g |
EREMS
France · 1979 · 2 productsEREMS is a French SME founded in 1979, specializing in the design and realization of electronic equipment and software for high technology fields including Space.

GR740 Module (ICU CPU Module)
CPU processing module for EREMS's Modular ICU on-board computer family — GR740 processor, MIL-STD-1553/SpaceWire/CAN bus support.
| Processor | GR740 |
| Bus interfaces | MIL-STD-1553, SpaceWire, CAN |

Modular ICU (On-Board Computer Architecture)
Modular on-board computer architecture for scientific, Earth observation, exploration, and security missions — GR740 or NG-ULTRA MPSoC CPU options.
| FPGA | NG-MEDIUM |
| Cpu option 1 | GR740 microprocessor |
| Cpu option 2 | NG-ULTRA MPSoC |
| Power module | DC/DC converter (CV module) |
EXA (Astro-und Feinwerktechnik)
Germany · 1993 · 1 productGerman manufacturer of reaction wheels, CubeSat picosatellite deployers, and AOCS components for small satellites, based in Berlin-Adlershof.

ASTROFEIN GPS receiver unit- ARGO
ARGO-L1 is a configurable, redundant GPS receiver unit designed for LEO missions, offering improved solution availability through a dual independent passive receive antenna system.
| Frequency | GPS L1 Band, C/A code |
| Number of correlator channels | 12 |
| Signal acquisition threshold | 35 dB-Hz |
| Receiver startup mode ttff warm start | < 3 min (90%) |
| Receiver startup mode ttff cold start | < 15 min (90%) |
Exolaunch
Germany · 2008 · 1 productBerlin-based launch and deployment services company providing end-to-end rideshare missions, satellite integration, and proprietary separation hardware for small satellites.

EXObox
Deployment sequencer managing up to 50 satellites per unit, galvanically isolated with internal power supply; 7 missions, 132 smallsats flown.
| Maximum satellites managed per unit | 50 |
| Power supply | Internal, galvanically isolated from launch vehicle |
| Cpu redundancy | Redundant CPU and power supply |
| Telemetry | Deployment confirmation and telemetry relay (transparent transceiver) |
| Scalability | Multiple units per mission (unlimited cluster size) |
Gaisler
Sweden · 2001 · 1 productRadiation-hardened microprocessors, IP cores, and software for space and high-reliability embedded systems.

GR740
The GR740 is a radiation-hardened system-on-chip featuring a quad-core fault-tolerant LEON4FT SPARC V8 processor, an eight-port SpaceWire router, and various interfaces for space a
| TRL | 9 |
| Frequency | 250 MHz |
| Interface | PC100 SDRAM |
GAUSS Srl
Italy · 2012 · 1 productItalian company specializing in complete lifecycle management of CubeSats and NanoSatellites: design, manufacturing, subsystems, ground stations and deployers.

ABACUS On-Board Computer
General-purpose dual-core (MCU + FPGA) on-board computer for satellite and CubeSat missions with flight-proven heritage.
| Cores | Two cores (MCU MSP430 and FPGA Spartan-3E) directly interconnected with a 24-line bus |
| Mcu | MSP430 EP series, 16-bit RISC MCU, up to 25 MHz, HiRel Enhanced Product (Texas Instruments |
| Analog i/o | 10x 3.3 V analog input; up to 45x digital GPIO channels |
| Gpio | 16x voltage-level-shiftable GPIOs with interrupt features |
| Com ports | 4x COM ports (one also RS422/485, Full or Half Duplex) |
GomSpace
Denmark · 2007 · 6 productsGomSpace is a Danish CubeSat manufacturer producing satellite platforms, subsystems, and end-to-end mission solutions. Products include the NanoCom radio modules, NanoPower EPS, and complete 1U–12U satellite platforms. GomSpace has one of t

NanoDock DMC-3
The NanoDock DMC-3 is designed to carry up to four GomSpace daughterboards or up to two daughterboards while also providing mounting and interfacing for a GPS receiver.
| Operating temperature | -40…+85 °C |
| Dimensions | 91.9 x 88.7 x 8.6 mm |

NanoDock SDR (MK2)
The GomSpace NanoDock system provides a flexible system for configuring a satellite, allowing multiple functional subsystems to be mounted on a single PC104 type dock board.
| Operating temperature | -20°C to +85°C |
| Storage temperature | -20°C to +85°C |
| Mass | 74.2 g |
| Frequency | 40 MHz |
| Interface | MicroSD card, USB to UART, RS422, I2C, CAN |

NanoMind A3200
The NanoMind A3200 is a highly miniaturized on-board computer designed for seamless integration with GomSpace NanoDock platforms and diverse space missions.
| Form factor | PC104 (9.0 cm x 9.6 cm) |
| Mcu | AVR32 with power-saving capabilities |
| Flash memory | 512 KB built-in flash, 128 MB NOR flash (2 x 64 MB dies) |
| Fram | 32 kB for configuration storage |
| Sdram | 32 MB |

NanoMind A3200 On-Board Computer
GomSpace on-board computer that seamlessly integrates with the NanoDock platform ecosystem for CubeSat command and data handling.
| Type | On-board computer (C&DH) |
| Integration | GomSpace NanoDock platform compatible |
| Protocol | CSP (CubeSat Space Protocol) |
| Application | CubeSat command and data handling |
| Clock frequency | 8 MHz to 64 MHz |

NanoMind HP MK3
The NanoMind HP MK3 is a powerful On-board computer designed for high-performance, efficient on-board processing and hardware acceleration functions to meet the demands of complex
| SoC | Xilinx Zynq 7030/7045 Programmable SoC |
| Processor | Dual ARM Cortex A9 MPCore, up to 800 MHz |
| FPGA module | 125K / 350K logic cells |
| Volatile Memory | 1024 MB DDR3 (512 MB with ECC enabled) |
| Non-volatile memory | 256 MB NOR flash, 70 GB eMMC (pSLC), 233 GB eMMC (MLC) |

NanoMind Z7000
The NanoMind Z7000 is a powerful ARM/FPGA onboard computer designed for space applications, featuring a dual ARM core running Linux and a flexible FPGA for payload data processing.
| Processor | Dual ARM Cortex A9 MPCore up to 800 MHz |
| FPGA | 125k logic cells |
| RAM | 1 GB DDR3 |
| Storage | 32 GB |
| Operating System | Linux |
Hongqing Technology (鸿擎科技)
China · 2021 · 1 productBeijing satellite constellation company partnered with Blue Arrow Aerospace; develops communications, remote sensing, and science satellites plus in-house Jinwu propulsion, Chiyu power, and Baize electronics subsystems.

Baize Integrated Electronics System
The Baize Integrated Electronics System is Hongqing Technology onboard satellite avionics platform, serving as the mission commander for all satellite operations. It integrates att
| Functions | Attitude control, power management, thermal control, telemetry/telecommand, health monitor |
| Architecture | Highly integrated single-board avionics platform |
| Software | Advanced software architecture with in-orbit reconfiguration support |
| Health monitoring | Autonomous anomaly detection and corrective action |
| In-orbit reconfiguration | Supported |
ibeos
2013 · 1 productIbeos designs and manufactures satellite electronics, including processors, single board computers, and electric power subsystems, for LEO, GEO, and beyond missions.

EDGE-1100
The EDGE-1100 is a radiation-tolerant payload processor built on AMD Ryzen technology, offering impressive processing power and versatility for space missions.
| Processing Power | 1.1 TFLOPS (2 TFLOPS single precision) |
| CPU | Quad-core, 8-threaded x86 |
| GPU Cores | 512 |
| Form Factor | 3U SpaceVPX |
Innoflight
United States · 2004 · 7 productsInnoflight, Inc. is a US-based aerospace electronics company headquartered in San Diego, California, developing advanced software-defined radios (SDR), cryptographic communication systems, and flight computers for small satellites, CubeSats

CFC-400XS Compact Flight Computer
CubeSat compact flight computer with defense-grade Xilinx UltraScale+ MPSoC, CyberDog software suite and Linux reference design, flying since 2021.
| Processor board | Defense-grade Xilinx UltraScale+ MPSoC (GPP + FPGA) |
| Supervisor board | Radiation tolerant, implementing radiation mitigation techniques |
| Daughter card interfaces | Low + medium + high speed serial; 3x-8x 1000Base-T (GbE) Ethernet |
| Software | CyberDog Software Suite, Linux reference design; on-orbit re-programmable |
| Applications | C&DH, payload interface and data processing, BMC3 |

CFC-405XP / CFC-450XP Compact Flight Computer
3U VPX compact flight computer with defense-grade Xilinx UltraScale+ MPSoC, five gigabit Ethernet ports and serial interfaces, flying since 2025.
| Processor board | Defense-grade Xilinx UltraScale+ MPSoC (GPP + FPGA) |
| Supervisor board | Radiation tolerant, implementing radiation mitigation techniques |
| Interfaces | Ethernet 5x 1000Base-T (GbE); serial RS-422, LVDS, UART |
| Software | CyberDog Software Suite, Linux reference design; on-orbit re-programmable |
| Form factor | 3U VPX module 171 x 100 x 25 mm |

CFC-510P Compact Flight Computer
GPU-based 3U VPX flight computer on AMD Ryzen with CUDA runtime environment, 539 g and 40 W max, flying since 2025.
| Processor board | AMD Ryzen GPU |
| Supervisor board | Radiation tolerant, implementing radiation mitigation techniques |
| Software | CyberDog Software Suite, Linux reference design, CUDA runtime environment |
| Heritage platform | CFC-500S / CFC-500P (NVIDIA Tegra K1 GPU) |
| Form factor | 3U VPX module 171 x 100 x 25 mm |

CFC-600P Compact Flight Computer (AI/ML)
AI/ML flight computer on defense-grade AMD Versal AI Edge adaptive SoC, 3U VPX, 500 g, 70 W max.
| Processor board | Defense-grade AMD Versal AI Edge adaptive SoC |
| Supervisor board | Radiation tolerant, implementing radiation mitigation techniques |
| Software | CyberDog Software Suite, Linux reference design; on-orbit re-programmable |
| Applications | AI/ML, C&DH, mission data processor, payload interface electronics, BMC3 |
| Form factor | 3U VPX module 172 x 100 x 25 mm |

IOI-8 Input/Output Interfaces Module
3U VPX Ethernet I/O module with four 2.5GBase-T and four 1000Base-T ports, 501 g and 7 W.
| Interfaces | 4x 2.5GBase-T (2.5 GbE), 4x 1000Base-T (GbE) |
| Form factor | 3U VPX module 171 x 100 x 24 mm |
| Mass | 501 g |
| Power | 7 W |
| TRL / mrl | 9 / 10 |

MTE-110 Mission Timing Electronics
CubeSat timing unit with embedded chip scale atomic clock (CSAC) and radiation-tolerant IA design, 250 g at 3 W.
| Clock | Embedded Chip Scale Atomic Clock (CSAC) |
| Design | Radiation tolerant Information Assurance (IA) |
| Control | 2x RS-422 UART |
| Inputs | 2x RS-422 PPS (Red), typically GPS receivers |
| Outputs | 3x LVDS PPS (Red), 8x LVDS PPS (Black), 2x RS-422 PPS (Black), 8x LVDS 10 MHz (Black) |
SSD-2000 Solid-State Drive
3U VPX solid-state storage module with up to 2 TB, dual PCIe m.2 SSDs at 1300 MB/s read and 500 MB/s write.
| Capacity | Up to 2 TB |
| Drives | 2x PCIe m.2 SSDs |
| Read speed | 1,300 MB/s |
| Write speed | 500 MB/s |
| I/o | Through VPX backplane |
Institute of Aeronautical Engineering
India · 1 productThe Institute of Aeronautical Engineering (IARE) in Hyderabad is a specialized engineering institution with a core focus on aeronautical and aerospace engineering. IARE offers cutting-edge programs in aerospace systems, avionics, and satell
IARE Aerospace Systems Laboratory
The IARE Aerospace Systems Laboratory at the Institute of Aeronautical Engineering conducts research in aerospace systems, avionics, and satellite technology, supporting developmen
| Type | Research Laboratory |
| Specialization | Aeronautical and Aerospace Systems |
| Institution | IARE Hyderabad |
| Country | India |
JAVAD GNSS
United States · 2007 · 1 productAmerican GNSS technology company manufacturing high-precision positioning receivers for surveying, geodesy, and machine control applications.
TR-2S LEO
The TR-2S LEO is a USA-built GNSS board specifically designed for Low Earth Orbit (LEO) applications, manufactured by JAVAD GNSS.
| Channels | 874 |
| Memory | 64 GB |
| Interfaces | Ethernet, USB, serial, IRIG time codes, external frequency in/out, CAN, 1PPS/event marker |
| Antenna inputs | 1x (3S/3SW), 2x (DI/DIW), 4x (QM) |
Kayser Space
Italy · 1986 · 2 productsKayser Space designs, manufactures, integrates, and tests hardware and platforms for space programs, supporting over 100 missions and microgravity research.

Instrument Control Unit (ICU)
Space-qualified central electronic architecture interfacing spaceborne scientific instruments with the host spacecraft — modular design for automated or crew-assisted operations.
| Functions | Power distribution, command handling, data acquisition, communications interface |
| Design | Modular — adapts to automated or crew-assisted operations |

TPPRE (Thruster Pointing and Pressure Regulation Electronics)
Electronics subsystem controlling electric propulsion thruster pointing and Xenon pressure regulation — hot/cold redundancy, double-failure-tolerant for deep-space missions.
| Function | Xenon valve actuation and thruster pointing control |
| Redundancy | Hot/cold redundancy, double-failure-tolerant |
| Interfaces | Xenon Pressure Regulator Unit, Thruster Pointing Mechanisms |
KP Labs
Poland · 2016 · 4 productsPolish space AI company developing advanced on-board data processing solutions for satellites, enabling real-time AI-powered Earth observation and mission autonomy in orbit.

Antelope
Antelope is an advanced data processing unit designed to enable AI capabilities for CubeSats, delivering real-time processing and AI-driven analysis for autonomous satellite missio
| Size | 13.24 x 95.9 x 90.1 mm |
| Form factor | PC-104 |
| Mass | Around 130-150 g |
| Processing cores | Zynq UltraScale+ MPSoC ZU3/4/5CG: • Dual ARM Cortex-A53 CPU up to 1.5 GHz • Dual ARM Corte |
| Interfaces | CAN, I2C, GPIO, SPI, RS422/485, UART, GPS PPS, LVDS or GTH transceivers, USB 3.0, USB 2.0, |

Antelope Advanced Data Processing Unit
PC-104 CubeSat data processing unit with AMD Zynq UltraScale+ MPSoC, 160 GOPS, 4-8GB DDR4 ECC, enabling onboard AI and signal processing at ~130g with CAN/SpaceWire/Ethernet interf
| Processor | AMD Zynq UltraScale+ MPSoC (ZU2/3/4/5 variants) |
| Cpu cores | Quad ARM Cortex-A53 @ up to 1.5 GHz + Dual Cortex-R5 |
| FPGA | Included (programmable fabric) |
| Performance | 160 GOPS |
| Ram | 4-8 GB DDR4 with ECC |

Leopard
Leopard is a flight-proven Data Processing Unit supporting the full payload data handling chain on-board, designed for Edge AI in micro and mini satellites.
| Processing cores | AMD Zynq UltraScale+ MPSoC ZU6EG | ZU9EG | ZU15EG |
| CPU | Quad ARM Cortex-A53 1.2 GHz |
| FPGA | for custom function implementation |
| PS-DDR4 Memory | 16 GiB (with ECC) |
| Boot flash | 64 MB (NOR) with TMR |

Lion
Lion is a backplane-based DPU in ADHA 3U form factor designated to satellites up to 600 kg, designed for ESA Mission Class III and IV.
| Processing Cores | Kintex Ultrascale KU060 |
| Supervising Circuit | Gaisler GR716B |
| Memory | 16 GiB DDR4 with ECC, 1 GB bitstream storage |
| Backplane Interfaces | ADHA Extended Peripheral module or ADHA Peripheral Module, 4x SpaceWire + 4x SpaceFiber on |
| Front Panel Interfaces (Baseline) | 4x SpaceWire + 8x SpaceFiber |
LiquidCool Solutions
United States · 2006 · 1 productTotal 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.

LCS MiniNODE Industrial Computing System
IP67-sealed fanless industrial PC with immersion cooling — AMD Ryzen 5, 32 GB DDR4, 1 TB NVMe, no AC/water needed, 0°C–45°C, for harsh environments including space, defense, oil &a
| Cpu | AMD Ryzen 5 5600G (6C/12T, 4.4 GHz boost) |
| Memory | 32 GB DDR4 2933 MHz (64 GB max) |
| Storage | 1 TB M.2 NVMe |
| IP rating | IP67 sealed |
| Dimensions | 16″ W × 18″ D × 4.5″ H |
Mercury Systems
United States · 9 productsMercury Systems delivers end-to-end processing ecosystems for aerospace and defense systems. They provide signal, compute, data management, display, and secure products. They have supported over 75 different spacecraft missions, including e

CCM3012 3U OpenVPX I/O Carrier Board
The EnsembleSeries™ CCM3012 is a compact, 3U OpenVPX PMC/XMC carrier that provides processor modules high-bandwidth access to additional mezzanine sites via PCIe Gen 3 interfaces.
| PMC-X sites | 1 |
| PCI support | 33 and 66 MHz |
| PCI-X support | 66, 100, and 133 MHz |

CCM6020 6U OpenVPX I/O Carrier Board
The EnsembleSeries™ CCM6020 PMC/XMC carrier module expands processing module capabilities by providing high-bandwidth access to additional mezzanine sites.
| PMC/XMC sites | 2 |
| PCI support | 33 and 66 MHz |
| PCI-X support | 66, 100, and 133 MHz |
| Interface | I2C |

GSC6203 6U OpenVPX GPGPU Coprocessing Board
The EnsembleSeries GSC6203 accelerator is a 4th generation 6U OpenVPX module powered by dual NVIDIA Pascal GPUs, with field-proven deployments in commercial and defense programs.
| GPU | Dual NVIDIA Pascal P5200E MXM |
| Cores | 5120-cores |
| TFLOPS | 17.8 TFLOPS |
| Memory | 32 GB GDDR5 |
| Bandwidth | 230 GB/s |

HDS6603B 6U OpenVPX, SOSA-aligned, Multiprocessing Board
The EnsembleSeries™ HDS6603B is a 6U OpenVPX multiprocessing server blade powered by dual Intel® Xeon® E5 processors with Mellanox ConnectX-3 40 Gb/s Ethernet or InfiniBand switch
| Processors | Dual Intel 2.2 GHz 10-core or 1.8 GHz 14-core Xeon (Broadwell) server-class processors |
| SDRAM | Up to 64 GB DDR4-2133 SDRAM (per processor), 128 GB planned (for 256 GB total blade memory |
| Switch Fabrics | 40 Gb/s Ethernet or InfiniBand high switch fabrics |
| PCIe | Gen3 PCIe coprocessing and I/O expansion plane communications |
| Environmental Protection | MOTS+ extreme environmental protection |

LDS3517 3U OpenVPX Single Board Computer
The EnsembleSeries™ LDS3517 is a 3U OpenVPX single board computer (SBC) that delivers high performance signal and mission processing capability.
| Main processor | Intel 8-core, 64 bit, Xeon D-1539 |
| FPGA | Xilinx UltraScale XCKU095 |
| System Memory | 16 GB DDR4-2133 |
| OpenVPX messages | VITA 48.1 Air-cooled |

LDS6525 6U OpenVPX Single Board Computer
The EnsembleSeries™ LDS6525 6U OpenVPX single board computer integrates Intel Core i7 processing, serial RapidIO or 10 Gigabit Ethernet data paths, and dual mezzanine sites for sca
| Processor | 4th Generation Intel® Core™ i7, quad-core processor (Haswell mobile class) |
| Switch Fabrics | Software defined FPGA Gen2 Serial RapidIO®, 10 GbE |
| PCIe Switching | Integrated Gen3 PCIe switching for on/off-board coprocessing |
| Mezzanine Sites | XMC and XMC/PMC |
| Environmental Protection | MOTS+ extreme environmental protection |

LDS6527 6U OpenVPX Single Board Computer
The EnsembleSeries™ LDS6527 6U OpenVPX single board computer provides scalable computing for electronic warfare, radar, IMINT, sensor fusion, and AI applications.
| Processor | Intel Xeon D 12-core server-class SoC processor with AVX2 |
| Memory | Up to 32 GB DDR4 |
| Switch Fabrics | Mellanox CX-3 bridged Ethernet or InfiniBand high bandwidth |
| Mezzanine Sites | 1x XMC and 1x XMC/PMC |
| Environmental Protection | MOTS+ extreme |

MFCC-8558 XMC Single Board Computer with BuiltSAFE
The MFCC-8558 with BuiltSAFE™ technology is a DAL-C safety-certifiable single board computer designed for aerospace and defense applications.
| Processor | NXP QorIQ T2080 four dual threaded e6500 cores |
| Memory | 4 GB DDR3L at 14.4 GB/s peak with ECC protection |
| Flash EPROM | 4 GB (NAND), 512 MB (NOR) |
| NVRAM | 256 KB FRAM |
| PCIe Gen2 on XMC-P6 | 3x x1 |

ROCK-2 3U OpenVPX Mission Computer, BUILTSAFE™
The ROCK-2 3U OpenVPX mission computer is designed for space constrained mission-critical applications requiring flight-safety certification, offering comprehensive and reusable De
| Form Factor | 3U OpenVPX |
| Certifiability | DO-178C/DO-254 up to DAL-A |
| Processors | Up to 4x QorIQ™ T2080 or Optional Intel® Core™ i7 or Xeon® |
| Cooling | Sealed, conduction-cooled |
| Operating Temperature | -40°C to +70°C |
MinoSpace
China · 2017 · 1 productChinese commercial satellite manufacturer building Earth observation, communications, and remote sensing satellites, plus payloads, components, and ground terminal systems.

Satellite Attitude Control Computer
A 3U board-sized attitude control computer for small satellites (50-200kg) that handles attitude information acquisition, adjustment, and control.
| Board card size | Standard 3U |
| Suitable for satellite weight | 50-200 kg |
Motiv Space Systems
United States · 2014 · 1 productMotiv Space Systems designs and builds space robotics, motor controllers, and mechanisms, including the robotic arm on NASA's Mars 2020 Perseverance rover.

BRAVO-II Motor Controller
The BRAVO-II is a dual-axis motor controller card designed for space applications, supporting BLDC and 3-axis stepper motors with current, velocity, and position control.
| Axis | Dual Axis Motor Controller Card |
| Motor support | BLDC / 3-Axis Stepper |
| Control | Current, Velocity, & Position |
| Motor velocity | 500-10,000 RPM (typ) |
| Environment | GEO |
Muon Space
United States · 2021 · 1 productMuon Space is the Mission Foundry, designing, building, and operating high-performance satellite constellations for defense, civil, and commercial customers.

MuCore
Software-defined instrument core built on a Network-on-Chip architecture for flexible, high-bandwidth sensor data processing.
| Architecture | Software-defined Network-on-Chip (NoC) |
| Signal processing | Parallel signal processing chains (GNU Radio-like compute blocks) |
| Sensor compatibility | Flexible interfacing with a wide variety of high-performance sensor hardware |
| Data routing | Routes processed data to various communication interfaces for downlink or cross-spacecraft |
N7 Space
1 productN7 Space provides embedded software development and MBSE solutions for the space industry, specializing in on-board software for satellites and offering related services and toolchains.
ICE Cube — On-Board Computer Unit (OBCU)
Radiation-tolerant on-board computer unit for CubeSats — LEON3 SPARC V8 processor, RTEMS RTOS, SpaceWire and CAN interfaces, developed for ESA/CERN ICE Cube experiment.
| Processor | LEON3 SPARC V8 |
| Os | RTEMS |
| Interfaces | SpaceWire, CAN |
| Radiation tolerance | Radiation-tolerant memory and logic |
| Program | ESA/CERN ICE Cube (ISS experiment) |
NanoAvionics
Lithuania · 2014 · 1 productPre-integrated nanosatellite buses (3U–16U+ MP42), green chemical propulsion, mission integration.

CubeSat Payload Controller
Dedicated payload controller / on-board data storage module for CubeSat experiments.
| Type | Payload data / control unit |
| Function | Power switching, data acquisition, storage |
| Flight heritage | 60+ satellites launched, 300+ in production (per nanoavionics.com) |
Needronix
Poland · 2017 · 1 productPolish smallsat hardware company designing and manufacturing components and subsystems for CubeSats and small satellites, serving commercial and institutional space customers across Europe.

Sparrow OBC Node
Miniature on-board computer (OBC) node for CubeSat satellite bus — distributed computing architecture, RTOS support, low power, compatible with Needronix ADCS and communications pr
| Type | Distributed OBC node |
| Os support | RTOS |
| Functions | Command/data handling, payload interface, housekeeping |
| Compatibility | Needronix Cormorant, Eagle, ADCS ecosystem |
Novi
United States · 2020 · 2 productsAmerican space technology company developing satellite systems and space infrastructure solutions.

NOVI Space Compute and AI Infrastructure
NOVI offers space compute and AI infrastructure, including flight-proven On-Board Computers (OBCs), Mission-as-a-Service, and GENIEedge™ smart satellites, enabling advanced computi
| Flight heritage | Supported missions for the U.S. Air Force and the Missile Defense Agency |
| TRL | 9 (for NOVI’s satellites and its SP240 On-Board Computer) |
SP240 On-Board Computer
Flight-proven (TRL 9) radiation-tolerant on-board computer for smallsats, incorporating the VORAGO microcontroller for on-orbit AI and software processing at the space edge.
| TRL | 9 (flight-proven, operational on orbit) |
| Microcontroller | VORAGO (radiation-tolerant) |
| Capability | On-orbit edge AI inference and software processing |
| Flight heritage | ISS, SpaceX Transporter-12 and prior missions |
| Supported programs | US Air Force, Missile Defense Agency |
NTC Module
1 productNTC Module (АО «НТЦ «Модуль») — Russian space industry enterprise, Moscow. Its products listed on NewSpace Market come from the Glavkosmos export catalogue.

Integrated Circuit 1879 VM8Y
28 nm CMOS heterogeneous computing microcircuit with ARM Cortex-A5 core for real-time video, radar and neural-network processing.
| Package type | HFCBGA-1444 |
| Supply voltage | Core 0.9 V; CMOS I/O 1.8 V; DDR3 I/O 1.5 V |
| Dynamic current consumption | CMOS buffers: 3 A (UCC1=1.98 V); DDR3 buffers: 3.8 A (UCC2=1.60 V) |
| Operating temperature | -60°C to +85°C |
| Technology | CMOS 28 nm |
O.C.E. Technology
1 productOCE Technology designs and manufactures high-reliability embedded software, hardware, and satellite subsystems for challenging applications, with heritage on Chinese satellites.

OCEOS (single core) & OCEOSmp (multicore) RTOS
OCEOS and OCEOSmp are real-time operating systems developed to meet ESA's evolving requirements for existing and new System-on-Chips, offering deterministic behavior and robust per
| Code Footprint | <10 kB (core functionality) |
| Supported Architectures | SPARC, ARM, RISC-V |
| Certification | ESA ECSS Category B standard |
| Multicore Certification | RISC-V Microchip PolarFire®, SPARC LEON4 E698PM, ARM Cortex-A9 HISAOR AI SOC |
Omnipresent Robot Technologies
India · 2010 · 1 productIndian deep-tech company building autonomous space, aerial and robotic systems, including SAR satellites, onboard edge-computing payloads and AI perception software for defense and commercial use.
OmniEye
Onboard satellite edge-computing module for real-time data fusion and analytics.
OrbitsEdge
United States · 2018 · 1 productOrbitsEdge is a Cocoa Beach, Florida-based company developing ruggedized, flight-qualified edge computing platforms that bring high-performance data processing and AI inference directly into orbit.
OrbitsEdge Orbital Edge Platforms and Ground-Based Development Boards
OrbitsEdge delivers high-performance, ruggedized compute systems for spacecraft, enabling real-time data processing and AI inference in orbit, alongside ground-based development bo
Pumpkin, Inc.
United States · 1995 · 25 productsSan 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.

Breakout Board Module
A CubeSat Kit development module that breaks out all bus I/O, USER and MHX signals to headers compatible with common logic analyzers and protocol analyzers.
| SKU | 711-00380 |
| Price | $255.00 |
| Classification | Development Hardware |
| Breakout signals | 48 I/O signals (IO.[47..0]), 8 USER[7..0] signals, MHX signals, -RESET |
| Protocol analyzer header | 10-pin breakout header for I2C/SPI protocol analyzers |

CubeSat Kit Upgrade to C8051
A hardware-and-software upgrade bundle that adds Silicon Labs C8051F120 development and flight capability to an existing CubeSat Kit.
| SKU | 711-00717 |
| Includes | Pluggable Socketed Processor Module B (PSPM B) with C8051F120; Pluggable Processor Module |
| Required toolchain | Keil PK51 Professional Developer's Kit (purchased separately) |
| Hardware/software class | Development Hardware | Development Software | Flight Hardware | Flight Qualified | Space P |
| Purchase restriction | Available only to customers who have already purchased a CubeSat Kit |
CubeSat Kit Upgrade to dsPIC33
A software and hardware upgrade package adding Microchip dsPIC33FJ256GP710 support to an existing CubeSat Kit purchase, for customers who originally bought a Kit with a different p
| SKU | 711-00719 |
| Price | $5,455.00 per item |
| Hardware/software classification | Development Hardware | Development Software | Flight Hardware | Flight Qualified | Space P |
| Included component | Pluggable Socketed Processor Module D (PSPM D) with dsPIC33FJ256GP710 |
| Included component (2) | Pluggable Processor Module D2 (PPM D2) |
CubeSat Kit Upgrade to MSP430
A hardware-and-software upgrade bundle that adds Texas Instruments MSP430 development and flight capability to an existing CubeSat Kit.
| SKU | 711-00716 |
| Includes | MSP-TS430PM64 Adapter with MSP430F2618/F1612/F1611; Pluggable Processor Module A3 (PPM A3) |
| Required toolchain | CrossWorks for MSP430 (Rowley Associates), purchased separately |
| Hardware/software class | Development Hardware | Development Software | Flight Hardware | Flight Qualified | Space P |
| Purchase restriction | Available only to customers who have already purchased a CubeSat Kit |
CubeSat Kit Upgrade to PIC24 (PIC24FJ256GA110)
A software and hardware upgrade package adding Microchip PIC24FJ256GA110 support to an existing CubeSat Kit purchase, for customers who originally bought a Kit with a different pro
| SKU | 711-00718 |
| Price | $5,455.00 per item |
| Hardware/software classification | Development Hardware | Development Software | Flight Hardware | Flight Qualified | Space P |
| Included component | Pluggable Socketed Processor Module D (PSPM D) with PIC24FJ256GA110 |
| Included component (2) | Pluggable Processor Module D1 (PPM D1) |
CubeSat Kit Upgrade to PIC24 (PIC24FJ256GB210)
A software and hardware upgrade package adding Microchip PIC24FJ256GB210 support to an existing CubeSat Kit purchase, for customers who originally bought a Kit with a different pro
| SKU | 711-00795 |
| Price | $5,455.00 per item |
| Hardware/software classification | Development Hardware | Development Software | Flight Hardware | Flight Qualified | Space P |
| Included component | Pluggable Socketed Processor Module E (PSPM E) with PIC24FJ256GB210 |
| Included component (2) | Pluggable Processor Module E1 (PPM E1) |

Development Board (DB)
Pumpkin CubeSat Kit module that hosts a Pluggable Processor Module (PPM) to form a low-power 8- or 16-bit MCU/DSC command-and-data-handling (C&DH) module for a CubeSat.
| SKU | 710-00297 |
| Price | $1,710.00 |
| Bus interface | CubeSat Kit Bus standard, 104-pin connector |
| Compatible processor modules | PPM A1, PPM A2, PPM A3, PPM B1, PPM D1, PPM D2, PPM E1 |
| Ordering restriction | A la carte orders require prior purchase of a complete CubeSat Kit |

Development Board 2 (DB2)
A simple development tool board for CubeSat modules conforming to the 104-pin CubeSat bus standard, used to characterize power requirements and support testing of CubeSat Kit-compa
| Bus connectors | Two interconnected 104-pin CubeSat bus connectors with M3 standoffs |
| Module stacks supported | Two |
| Debug header | 10-pin header for Total Phase I2C host adapters/protocol analyzers (I2C, first SPI bus sig |
| Power bus test points | Four pairs red/black banana jacks (plus a fifth pair reserved for EPSM 1) |
| USB debug adapter mounting | Mounting hole pattern provided in a corner of the DB2 |

I/O LED Module
A CubeSat Kit development module that visually displays the status of all 48 bus I/O lines on LEDs for at-a-glance monitoring during integration and test.
| SKU | 710-00521 |
| Price | $360.00 |
| Classification | Development Hardware |
| I/o signals monitored | 48 (IO.[47..0]) |
| Signal buffering | Every I/O signal buffered |

Motherboard Module (MBM)
Pumpkin's flagship flight on-board computer carrier module: combined with a Pluggable Processor Module it forms a low-power 8- or 16-bit MCU/DSC command-and-data-handling (C&DH
| Price | $1,575.00 |
| Hardware classification | Flight Hardware | Flight Qualified | Space Proven |
| Module height | 0.600 in (15.24 mm) |
| Bus interface | CubeSat Kit Bus standard, 104-pin connector |
| Type options | Stackthrough, Non-Stackthrough |

Motherboard Module 2 (MBM2)
1 GHz ARM Cortex-A8 Linux on-board computer module for CubeSats with 4.5× UARTs, I2C, SPI, Ethernet, RS-422, and 104-pin CubeSat Kit bus.
| Processor | 1 GHz ARM Cortex-A8 (BeagleBone Black) |
| Operating system | Linux |
| Programming languages | C, C++, Python, Perl, Rust |
| Uarts | 4.5× |
| Gpio | 6× |

Pluggable Processor Module A1 (PPM A1), with TI’s MSP430F1612
Flight-qualified, space-proven pluggable command-and-data-handling processor module built around TI's MSP430F1612 16-bit MCU, for use with the CubeSat-compatible Motherboard Module
| SKU | 710-00485 |
| Mcu | TI MSP430F1612, 16-bit |
| Internal flash memory | 55KB |
| Internal ram | 5KB |
| Clock speed | 7.3728 MHz |

Pluggable Processor Module A1 (PPM A1), with TI’s MSP430F1612
The Pluggable Processor Module A1 (PPM A1) is a component for CubeSat Kits, featuring TI's MSP430F1612 processor.

Pluggable Processor Module A2 (PPM A2), with TI’s MSP430F1611
Flight-qualified, space-proven pluggable command-and-data-handling processor module built around TI's MSP430F1611 16-bit MCU, for use with the CubeSat-compatible Motherboard Module
| SKU | 710-00486 |
| Mcu | TI MSP430F1611, 16-bit |
| Internal flash memory | 48KB |
| Internal ram | 10KB |
| Clock speed | 7.3728 MHz |

Pluggable Processor Module A3 (PPM A3), with TI’s MSP430F2618
Flight-qualified, space-proven pluggable command-and-data-handling processor module built around TI's MSP430F2618 16-bit MCU, for use with the CubeSat-compatible Motherboard Module
| SKU | 710-00516 |
| Mcu | TI MSP430F2618, 16-bit |
| Internal flash memory | 116KB |
| Internal ram | 8KB |
| Clock speed | 7.3728 MHz |

Pluggable Processor Module B1 (PPM B1)
Flight-qualified, space-proven pluggable command-and-data-handling processor module built around Silicon Labs' C8051F120 8-bit MCU, for use with the CubeSat-compatible Motherboard
| SKU | 710-00487 |
| Mcu | Silicon Labs C8051F120, 8-bit, soldered in place |
| Internal flash memory | 128KB |
| Internal ram | 8,848B |
| Max clock speed | 100 MHz |

Pluggable Processor Module D1 (PPM D1)
Flight-qualified, space-proven CubeSat Kit processor module for the Motherboard Module (MBM), built around a soldered Microchip PIC24FJ256GA110 microcontroller.
| SKU | 710-00527 |
| Price | $655.00 per item |
| Hardware classification | Flight Hardware | Flight Qualified | Space Proven |
| Processor | Microchip PIC24FJ256GA110 (16-bit MCU, soldered) |
| Internal flash memory | 256 KB |

Pluggable Processor Module D2 (PPM D2)
Flight-qualified, space-proven CubeSat Kit processor module for the Motherboard Module (MBM), built around a soldered Microchip dsPIC33FJ256GP710 Digital Signal Controller.
| SKU | 710-00528 |
| Price | $655.00 per item |
| Hardware classification | Flight Hardware | Flight Qualified | Space Proven |
| Processor | Microchip dsPIC33FJ256GP710 (16-bit DSC, soldered) |
| Internal flash memory | 256 KB |

Pluggable Processor Module E1 (PPM E1)
Flight-qualified, space-proven CubeSat Kit processor module for the Motherboard Module (MBM), built around a soldered Microchip PIC24FJ256GB210 microcontroller.
| SKU | 710-00748 |
| Price | $655.00 per item |
| Hardware classification | Flight Hardware | Flight Qualified | Space Proven |
| Processor | Microchip PIC24FJ256GB210 (16-bit MCU, soldered) |
| Internal flash memory | 256 KB |

Pluggable Socketed Processor Module B (PSPM B)
A socketed development version of Pumpkin's C&DH processor module built around Silicon Labs' C8051F120 8-bit MCU, for use with the CubeSat-compatible Development Board (DB).
| SKU | 710-00607 |
| Mcu | Silicon Labs C8051F120, 8-bit, in 100-pin ZIF socket |
| Internal flash memory | 128KB |
| Internal ram | 8,848B |
| Max clock speed | 100 MHz |

Pluggable Socketed Processor Module D (PSPM D)
A pluggable, socketed processor module for the CubeSat Kit Development Board, built around a Microchip PIC24FJ256GA110 MCU or dsPIC33FJ256GP710 DSC in a user-replaceable ZIF socket
| SKU | 710-00608 |
| Price | $855.00 per item |
| Hardware classification | Development Hardware |
| Processor options | Microchip PIC24FJ256GA110 (16-bit MCU) or Microchip dsPIC33FJ256GP710 (16-bit DSC) |
| Socket | 100-pin ZIF (Zero Insertion Force) socket |

Pluggable Socketed Processor Module E (PSPM E)
A pluggable, socketed processor module for the CubeSat Kit Development Board, built around a Microchip PIC24FJ256GB210 MCU in a user-replaceable ZIF socket, with built-in USB.
| SKU | 710-00711 |
| Price | $855.00 per item |
| Hardware classification | Development Hardware |
| Processor | Microchip PIC24FJ256GB210 (16-bit MCU) |
| Socket | 100-pin ZIF (Zero Insertion Force) socket |

Protoboard Module Kit
A prototyping PCB module for the CubeSat Kit that lets engineers wire through-hole components into circuitry connected to the CubeSat Kit Bus Connector.
| SKU | 711-00303 |
| Price | $100.00 per item |
| Category | Prototyping Hardware |
| Grid pitch | 0.100" |
| Plated holes | roughly 500 |

Pumpkin CubeSat Kit Motherboard Module 2 (MBM2)
A CubeSat Kit-compatible motherboard module designed to host a BeagleBone Black (BBB) single-board computer, serving as an on-board computer for nanosatellites and similar equipmen
| Hardware revision | F |
| Height | 0.600” |
| Bus connector | 104-pin CubeSat Kit™ Bus |
| Footprint | PC/104-size |
| Uarts on csk bus connector | 4.5x |

Pumpkin Motherboard Module (MBM) 2 Rev. F
A motherboard module designed to interface a BeagleBone Black (BBB) processor with a CubeSat Kit (CSK) bus, providing various I/O options and power management.
| Operating temperature | -40 to +85 ºC |
| Voltage on +5v_usb bus | -0.3 to +6 V |
| Voltage on +5v_sys bus | -0.3 to +6 V |
| Voltage on vcc_sys bus | -0.3 to +3.6 V |
| Voltage on local vcc bus | -0.3 to +3.6 V |
Rakon Limited
New Zealand · 1967 · 8 productsGlobal leader in frequency control and timing solutions — space-qualified oscillators, GNSS receivers and S-band transceivers — with 40+ years of flight heritage.

ESCC3503001 Space Clock Oscillator (XO)
ESCC Qualified Parts List (QPL) space clock oscillator (4–100 MHz) for mission-critical satellite timing with −55 to +110°C operating range.
| Frequency range | 4–100 MHz |
| Frequency stability | ≤±30–40 ppm |
| Operating temperature | −55 to +110°C |
| Dimensions | 16 × 16 × 3.8 mm |
| Package | SMD |

NewSpace Compact Master Reference Oscillator
A compact Master Reference Oscillator (MRO) designed for NewSpace constellations, generating and distributing highly stable and reliable frequency signals for telecommunications, n
| Output frequency | 100 MHz/200 MHz |
| Overall frequency stability (2 years) | ±50 ppb |
| Overall frequency stability (12 years) | ±200 ppb |
| Output power | 9 dBm |
| Typical phase noise @100 mhz (@10 Hz) | -100 dBc/Hz |

RK300 Space TCXO
Hi-Rel space temperature-compensated crystal oscillator (10–100 MHz, ≤±0.5–5 ppm) for satellite frequency reference applications.
| Frequency range | 10–100 MHz |
| Frequency stability | ≤±0.5–5 ppm over temperature |
| Dimensions | 20 × 20 × 13 mm |
| Type | TCXO (Temperature-Compensated Crystal Oscillator) |
| Product class | Hi-Rel Space |

RK300NS NewSpace TCXO
NewSpace TCXO at 80 and 100 MHz with ±2–4 ppm stability for small satellite and CubeSat frequency reference.
| Frequency | 80 MHz / 100 MHz |
| Frequency stability | ±2–4 ppm |
| Type | TCXO (NewSpace grade) |
| Product class | NewSpace |
| Supply voltage | 5 V |

RK409AV Ultra-Stable Space OCXO
Ultra-stable space OCXO at 10/10.23/10.24 MHz with 2.5×10⁻¹³ Allan deviation at 1s for navigation satellite and scientific mission timing.
| Frequency | 10 MHz / 10.23 MHz / 10.24 MHz |
| Frequency stability | 10⁻⁹ |
| Allan deviation | 2.5×10⁻¹³ @ 1s averaging time |
| Dimensions | 60 × 60 × 32 mm |
| Type | Ultra-Stable OCXO |

RK409NS NewSpace OCXO
NewSpace OCXO with 10–125 MHz range and ±1–1000 ppb frequency pulling for LEO constellations and CubeSat timing.
| Frequency range | 10–125 MHz |
| Frequency pulling range | ±1–1000 ppb |
| Type | OCXO (NewSpace grade) |
| Product class | NewSpace |
| Target applications | LEO constellations, CubeSats, small satellites |

RK410 High Reliability Space OCXO
MIL/ECSS-qualified space oscillator with 10^-10 stability class, used operationally by international space agencies for decades.
| Package size (LxWxH) | 99 x 88 x 54 mm |
| Nominal frequency | 5 to 10 MHz |
| Stability class | 10^-10 |
| Operating temperature | 0 to 60 C / -20 to 60 C / -30 to 60 C (variants) |
| Allan deviation (ADEV) | 1-10s: 2 x 10^-13 |

RK410 Space OCXO
High-reliability space-qualified oven-controlled crystal oscillator (5–10 MHz) with 10⁻¹⁰ stability for precision satellite timing.
| Frequency range | 5–10 MHz |
| Frequency stability | 10⁻¹⁰ |
| Phase noise | −122 dBc/Hz @ 1 Hz offset |
| Dimensions | 99 × 88 × 54 mm |
| Type | OCXO (Oven-Controlled Crystal Oscillator) |
Ramon.Space
Israel · 2004 · 1 productIsraeli developer of space-resilient, radiation-tolerant onboard computing infrastructure — AI/DSP processors, storage and communication processors that turn satellites into software-defined, autonomous systems.

Resilient Space Computing Systems (NuStream, NuPod, NuComm)
Ramon.Space offers a platform of resilient space computing systems, including NuStream (Storage System), NuPod (Edge Compute System), and NuComm (Communication Processor), designed
| Operating orbits | LEO, MEO, GEO and deep space |
| Core technology | Vertically integrated |
| Architecture | Modular and scalable |
| Software | In orbit SW upgrades |
| Storage | High-density |
Redwire Space Belgium (ex-QinetiQ Space)
Belgium · 1988 · 1 productBelgian satellite systems facility in Kruibeke, formerly QinetiQ Space nv, acquired by Redwire Space in 2022; delivers entire satellites, avionics, and the International Berthing and Docking Mechanism (IBDM).

Satellite Avionics & Power Systems
Redwire Space Belgium’s Kruibeke facility designs and manufactures satellite avionics hardware, including on-board computers (OBC), power control and distribution units (PCDU
| Product family | On-board computers (OBC) |
| Product family (2) | Power control and distribution units (PCDU) |
| Product family (min) | Remote terminal units (RTU) |
| Application | Small satellites and satellite platforms |
| Facility | 450 m² ISO7 and 250 m² ISO8 cleanrooms, Kruibeke, Belgium |
Rogue Space Systems Corp.
United States · 2020 · 1 productUS builder of autonomous orbital robots (Orbots) for proximity operations, satellite inspection, in-space compute, and orbital logistics, headquartered in Laconia, New Hampshire.

Scalable Compute Platform
The Scalable Compute Platform (SCP) is a low-SWaP, flight-demonstrated flexible compute layer for spacecraft, providing a full Linux high-performance computing environment for onbo
| Flight heritage | Flight-demonstrated on OTP-2 |
| Third generation scp ai performance | 248 TOPS |
| Third generation scp launch | Q1 2027 aboard the OTP-2B mission |
Réaltra Space Systems Engineering
Ireland · 2017 · 1 productIrish space-electronics company designing and manufacturing ruggedized avionics and telemetry systems for launch vehicles and space missions.

RLT-ETH-x
The RLT-ETH-x is a series of high-performance Ethernet switches designed for harsh space environments, simplifying complex distributed systems by managing critical and non-critical
| Number of ethernet ports | Up to 4, 12, and 20 |
| Delivery jitter | Below 1 microsecond |
| Mass | 2.19 Kg |
| Dimensions | 243.0 x 80.0 x 97.0 mm |
| Power Consumption | 23.6 W |
S4 - Smart Small Satellite Systems GmbH
Germany · 2017 · 2 productsGerman manufacturer (Wuerzburg) of pico/nanosatellite subsystems and tailored small satellite systems, with flight heritage tracing back to the first German pico-satellite UWE-1.

Robust On-Board Data Handling Unit
A radiation-tolerant On-Board Data Handling (OBDH) unit that uses software-based fault protection and commercial components, offering standard UNISEC bus interfaces for satellite i
| Radiation protection approach | Software-based, using advanced FDIR and redundancy |
| Component type | Commercial (COTS) chips |
| Flight heritage | More than 5 years without any interruption of service in polar LEO |
| Bus interface | Standard UNISEC bus electrical interfaces |
| Momentum | 2.0 mNms |

Robust On-Board Data Handling Unit (OBC)
Ultra-low-power, dual-redundant 16-bit RISC on-board computer for CubeSats with flight heritage since 2013.
| Power consumption | < 15 mW |
| Power supply | 3.3 V |
| Backup power supply | 3.3-9 V |
| Mass | 38 g |
| Dimensions | 90 x 90 x 6.9 mm |
Saturn Satellite Networks
United States · 2017 · 1 productSatellite hardware company developing MiniGeoSat and Nationsat platforms, along with software-defined radio and shared-launch programs for affordable GEO and regional satellite missions.
Andromeda: Guidance, Navigation & Control (GNC) Software
Andromeda is a spacecraft Guidance, Navigation & Control (GNC) software developed by Saturn Satellite Networks, compatible with any CPU running a real-time operating system.
| Compatible orbits | GEO, MEO, LEO |
| Cpu compatibility | Any CPU running a real-time operating system |
| Included features | Fully operational Space environmental model |
| Testing | Extensively tested |
| Flight heritage | Scheduled to fly on a LEO mission in 2025 |
Saturn Space
United States · 2017 · 1 productSaturn Satellite Networks (SSN) Inc. is a US-based space technology company that designs and manufactures reliable, affordable satellites for GEO, MEO, and LEO applications.
Andromeda: Guidance, Navigation & Control (GNC) Software
Andromeda is a spacecraft Guidance, Navigation & Control (GNC) software developed by Saturn Satellite Networks, compatible with any CPU running a real-time operating system.
| Compatible orbits | GEO, MEO, LEO |
| Cpu compatibility | Any CPU running a real-time operating system |
| Included features | Fully operational Space environmental model |
| Demonstrated platform | Arduino Nano ESP32 running FreeRTOS |
| Flight heritage | Scheduled to fly on a LEO mission in 2025 |
Serenum Space
Czech Republic · 2020 · 1 productSERENUM 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.

ZHP Payload Computer
High-performance, power-efficient Zynq 7015-based payload computer with FPGA, SpaceWire, Ethernet, and PCIe Gen2 for CubeSats.
| Processor | Zynq 7015, dual-core Cortex-A9 up to 766 MHz, with FPGA |
| Form factor | 95.0 x 90.0 mm |
| High-speed interfaces | SpaceWire (up to 200 Mbps), 1 Gbps/100 Mbps Ethernet, PCIe Gen2 x4 |
| Pc/104 connector | 2x CAN, I2C, power, PPS (configurable in/out) |
| Peripheral interfaces | USB 2.0 (OTG), 3x RS-422/485, SPI, UART, I2C, JTAG/serial debug |
Sidus Space, Inc.
United States · 2012 · 1 productUS space and defense technology company (NASDAQ: SIDU) building the LizzieSat multi-mission satellite platform, AI/ML edge-computing avionics, and precision satellite manufacturing services from its Florida Space Coast facilities.

Fortis™ VPX
Fortis™ is a mission-ready VPX module designed for command and data handling, AI-driven processing, and advanced navigation, supporting complex mission requirements from developmen
| System components | SSBC (Quad-Core ARM, rad-hard PolarFire FPGA, 8 GB DDR4), PNT module, SDR (S/X-band), Feat |
| I/o | LVDS 4x SpaceWire + Camera Link, Ethernet 4x 1GbE + 2x 10GbE, USB 3.1 Gen1, UART 14x RS-42 |
| Power input | 28VDC/12 A, 330 W max |
| Operating temperature | -55 C to +125 C |
| Dimensions | 3U OpenVPX-SOSA |
SkyLabs d.o.o.
Slovenia · 2013 · 7 productsSkyLabs 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.

NANOhpc-AI
High-performance, power-efficient AI accelerator extension for NANOhpc-obc using dual Hailo-8 accelerators.
| Standard | ISO 19683, IPC Class 3+ |
| TRL | 5 |
| Mait | In-house |
| Ai extension ai technology | Dual Hailo-8 accelerator |
| Performance | Up to 52 TOPS |

NANOhpc-DPU
High-performance reconfigurable data processing unit extension for NANOhpc-obc, built around AMD Zynq UltraScale+ MPSoC.
| Standard | ISO 19683, IPC Class 3+ |
| TRL | 5 |
| Mait | In-house |
| Dpu extension ai technology | AMD Zynq UltraScale+ MPSoC ZU7EV |
| FPGA fabric | 504K system Logic Cells |

NANOhpc-obc
64-bit high-performance multicore RISC-V on-board computer for AI@Edge and demanding LEO applications.
| Standard | ISO 19683, IPC Class 3+ |
| TRL | 9 |
| Mait | In-house |
| Main cpu cluster | 4x RISC-V 64-bit processors @ max 600 MHz |
| Supervisor | RISC-V monitoring core @ max 600 MHz |

NANOhpm-obc
High-performance MCU-based fault-tolerant on-board computer.
| Standard | ISO 19683, IPC Class 3+ |
| TRL | 9 |
| Mait | In-house |
| Processor | NOEL-V 32-bit core (RV32IMAFD) with FPU |
| Memory | 256 MB DDR3 (EDAC protected) |

NANOif-2
Intelligent remote terminal unit with unified TM/TC interface for satellite sensors, instruments and payloads.
| Standard | ISO 19683, IPC Class 3+ |
| TRL | 9 |
| Mait | In-house |
| User interfaces | 2x CAN (with CSP bridge), 5x RS422, 24x ADC, 28x GPIO (8 with remapping to SPI, I2C, UART) |
| Interfaces | Redundant CAN for TM/TC |

NANOobc-2
Fault-tolerant second-generation on-board computer for mission-critical satellite operation.
| Standard | ISO 19683, IPC Class 3+ |
| TRL | 9 |
| Mait | In-house |
| Processor | PicoSkyFT 8/16-bit core with single precision FPU |
| Code memory | 4 MB MRAM (EDAC protected) |

picoRTU system
Highly modular remote terminal unit system for LEO small and micro satellite missions.
| Standard | ISO 19683, IPC Class 3+ |
| TRL | 7 |
| Mait | In-house |
| Bus interface | Redundant CAN (ISO 11898-2), CANopen per ECSS-E-ST-50-15C |
| Discrete user interfaces | Compliant with ECSS-E-ST-50-14C specifications |
Space Cubics Inc.
Japan · 2018 · 2 productsJAXA-affiliated Japanese venture (Sapporo, founded 2018) designing FPGA-based onboard computers for CubeSats and small satellites, with flight heritage on ISS Kibo and lunar landers.

SC-OBC Module A1
CubeSat on-board computer on a Xilinx Artix-7 FPGA with Zephyr RTOS, 70 x 70 x 9.6 mm, 30 g, 2.0 W max, built on JAXA-derived technology.
| Main processor | Xilinx Artix-7 FPGA |
| Main cpu | Cortex-M3 / MicroBlaze-V |
| Preinstalled os | Zephyr RTOS |
| Communication interface | CAN, I2C, UART |
| FPGA user i/o | 38 pin |

SC-OBC Module V1
High-end space-grade on-board computer on the AMD Versal AI Edge VE2302 adaptive SoC, with rad-tolerant 4 GB DDR4 ECC, 64 GB eMMC, 100 x 150 mm, 110 g.
| Main processor | AMD Versal AI Edge Series VE2302 |
| Application processor | Dual core Arm Cortex-A72 up to 1.3 GHz (48/32 KByte L1 with parity and ECC, 1 MByte L2 wit |
| Real-time processor | Dual core Arm Cortex-R5F up to 600 MHz (32/32 KByte L1, 256 KByte TCM with ECC) |
| Ai engine | AI Engine-ML tiles 34; AIE/AIE-ML data memory 17 Mbit; AIE-ML shared memory 68 Mbit |
| Programmable logic | System logic 328,720; LUTs 150,272; DSP engines 464; block RAM 5.4 Mbit; UltraRAM 43.6 Mbi |
Space Inventor ApS
Denmark · 2015 · 2 productsSpace Inventor ApS is a Danish second-generation NewSpace company providing non-ITAR CubeSat, nanosat, and microsat components, platforms, and turnkey satellite missions with full vertical integration, headquartered in Aalborg with offices

OBC
Quad-core ARM Cortex-M7 onboard computing platform for redundant mission-critical satellite functions.
| Msrp | €9,000 |
| Architecture | Four independent ARM Cortex-M7 modules |
| Operating system | FreeRTOS |
| Redundancy | Hot/cold redundancy across four independent modules |

Z7000-P4
Versatile payload and onboard computing platform based on a dual-core ARM Cortex-A9 SoC with integrated FPGA logic.
| Msrp | €18,000 |
| Processor | Dual-core ARM Cortex-A9 MP-Core with NEON SIMD |
| FPGA logic | 125K programmable cells |
| Interfaces | LVDS/SpaceWire, up to 1 Gb Ethernet, CAN, RS-422, I2C |
| Data storage | Up to 64 GB eMMC |
Space Products and Innovation (SPiN)
Italy · 2015 · 3 productsSPiN (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

MA61C cPCI
Plug-and-play Command and Data Handling system integrating multiple subsystems with a cPCI Serial Space processing unit; candidate backplane for ESA/EC Copernicus missions.
| Interfaces supported | SpaceWire, I2C, CAN, RS422, RS232, MIL-STD-1553B, GPIO |
| Form factor | cPCI Serial Space |
| Processor | GR712RC dual-core 32-bit LEON3-FT SPARC V8 |
| Memory | 64 Mbit SRAM, 64 Mbit FLASH |
| Host interface | USB (API + Windows GUI included) |

MA61C CubeSat
Plug-and-play Command and Data Handling (C&DH) unit for CubeSats, based on the PC/104 standard, with flight heritage (TRL 9).
| Interfaces supported | SpaceWire, I2C, SPI, CAN, RS422, RS485, RS232, GPIO |
| Mechanical standard | PC/104 |
| Processor | GR712RC dual-core 32-bit LEON3-FT SPARC V8 |
| Memory | 64 Mbit SRAM, 64 Mbit FLASH |
| Host interface | USB (API + Windows GUI included) |

MA61C SmallSat
Plug-and-play Command and Data Handling (C&DH) unit for small satellites, adding MIL-STD-1553 support for higher-complexity missions.
| Interfaces supported | SpaceWire, MIL-STD-1553, I2C, SPI, CAN, RS422, RS485, GPIO |
| Processor | GR712RC dual-core 32-bit LEON3-FT SPARC V8 |
| Memory | 64 Mbit SRAM, 64 Mbit FLASH |
| Host interface | USB (API + Windows GUI included) |
| Supply voltage | +5 V to 24 V |
Spacemanic s.r.o.
Slovakia · 2017 · 3 productsSlovak-Czech full-service nanosatellite mission provider offering CubeSat platforms (1U-16U), onboard subsystems, rideshare launch integration, and ground segment services.

CELESTE GNSS Receiver
CELESTE is a compact, multi-constellation GNSS receiver designed for small satellite applications, offering high accuracy and various interface options.
| Operating temperature | -40°C to +85°C |
| Dimensions | 67 x 42 x 7.5 mm |
| Mass | 25 g |
| Power supply | 3.3 V |
| Power supply (for CAN) | 5 V |

Deep Thought
Deep Thought is a compact, flight-proven on-board computer designed for small satellites, offering robust processing capabilities, extensive interfaces, and integrated sensors.
| Operating temperature | -40°C to +85°C |
| Dimensions | 67 x 42 x 7.5 mm |
| Mass | 25 g |
| Power supply | 3.3 V |
| Power consumption | 330 mW (average) |

EDDIE
EDDIE is a compact, low-power on-board computer module designed for space applications, featuring an MSP430 microcontroller, FreeRTOS, and a variety of interfaces.
| Operating temperature | -40°C to +85°C |
| Dimensions | 67 x 42 x 7.5 mm |
| Mass | 25 g |
| Power supply | 3.3 V |
| Power supply (2) | 5 V (for CAN) |
SpaceTech GmbH
Germany · 2004 · 1 productGerman space company designing, developing and producing solar arrays, laser-optical instruments and space electronics for satellite missions.

SpaceTech Remote Terminal Unit (RTU)
cPCI-Serial-Space based Remote Terminal Unit collecting data from avionic sensors and controlling avionic actuators.
| Processor | Dual Core LEON3 processor, also usable for data pre-processing |
| Onboard connection | CAN-Bus or SpaceWire |
| IO architecture | Standardized IO-module based on cPCI-Serial-Space standard |
| Pt1000 interface | 28 channels |
| Analogue voltage input | 8 channels |
Spiral Blue
Australia · 2021 · 1 productAustralian space technology company building LiDAR and AI edge computing systems for LEO satellites.

SE-1 Space Edge Computer
Most powerful commercially available satellite edge computer (outside a space station) — NVIDIA Jetson Xavier NX, reduces raw data downlink by up to 99.7%. 10 units in orbit since
| Processing module | NVIDIA Jetson Xavier NX |
| Orbit | LEO |
| First operational date | April 2023 |
| Units in orbit | 10 |
| Data reduction demonstrated | 99.7% (1,004 MB to 3.063 MB) |
SPUTNIX
Russia · 2011 · 11 productsSPUTNIX is a Russian manufacturer of nanosatellite and microsatellite platforms, onboard subsystems and ground infrastructure, operating as a subsidiary brand of Sitronics Group.

CubeSat OBC / ADCS Motherboard SXC-MB-04-ADC
Raspberry Pi CM3+ carrier board with integrated ADCS controller, magnetometer, gyroscope, EM coil driver, temperature sensor, RTC, and 3-channel power switch. CAN bus throughout.
| Form factor | PC/104 |
| Computer | Raspberry Pi CM3/CM3+ |
| ADCS | Integrated standalone controller |
| Interfaces | CAN, SPI, I2C, UART, USB 2.0, Ethernet |
| Connectivity | WiFi hotspot/client module |

Motherboard
A Raspberry Pi Compute Module carrier board for satellite control, integrating ADCS sensors, an EM torquer driver and an onboard ADCS controller on a CAN bus architecture.
| Purpose | Designed for satellite control. Provides satellite stabilization. |
| Year of release | 2017 |
| Design life | 1 years |
| Lead time | 2 months |
| Flight qualification of the product | Yes |

Motherboard (w/Raspberry-Pi, Soft, and ADCS-controller)
Raspberry Pi Compute Module nanosatellite OBC+ADCS carrier (60 g, CAN/I2C/SPI/UART, -40 to +60 °C) with integrated ADCS controller.
| Purpose | Satellite control with ADCS — stabilization and target algorithm execution, three-axis ori |
| Year of release | 2018 |
| Design life | 1 year |
| Lead time | 2 months |
| Flight qualification | Not yet flight qualified |

Motherboard (w/set of Sensors, Raspberry-Pi and Soft)
A Raspberry-Pi Compute Module carrier board with integrated sensors and ADCS controller, designed for satellite control and stabilization.
| Purpose | Designed for satellite control. Provides satellite stabilization and target algorythms per |
| Year of release | 2017 |
| Design life | 1 years |
| Lead time | 2 months |
| Flight qualification of the product | No |

Nanosatellite Onboard Computer
An onboard computer for nanosatellites that collects sensor data, processes measurements, stores results, forms control actions, and processes telecommands/telemetry.
| Year of release | 2016 |
| Design life | 1 year |
| Lead time | 6 months |
| Flight qualification of the product | No |
| Possibility to adapt the product to customer requirements | Yes |

On-board computer
A radiation-tolerant, dual-redundant onboard computer (SX-SBOX-OBC-01) built on a SPARC v8 Leon4FT processor with CAN, SpaceWire and optional MIL-STD-1553-like interfaces.
| Dimensions | 171 x 111 x 51 (without fasteners) mm |
| Mass | 0.86 kg |
| Power voltage | 22-34, galvanic isolation 500 V |
| Power consumption, wt | up to 10 |
| Duplicated interfaces | CAN2B, SpaceWire, MKO/MIL-STD-1553-like bus (optional) |
On-board computer (with a set of sensors and ADC controller)
A Raspberry Pi Compute Module carrier board (SXC-MB-04-ADC) integrating an ADCS controller, gyroscope/magnetometer sensors, coil driver and power switching for CubeSats.
| Model | SPUTNIX SXC-MB-04-ADC |
| Feature | Flexible architecture, all devices on CAN bus interconnect |
| Feature (2) | Raspberry Compute Module CM3/CM3+ |
| Feature (3) | Sensors on CAN bus (magnetometer, attitude rate sensor, temperature, voltages, currents) |
| Feature (4) | EM torquer driver |

Payload Baseboard
A PC/104 compatible Payload Baseboard designed for the development of satellite payloads and other systems, featuring a microcontroller with a CAN driver for satellite bus access.
| Purpose | Can be used for development of payload and other systems compatible with PC/104 bus. |
| Year of release | 2018 |
| Design life | 1 years |
| Lead time | 1 months |
| Flight qualification of the product | No |

Payload baseboard for platforms SXC1/3
A PC/104-compatible breadboard carrier for developing payloads and other systems that need access to the satellite's CAN bus.
| Model | SPUTNIX SXC-MBB-03 |
| Feature | approved MCU with CAN bus design |
| Feature (2) | user area with 2.54 mm pitch |
| Feature (3) | controllable power system for user area |
| Feature (4) | board schematic provided |

SpaceWire-router and on-board storage device of the on-board computer complex
A redundant 16-port SpaceWire routing switch with built-in MRAM storage for on-board data networking of the onboard computer complex.
| Dimensions | 117 x 111 x 51 (without fasteners) mm |
| Mass | 0.96 kg |
| Power voltage | 22-34, galvanic isolation 500 V |
| Power consumption, wt | 4 |
| Built-in memory, mb | 8 |

SX-SBOX Onboard Computing (Microsatellite)
Onboard computing line of the SX-SBOX instrument suite for microsatellite (Pallada-class) platforms: the onboard computer, a SpaceWire router with onboard mass memory, and flight s
| Family | Onboard computing (SX-SBOX line) |
| Onboard computer sx-sbox-OBC-01 | 171 × 111 × 51 mm, 0.86 kg, ≤10 W; CAN2B, SpaceWire, MIL-STD-1553 (opt) |
| Spacewire router + memory sx-sbox-spw-obdh-mem-01 | 8 MB, up to 16 ports, SpaceWire up to 200 Mbit/s, RMAP (ECSS-E-ST-50-52C) |
| Flight software | SX-SBOX-KINOSOFT |
| Supply voltage | 22–34 V (500 V galvanic isolation) |
SSTL (Surrey Satellite Technology)
United Kingdom · 1985 · 1 productSSTL designs, builds, tests, and operates small satellites, pioneering the use of COTS components and having launched approximately 70 satellites for 22 countries.

SSTL Core
The SSTL Core is a centralized and compact avionics solution that integrates SSTL's flight-proven avionics into a single module.
ST Engineering Satellite Systems
Singapore · 1997 · 1 productSingapore-based satellite manufacturer providing end-to-end satellite design, manufacturing, testing, launch and ground segment services, plus flight-proven space avionics.

ST Engineering Spacecraft On-Board Computer (OBC)
Radiation-tolerant dual-core LEON3-FT on-board computer for reliable LEO satellite data handling and platform control.
| Processor | Dual-Core LEON3-FT Sparc V8 |
| System clock | 40 MHz (up to 80 MHz) |
| Fpu | IEEE-754 compliant, double precision |
| Boot memory | 2 MB |
| Non-volatile memory | 8 MB MRAM |
Tata Advanced Systems (Space)
India · 2006 · 1 productTata Group aerospace and defense manufacturer providing satellite Assembly, Integration and Testing (AIT) services for ISRO and commercial operators

Mission Systems and Avionics
Tata Advanced Systems has developed several mission critical systems and avionics such as Mission Computers, On-board Computers, Military GPS Units, Gimbaled Payloads and Ground Co
TelePIX
South Korea · 2019 · 1 productEnd-to-end satellite solutions from payload development to AI-powered analytics — hyperspectral/EO payloads, onboard edge-AI processors, and satellite imagery analytics software.

TetraPLEX
TetraPLEX is a high-performance AI on-board processor designed for edge computing in space, enabling in-space AI processing and edge computing.
| Space heritage | 2024 |
| Processor | RISC-V FPGA SoC+ 4-core |
| Gpu | 1024-core embedded GPU |
| Dimensions | 100 mm x 100 mm x 90 mm |
| Mass | 500 g |
Terma
Denmark · 1949 · 1 productTerma is a global aerospace, defense, and security company that develops and manufactures radar systems, aircraft self-protection systems, and space components like star trackers for international cus
On-Board Computer (OBC)
Radiation-tolerant on-board computer for ESA and commercial satellites — LEON2/3/4 processor, MIL-STD-1553 and SpaceWire interfaces, proven heritage on multiple ESA science and EO
| Processor | LEON2/3/4 (SPARC V8/V9 ISA) |
| Data buses | SpaceWire, MIL-STD-1553, UART, SPI, I²C |
| Memory | Rad-tolerant SRAM + EEPROM/FLASH NVM |
| Qualification | ESA ECSS, full documentation |
| Radiation | TID and SEU mitigation |
Tethers Unlimited, Inc. (AMERGINT)
United States · 1994 · 1 productUS developer of deployable space structures, the SWIFT software-defined radio, HYDROS water-electrolysis thrusters and in-space manufacturing tech; now part of ARKA Group (formerly AMERGINT).

CryptoSWIFT FIPS140-2
CryptoSWIFT FIPS140-2 is a hardware encryption solution for LEO small satellite missions, offering high-performance AES-256 encryption up to 55 Mbps.
| Built for | LEO small satellite missions |
| TRL | 9 Hardware |
| Encryption | High performance AES-256 encryption |
| Speeds | up to 55 Mbps |
| Certification | NIST FIPS140-2 Level 1 Certification in Process |
Tiger Innovations, Inc.
United States · 1997 · 1 productUS aerospace electronics firm (General Atomics subsidiary); solar array simulators, RF devices, EGSE, and payload testing for space programs.

Integrated Electronics Module (IEM)
Modular, radiation-hardened spacecraft avionics suite combining C&DH and EPS functions, with flight heritage on STPSat-1.
| Power consumption | 24 Watts |
| Mass | < 5.25 kg |
| Dimensions | 7" x 7.125" x 4.437" |
| Processor | RAD-750 |
| Analog signals | 56 |
Totum Labs
United States · 2018 · 1 productSatellite IoT connectivity company delivering direct-to-satellite, indoor-capable tracking and monitoring using its proprietary DMSS waveform and LEO nanosatellite constellation.

ORC3990 — Space-Grade Processing SoC for Satellite Avionics
The ORC3990 is a radiation-tolerant, space-grade System-on-Chip (SoC) developed by Totum Labs (in partnership with Orca Systems) for use in satellite onboard computers, payload pro
| Device type | Radiation-tolerant System-on-Chip (SoC) |
| Radiation tolerance | SEU mitigation, latch-up protection, EDAC memory |
| Target orbits | LEO, MEO; radiation-belt tolerant |
| Integrated functions | Processor core + image processing + RF signal processing + data compression |
| Avionics interfaces | SpaceWire, CAN bus, UART, SPI, I2C |
Tsd-space
Italy · 1977 · 1 productItalian space imaging and avionics company in Pozzuoli; cameras, focal plane arrays, image compression, OBCs, C&DH systems, power management, and ground segment equipment.

Payload Electronics
TSD offers a range of payload electronics, including image data handling and storage units, high-data-rate image compression modules, data processing units, and control and data ac
| Pilot-d cdiu mission | Luna-25 (Luna-Glob) mission |
| Pilot-d cdiu functionality | Image Data Handling and Storage Unit, interface unit, communication I/Fs, video data stora |
| Multi/hyperspectral module mission | PRISMA Hyperspectral Mission |
| Multi/hyperspectral module component | PRISMA Payload Main Electronics Unit (SDAC) |
| Multi/hyperspectral module configuration | Upper board (nominal), lower board (redundant) |
Tyvak International S.r.l.
Italy · 2013 · 1 productItalian manufacturer of CubeSat and small satellite platforms and subsystems, a Terran Orbital company with deep flight heritage across scientific and commercial missions.

Command and Data Handling (C&DH) System
Onboard flight computer suite with redundant backup and multiple radio/communication interfaces.
Unibap Space Solutions AB
Sweden · 2013 · 6 productsSwedish space computing company offering the iX10/iX5 onboard computers, SCOS OS, and LOOM hyperspectral pipeline for AI-enabled satellite operations.

ADS
Unibap's Application Development hardware kit that lets developers build and verify onboard software on the same hardware architecture used in their space Engineering and Flight Mo
| Ix10 ads-x2 cpu | AMD Ryzen V1000 |
| Ix10 ads-x2 gpu | 8 x AMD Vega |
| Ix10 ads-x2 vpu | Intel Movidius Myriad X and Hailo-8 |
| Ix10 ads-x2 ram | 2 x 16 GB DDR4 |
| Ix10 ads-x2 storage | 512 GB SATA SSD |

Catalyst – Unibap Collaboration
This collaboration focuses on processing data and automating image selection directly at the source for space applications.

iX20
The iX20 transforms up to 100 Gbps of raw sensor data into actionable information through a real-time processing pipeline that combines hardware acceleration, image formation, and
| CPU | AMD Ryzen V8000 |
| GPU | AMD Radeon, 12-core, 2.7 GHz |
| VPU | 4 x Hailo-8 |
| RAM | 64 GB DDR5 ECC (CPU/GPU) |
| Storage | 4 x 4 TB NVMe SSD |

iX5
The iX5 is a versatile and efficient space-proven processing unit with machine learning capabilities, designed for a wide range of mission profiles and suitable for smaller spacecr
| Flight heritage | 5 missions launched |
| Successful days in space | >1 000 |
| Mass | 421 g |
| Power | 10 to 30 W |
| Supply voltage | 12 V DC |

iX5-100
Unibap's iX5-100 is an onboard processing solution used in the NASA HyTI Mission for data collection, processing, and communication from a 6U CubeSat platform.

Unibap iX10 Space Computer
Unibap's most powerful onboard space computer, combining CPU, GPU, and VPU processing with extensive I/O connectivity for demanding AI and edge-computing missions.
| Cpu | AMD Ryzen V1000 |
| Gpu | 8 x AMD Radeon |
| Vpu (iX10-101) | Intel Movidius Myriad X |
| Vpu (iX10-102) | Hailo-8 |
| Ram | 24 GB DDR4 ECC |
VECTRONIC Aerospace GmbH
Germany · 2000 · 2 productsGerman manufacturer of space subsystems — reaction wheels, star trackers, power control, and data handling units — with over 25 years of flight heritage on small satellite missions.

On-Board Data Handling
VECTRONIC Aerospace On-Board Data Handling systems are designed for small satellite applications, processing telecommands and providing autonomy with event-triggered processes.
| Power consumption | around 1.5 W |
| Signal interface | user definable number of standard asynchronous SCI’s on RS422/RS485 level |
| Baud rate | adjustable up to 1Mbaud |
| Flight heritage | 7 slightly different On-Board Data Handling systems in Orbit and several others waiting fo |

Payload Data Handling System VPDHS
The VPDHS is a Payload Data Handling System developed by VECTRONIC Aerospace for small satellite applications, designed to receive, store, compress, and format payload data for tra
| Dimensions | 290 mm x 192 mm x 34 mm |
| Mass | 2.3 kg |
| Mounting pattern | 6 x M4 |
| Power consumption | Max 15 W |
| Power supply | 9 V – 18 V, 18 V – 36 V |
VENG S.A.
Argentina · 2007 · 1 productArgentine space engineering company (Buenos Aires, founded 2007) and prime contractor to CONAE for the Tronador II launch vehicle programme, satellite avionics, propulsion, and ground-segment systems.

Antartix – Computadora OBC
The Antartix v2.0 OBC is a high-performance, easy-to-integrate on-board computer and FPGA development board built on the AMD Xilinx Artix-7 FPGA, optimized for MicroBlaze and PetaL
| Factor de forma | PCI/104-Express totalmente compatible |
| FPGA | AMD Artix-7 XC7A200T-1FBG484IHz |
| Memoria | DDR3L SDRAM 4Gb 933 MHz20 ns MT41J128M16HA-125:K |
| Memoria flash | A bordo – NOR Memory IC 128 Mbit SPI – Quad I/O 104 MHz |
| Memoria adicional | BPI a bordo – NOR Memory IC 512 Mbit Paralela 133 MHz – 96 ns |
VVDN Technologies
India · 2007 · 1 productIndia-based contract engineering and electronics manufacturing company serving aerospace and defence with avionics, tactical communications, UAS and satellite communications subsystems.

VVDN Aerospace & Defence Electronics Engineering
Full-lifecycle engineering and manufacturing services for mission-critical aerospace and defence electronics, spanning avionics, tactical comms, FPGA, RF, and ruggedized embedded p
| Engineering disciplines | FPGA, RF, embedded SW/HW, silicon, mechanical |
| Target applications | Tactical comms, avionics, UAS, missile sub-systems, surveillance |
| Environmental testing | MIL-STD-810 (environmental), MIL-STD-461 (EMI/EMC) |
| Quality standard | Aerospace Quality Management System |
| Airborne software standard | DO-178 / airborne software development |
Xiphos Technologies
Canada · 2003 · 11 productsXiphos Technologies designs low-SWaP Zynq and Versal-based computing modules and on-board computers for SmallSats, offering 120+ years of cumulative flight heritage.

Q7 Processor
The Q7 is a space-qualified processor board featuring a Xilinx Zynq SoC with dual-core Cortex-A9 MPCore processors and reprogrammable logic, designed for high-performance computing
| Processor | Xilinx Zynq SoC includes ARM dual-core Cortex-A9 MPCore processors supported by massive pr |
| Memory | LPDDR2 RAM (with ECC) |
| Memory (2) | 2x QSPI Flash (NOR) |
| Memory (3) | 2x MicroSD |
| Power | Typical 2 W |

Q8 Computer-on-Module
Low SWaP Zynq UltraScale+ MPSoC processor with 30 krad radiation tolerance for demanding satellite payloads and bus subsystems.
| Mpsoc | Xilinx Zynq UltraScale+ |
| Application cpu | Quad-core ARM Cortex-A53 |
| Real-time cpu | Dual-core ARM Cortex-R5 |
| Gpu | ARM Mali-400 |
| Ram | 4 GB LPDDR4 (ECC) |

Q8 Low SWaP Computer-on-Module
The Q8 is a spaceflight-ready miniature processing board, building on the Xiphos Q-card family's heritage, offering high performance and flexibility for demanding space application
| Processor | Xilinx Zynq UltraScale+ Multi-Processor System-on-Chip (MPSoC) Processing FPGA |
| Cpu | quad-core ARM Cortex-A53 Application Processing Unit |
| Real-time processing unit | dual-core ARM Cortex-R5 |
| Gpu | ARM Mali-400 |
| Ram | 4 GB LPDDR4 (with ECC) |

Q8 On-Board Computer
Flight-proven SmallSat on-board computer based on the Q8 processor, providing full spacecraft control with 120+ years of flight heritage.
| Processor | Xilinx Zynq SoC (ARM dual-core Cortex-A9 MPCore) |
| Control FPGA | Microchip ProASIC3 |
| Ram | 256 MB LPDDR2 (ECC) |
| Storage | 2x MicroSD |
| Serial interfaces | RS-422, RS-485, RS-232, CAN, LVDS-based protocols |

Q8J Computer-on-Module
Low SWaP Zynq UltraScale+ processor with GTH multi-Gbps transceivers and JESD204B support for next-generation SDR and high-speed payload applications.
| Mpsoc | Xilinx Zynq UltraScale+ |
| Application cpu | Quad-core ARM Cortex-A53 |
| Real-time cpu | Dual-core ARM Cortex-R5 |
| Ram | 4 GB LPDDR4 (ECC) |
| Flash | 2x 256 MB QSPI (NOR) |

Q8J Data Storage and Interface Board
High-capacity payload data storage and interface computer for the Q8J, providing 2 TB SSD storage and extensive high-speed I/O.
| Storage | 2x 1 TB SSD |
| Sustained write speed | >300 MB/s |
| Ethernet | 4x GigE (1 Gbps) with magnetics |
| CAN | 2x CAN controllers |
| RS-422 | 7x RS-422 ports |

Q8J Low SWaP with GTH Computer-on-Module
The Q8J is a low SWaP processor board designed for space applications, featuring a Xilinx Zynq UltraScale+ MPSoC and multi-Gigabit transceivers for high-speed interfaces.
| Processor | Xilinx Zynq UltraScale+ Multi-Processor System-on-Chip (MPSoC) Processing FPGA |
| Application processing unit | quad-core ARM Cortex-A53 |
| Real-time processing unit | dual-core ARM Cortex-R5 |
| Gpu | ARM Mali-400 |
| Ram | 4 GB LPDDR4 (with ECC) |

Q8RFG3 Gen 3 RFSoC Processor
Third-generation space-grade RFSoC processor with 8-channel 14-bit ADC/DAC up to 6 GHz RF input and multi-device synchronization for phased-array applications.
| Mpsoc | Xilinx Zynq UltraScale+ ZU48DR |
| Application cpu | Quad-core ARM Cortex-A53 @ up to 1.2 GHz |
| Real-time cpu | Dual-core ARM Cortex-R5 @ 500 MHz |
| Ps ram | 4 GB LPDDR4 DRAM (EDAC) |
| Pl ram | 4 GB DDR4 DRAM |

Q9 Versal Computer-on-Module
High-performance AMD Versal AI-edge compute module with 152 AI Engine tiles, 2 TB NVMe storage, and 30-50 W power budget for satellite AI/ML payloads.
| Mpsoc | AMD Versal SoC |
| Application cpu | Dual-core ARM Cortex-A72 @ 1.7 GHz |
| Real-time cpu | Dual-core ARM Cortex-R5F @ 750 MHz |
| Ai engines | 152 AI Engine-ML tiles |
| System logic cells | 820,000 |

Xiphos Q8RF Family
Zynq UltraScale+ RFSoC-based space processor family (Q8RF Gen 1 and Q8RFG3 Gen 3) combining direct RF sampling, FPGA logic, and ARM processing for onboard SDR.
| Operating temperature | -40 to +60 °C |
| Dimensions | 100 mm x 100 mm x 20 mm |
| Mass | 200 g |
| Power (Q8RF) | 20-30 W typical @ 5-9 V |
| Power (Q8RFG3) | 25-35 W typical @ 5-15 V |

Xiphos Q9 Versal Computer-on-Module
High-performance AI/ML-capable Versal-based COTS computer-on-module in a tiny form factor, built for intensive onboard processing.
| Operating temperature | -40 to +60 °C |
| Dimensions | 90 mm x 110 mm x 20 mm |
| Mass | 56 g without connectors |
| Power | 30-50 W typical; 8 to 14 VDC; over-current detection & protection (global and local) and b |
| Memory | 16 GB LPDDR4 DRAM (2x8 GB); 1 GB (4x 256 MB) QSPI Flash (NOR); 2x NVMe SSD, 1,000 GB each, |
Zaitra
Czech Republic · 2020 · 1 productCzech space-tech company building on-board data processing hardware and AI software that make Earth observation satellites more autonomous.

SKAIDOCK
SKAIDOCK delivers high-performance data processing and handling for small satellite missions. Designed for CubeSats, it offers seamless integration and plug-and-play compatibility
| Processor | AMD UltraScale+ XCZU7EG with ProASIC3 supervisor (Xiphos Q8J) |
| Ram | 4 GB LPDDR4 ECC |
| Flash (QSPI) | 2 × 256 MB QSPI |
| Storage (eMMC) | 2 × 128 GB eMMC |
| Operating temperature | -40 °C to +60 °C |
ZeroG Lab
China · 2016 · 1 productZeroG Lab (Zero Gravity Lab) develops integrated satellite systems and space-based intelligence solutions for government and enterprise customers. The company works across the full chain: satellite platforms and payloads, onboard systems, E

Onboard Flight Computers
Fault-tolerant onboard computers with AI acceleration for navigation and payload processing.
Zhongke Tiansuan (Comospace)
China · 2024 · 2 productsChinese space-based intelligent computing startup building satellite-borne AI supercomputers under its 'Tiansuan Plan.'

Aurora 1000 Satellite-Borne Intelligent Computer
First-generation satellite-borne AI computer carrying a domestic high-performance AI chip, in orbit since 2022.
| On-orbit operation | 1,000+ cumulative days (multiple satellites) |
| Launch year | 2022 |
| Reported ai compute | ~32 TOPS (INT8, per industry reporting) |
Comospace Satellite Edge Computing Platform
Chinese satellite computing constellation providing in-orbit edge computing and AI processing services for real-time Earth observation data analysis.
| Technology | In-orbit edge computing and AI processing |
| Advantage | Reduced latency vs. ground processing |
| Applications | Disaster response, real-time Earth observation |
ZIN Technologies
United States · 4 productsZIN Technologies is a Cleveland, Ohio aerospace engineering firm with 65+ years of heritage delivering flight-proven spacecraft power, computing, and systems integration hardware for NASA and DoD.

Proton2X-Box
Proton2X-Box is a modular, flight-proven digital avionics platform built around a dual-core PowerPC processor with FPGA-configurable I/O for spacecraft data handling and control.
| Processor | Dual-core PowerPC |
| I/o | FPGA-configurable digital I/O, analog and digital sensor/instrument channels |
| Storage | Solid-state storage with error correction |
| Flight heritage | Flight-proven, space-ready, proven program heritage |
| Operating temperature | -20°C to +100°C |

Proton600K Multi-Core Processor
Radiation-hardened 3U OpenVPX single-board computer with an 8-core ARM architecture for mission-critical edge computing.
| Form factor | 3U OpenVPX Single Board Computer |
| Radiation tolerance | Radiation-hardened, immune to destructive latch-up, patented H-Core mitigation for SEU/SEF |
| Cores | 8-core ARM: dual Cortex-A72 + quad Cortex-A53 + dual Cortex-M4F real-time cores |
| Controllers | Dedicated system controller and security processor |
| Memory | ECC-protected memory, on-chip ECC and external LPDDR4 support |

ProtonVPX-Box
A modular 3U VPX digital avionics compute platform built around the Proton600K multi-core space processor, configurable to meet varied mission objectives.
| Backplane | High-speed 3U VPX mesh backplane, no separate SRIO switches/SpW routers required |
| Chassis | Rugged thick-wall aluminum chassis |
| Baseline configuration | 5-slot: Proton600K Multi-Core Computer, SSR, Digital I/O, Analog I/O, Power Supply |
| Core processor | Proton600K multi-core high-performance space processor |
| Operating temperature | -40°C to +100°C |

SBCFA1000 Single-Board Computer
Flight-proven radiation-tolerant single-board computer for satellite command, data handling, and payload management.
| Type | Radiation-tolerant single-board computer (OBC) |
| Application | Command and data handling, payload management |
| Flight heritage | NASA ISS research activities (400+ experiments) |
Directory
Manufacturers in this sector
2NDSpace Srl
New Space company designing modular nanosatellite/CubeSat hardware: structures, solar panels, EPS, antennas, OBCs, and deployers/separation systems.
3D Plus (HEICO)
World-leading manufacturer of space electronic components using proprietary 3D interconnect technology for extreme miniaturization.
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AAC SpaceQuest (AAC Clyde Space subsidiary)
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Premier thermal management solutions company specializing in custom two-phase heat transfer technology for aerospace, defense, and industrial applications.
Aethero
Aethero designs and manufactures high-performance, space-rated computers and offers compute-as-a-service for various space platforms, from CubeSats to Space Stations.
Airbus Defence and Space
Airbus Defence and Space designs and manufactures satellites, spacecraft equipment, and provides related services for telecommunications, navigation, Earth observation, and space exploration
Aitech Systems
Designer and manufacturer of rugged, high-performance embedded computing solutions for aerospace, defense, and space applications.
Akula Tech
Melbourne-based deep-tech startup building AI-powered smart satellites with onboard hyperspectral data processing and in-orbit AI model execution.
Alba Orbital
Alba Orbital manufactures PocketQube satellites, provides launch and ground station services, and operates a fleet of nighttime imaging satellites for government and commercial clients.
Alpha Data Parallel Systems
Alpha Data Parallel Systems manufactures FPGA cards, I/O adaptors, carrier cards, and development kits. They provide custom solutions and legacy products for various markets, including space
ALTER Technology
ALTER Technology provides laboratory and engineering services for high-reliability EEE components, specializing in microelectronics and optoelectronics engineering, procurement, assembly, an
Alén Space
Alén Space designs, manufactures, and operates small satellites, providing end-to-end mission development services and advanced communication platforms, subsystems, and components for space
Aphelion Orbitals
Aphelion Orbitals is a New Jersey-based launch vehicle company developing the Helios nanosatellite launch system for regular, scheduled orbital access at low cost.
Aptos Orbital
Space-hardened compute and communications terminal connecting satellites directly to the cloud (AWS, Azure) with 99% global coverage.
Argotec Srl
Argotec is an Italian spacecraft manufacturer that designed and operates the ArgoMoon CubeSat and develops satellite platforms and subsystems for ESA and commercial missions.
Arquimea
Spanish space technology company founded 2007 in Leganes, developing MEMS relay switches, SiC power devices, and miniaturized power conditioning units for satellite applications.
Arralis
Irish developer of mmWave and RF/microwave MMICs, modules, phased-array antennas, and radar/comms front-end systems for satellite, aerospace and defense markets.
BAE Systems
UK defense and aerospace prime with a dedicated space division; develops Azalea radar satellites and offers Space-as-a-Service payload hosting.
Beijing Huali Chuangtong Technology Co., Ltd.
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)
Berlin Space Technologies
Berlin Space Technologies (BST) designs and mass manufactures small satellite systems and technologies, providing end-to-end solutions for space missions.
Beyond Gravity (ex-RUAG Space)
Swiss-Swedish space components manufacturer providing satellite structures, thermal control products, payload electronics, and antennas for commercial and institutional programs.
CAVU Aerospace
CAVU Aerospace designs and manufactures spacecraft avionics, including radiation-tolerant onboard computers, thermal control units, frame grabbers, and flight-proven satellite cameras for sp
CesiumAstro
US manufacturer of software-defined, phased-array communication systems and payloads for satellite constellations, defense, and space applications.
CONTEC
CONTEC provides an all-in-one solution for satellite data reception, processing, and analysis, supporting space missions through its global ground station network.
Cosmoleap
Dahang Transition develops and operates medium and large reusable launch vehicles and their on-board computers, supporting satellite Internet engineering.
CubeSat Aerospace
Indian CubeSat developer offering flight-ready 1U–6U satellite structures, subsystem components, environmental testing services, launch integration, and STEM education programs from Ahmedaba
Curtiss-Wright Defense Solutions
American aerospace and defense electronics company providing rugged computing and data acquisition systems for space and defense platforms.
Data Patterns (India) Ltd.
Vertically integrated Indian defence and aerospace electronics company designing and manufacturing avionics, microelectronics, RF/microwave, radar, test equipment and space systems.
Deimos Space (Indra)
Spanish space engineering group (founded as Deimos Space, part of Elecnor 2001-2024) now operating as Indra Space, delivering end-to-end satellite platforms, avionics, ground segment, GNSS a
Dragonfly Aerospace
South African manufacturer of high-performance electro-optical imaging payloads and satellite platforms for Earth observation.
DSI Aerospace Technology
DSI Aerospace Technology develops dependable electronics for space applications. They offer products such as On-board Computers, Payload Data Handling Units, Data Processing Units, Instrumen
Edge Aerospace
Developer of high-performance orbital Data Processing Units (DPUs) for autonomous space operations.
EDGX
Belgian NewSpace company developing in-orbit edge AI computing solutions; makes the EDGX Sterna Computer — Europe's first NVIDIA-based onboard payload data processing unit for satellites.
Eidel
Norwegian space and defence electronics company specializing in telemetry, secure communications, and mission-critical instrumentation since 1966.
ElmSpace
Developer of fluid-dynamic attitude control systems, gyroscopes, and air bearings for the space industry.
Emtech Space
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
Emxys
Emxys is a Spanish space electronics company specialising in advanced onboard computers, power systems, optical transceivers, and complete nanosatellite platforms for data-intensive space mi
EnduroSat
Software-flexible CubeSat platforms (1U–16U+), shared-satellite hosted-payload service.
EREMS
EREMS is a French SME founded in 1979, specializing in the design and realization of electronic equipment and software for high technology fields including Space.
EXA (Astro-und Feinwerktechnik)
German manufacturer of reaction wheels, CubeSat picosatellite deployers, and AOCS components for small satellites, based in Berlin-Adlershof.
Exolaunch
Berlin-based launch and deployment services company providing end-to-end rideshare missions, satellite integration, and proprietary separation hardware for small satellites.
Gaisler
Radiation-hardened microprocessors, IP cores, and software for space and high-reliability embedded systems.
GAUSS Srl
Italian company specializing in complete lifecycle management of CubeSats and NanoSatellites: design, manufacturing, subsystems, ground stations and deployers.
GomSpace
GomSpace is a Danish CubeSat manufacturer producing satellite platforms, subsystems, and end-to-end mission solutions. Products include the NanoCom radio modules, NanoPower EPS, and complete
Hongqing Technology (鸿擎科技)
Beijing satellite constellation company partnered with Blue Arrow Aerospace; develops communications, remote sensing, and science satellites plus in-house Jinwu propulsion, Chiyu power, and
ibeos
Ibeos designs and manufactures satellite electronics, including processors, single board computers, and electric power subsystems, for LEO, GEO, and beyond missions.
Innoflight
Innoflight, Inc. is a US-based aerospace electronics company headquartered in San Diego, California, developing advanced software-defined radios (SDR), cryptographic communication systems, a
Institute of Aeronautical Engineering
The Institute of Aeronautical Engineering (IARE) in Hyderabad is a specialized engineering institution with a core focus on aeronautical and aerospace engineering. IARE offers cutting-edge p
JAVAD GNSS
American GNSS technology company manufacturing high-precision positioning receivers for surveying, geodesy, and machine control applications.
Kayser Space
Kayser Space designs, manufactures, integrates, and tests hardware and platforms for space programs, supporting over 100 missions and microgravity research.
KP Labs
Polish space AI company developing advanced on-board data processing solutions for satellites, enabling real-time AI-powered Earth observation and mission autonomy in orbit.
LiquidCool Solutions
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
Mercury Systems
Mercury Systems delivers end-to-end processing ecosystems for aerospace and defense systems. They provide signal, compute, data management, display, and secure products. They have supported
MinoSpace
Chinese commercial satellite manufacturer building Earth observation, communications, and remote sensing satellites, plus payloads, components, and ground terminal systems.
Motiv Space Systems
Motiv Space Systems designs and builds space robotics, motor controllers, and mechanisms, including the robotic arm on NASA's Mars 2020 Perseverance rover.
Muon Space
Muon Space is the Mission Foundry, designing, building, and operating high-performance satellite constellations for defense, civil, and commercial customers.
N7 Space
N7 Space provides embedded software development and MBSE solutions for the space industry, specializing in on-board software for satellites and offering related services and toolchains.
NanoAvionics
Pre-integrated nanosatellite buses (3U–16U+ MP42), green chemical propulsion, mission integration.
Needronix
Polish smallsat hardware company designing and manufacturing components and subsystems for CubeSats and small satellites, serving commercial and institutional space customers across Europe.
Novi
American space technology company developing satellite systems and space infrastructure solutions.
NTC Module
NTC Module (АО «НТЦ «Модуль») — Russian space industry enterprise, Moscow. Its products listed on NewSpace Market come from the Glavkosmos export catalogue.
O.C.E. Technology
OCE Technology designs and manufactures high-reliability embedded software, hardware, and satellite subsystems for challenging applications, with heritage on Chinese satellites.
Omnipresent Robot Technologies
Indian deep-tech company building autonomous space, aerial and robotic systems, including SAR satellites, onboard edge-computing payloads and AI perception software for defense and commercia
OrbitsEdge
OrbitsEdge is a Cocoa Beach, Florida-based company developing ruggedized, flight-qualified edge computing platforms that bring high-performance data processing and AI inference directly into
Pumpkin, Inc.
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
Rakon Limited
Global leader in frequency control and timing solutions — space-qualified oscillators, GNSS receivers and S-band transceivers — with 40+ years of flight heritage.
Ramon.Space
Israeli developer of space-resilient, radiation-tolerant onboard computing infrastructure — AI/DSP processors, storage and communication processors that turn satellites into software-defined
Redwire Space Belgium (ex-QinetiQ Space)
Belgian satellite systems facility in Kruibeke, formerly QinetiQ Space nv, acquired by Redwire Space in 2022; delivers entire satellites, avionics, and the International Berthing and Docking
Rogue Space Systems Corp.
US builder of autonomous orbital robots (Orbots) for proximity operations, satellite inspection, in-space compute, and orbital logistics, headquartered in Laconia, New Hampshire.
Réaltra Space Systems Engineering
Irish space-electronics company designing and manufacturing ruggedized avionics and telemetry systems for launch vehicles and space missions.
S4 - Smart Small Satellite Systems GmbH
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.
Saturn Satellite Networks
Satellite hardware company developing MiniGeoSat and Nationsat platforms, along with software-defined radio and shared-launch programs for affordable GEO and regional satellite missions.
Saturn Space
Saturn Satellite Networks (SSN) Inc. is a US-based space technology company that designs and manufactures reliable, affordable satellites for GEO, MEO, and LEO applications.
Serenum Space
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.
Sidus Space, Inc.
US space and defense technology company (NASDAQ: SIDU) building the LizzieSat multi-mission satellite platform, AI/ML edge-computing avionics, and precision satellite manufacturing services
SkyLabs d.o.o.
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
Space Cubics Inc.
JAXA-affiliated Japanese venture (Sapporo, founded 2018) designing FPGA-based onboard computers for CubeSats and small satellites, with flight heritage on ISS Kibo and lunar landers.
Space Inventor ApS
Space Inventor ApS is a Danish second-generation NewSpace company providing non-ITAR CubeSat, nanosat, and microsat components, platforms, and turnkey satellite missions with full vertical i
Space Products and Innovation (SPiN)
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
Spacemanic s.r.o.
Slovak-Czech full-service nanosatellite mission provider offering CubeSat platforms (1U-16U), onboard subsystems, rideshare launch integration, and ground segment services.
SpaceTech GmbH
German space company designing, developing and producing solar arrays, laser-optical instruments and space electronics for satellite missions.
Spiral Blue
Australian space technology company building LiDAR and AI edge computing systems for LEO satellites.
SPUTNIX
SPUTNIX is a Russian manufacturer of nanosatellite and microsatellite platforms, onboard subsystems and ground infrastructure, operating as a subsidiary brand of Sitronics Group.
SSTL (Surrey Satellite Technology)
SSTL designs, builds, tests, and operates small satellites, pioneering the use of COTS components and having launched approximately 70 satellites for 22 countries.
ST Engineering Satellite Systems
Singapore-based satellite manufacturer providing end-to-end satellite design, manufacturing, testing, launch and ground segment services, plus flight-proven space avionics.
Tata Advanced Systems (Space)
Tata Group aerospace and defense manufacturer providing satellite Assembly, Integration and Testing (AIT) services for ISRO and commercial operators
TelePIX
End-to-end satellite solutions from payload development to AI-powered analytics — hyperspectral/EO payloads, onboard edge-AI processors, and satellite imagery analytics software.
Terma
Terma is a global aerospace, defense, and security company that develops and manufactures radar systems, aircraft self-protection systems, and space components like star trackers for interna
Tethers Unlimited, Inc. (AMERGINT)
US developer of deployable space structures, the SWIFT software-defined radio, HYDROS water-electrolysis thrusters and in-space manufacturing tech; now part of ARKA Group (formerly AMERGINT)
Tiger Innovations, Inc.
US aerospace electronics firm (General Atomics subsidiary); solar array simulators, RF devices, EGSE, and payload testing for space programs.
Totum Labs
Satellite IoT connectivity company delivering direct-to-satellite, indoor-capable tracking and monitoring using its proprietary DMSS waveform and LEO nanosatellite constellation.
Tsd-space
Italian space imaging and avionics company in Pozzuoli; cameras, focal plane arrays, image compression, OBCs, C&DH systems, power management, and ground segment equipment.
Tyvak International S.r.l.
Italian manufacturer of CubeSat and small satellite platforms and subsystems, a Terran Orbital company with deep flight heritage across scientific and commercial missions.
Unibap Space Solutions AB
Swedish space computing company offering the iX10/iX5 onboard computers, SCOS OS, and LOOM hyperspectral pipeline for AI-enabled satellite operations.
VECTRONIC Aerospace GmbH
German manufacturer of space subsystems — reaction wheels, star trackers, power control, and data handling units — with over 25 years of flight heritage on small satellite missions.
VENG S.A.
Argentine space engineering company (Buenos Aires, founded 2007) and prime contractor to CONAE for the Tronador II launch vehicle programme, satellite avionics, propulsion, and ground-segmen
VVDN Technologies
India-based contract engineering and electronics manufacturing company serving aerospace and defence with avionics, tactical communications, UAS and satellite communications subsystems.
Xiphos Technologies
Xiphos Technologies designs low-SWaP Zynq and Versal-based computing modules and on-board computers for SmallSats, offering 120+ years of cumulative flight heritage.
Zaitra
Czech space-tech company building on-board data processing hardware and AI software that make Earth observation satellites more autonomous.
ZeroG Lab
ZeroG Lab (Zero Gravity Lab) develops integrated satellite systems and space-based intelligence solutions for government and enterprise customers. The company works across the full chain: sa
Zhongke Tiansuan (Comospace)
Chinese space-based intelligent computing startup building satellite-borne AI supercomputers under its 'Tiansuan Plan.'
ZIN Technologies
ZIN Technologies is a Cleveland, Ohio aerospace engineering firm with 65+ years of heritage delivering flight-proven spacecraft power, computing, and systems integration hardware for NASA an
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