OBC & Avionics — Space Hardware Marketplace

OBC PolarFire VPX

• ProcessorMicrochip MPFS460T-1FCG1152I / MPFS460TS-1FCG1152I (with security)
• Risc-v coresQuad 64-bit U54 application cores + 1× E51 monitor core — >4,000 DMIPS total
• FPGA fabric461k logic elements, 784 DSP blocks — flash-based, no SRAM bitstream

OBC based on PolarFire FPGA SoC in 3U VPX

OBC-104

• ProcessorARM Cortex-M3 on FPGA
• Processor (2)Microchip/Microsemi SmartFuion2 Flash Based FPGA
• Processor (3)150 DMIPS @ 128 MHz

CubeSat OBC based in SmartFusion2

OBC-Cube-Polar

• ProcessorMicrochip PolarFire SoC Flash Based FPGA SoC
• Processor (2)Quad 64-bit RISC-V on FPGA + 1 RISC-V Monitoring Core
• MemoryRAM: 2 GB or 4 GB with ECC Protection

CubeSat OBC based on PolarFire FPGA

OBC-Hyper-Polar

• ProcessorRISC-V MSS: 4× 64-bit U54 application cores + 1× E51 monitor core
• FPGA fabricMicrochip PolarFire SoC FPGA — two variants: MPFS250T (254k LE) & MPFS460T (461k LE)
• Memory (Fabric)DDR4 SDRAM 8 GB 72-bit ECC Enabled

OnBoard Computer based on PolarFire FPGA SoC

Typhoon Edge

• ProcessorNVIDIA JETSON ORIN AGX Industrial & Microchip PolarFire SoC MPFS460T
• Ai performance248 TOPS
• Memory64 GB ECC LPDDR5

AI OnBorad Computer- PolarFire FPGA paired with NVIDIA Jetson

FERMI OBC&DH Miniaturized Rad-Hard On-Board Computer

• TypeOn-Board Computer and Data Handling unit (OBC&DH)
• RadiationRad-hard, described by the vendor as best-in-class radiation hardening assurance
• Target platformsMicrosatellite platforms; fitted to Argotec HAWK LITE

Miniaturized radiation-hardened on-board computer and data handling unit for microsatellite platforms, for spacecraft management and computationally intensive algorithms.

MTE-110 Mission Timing Electronics

CubeSat timing unit with embedded chip scale atomic clock (CSAC) and radiation-tolerant IA design, 250 g at 3…

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.

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…

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.

CFC-510P Compact Flight Computer

GPU-based 3U VPX flight computer on AMD Ryzen with CUDA runtime environment, 539 g and 40 W max,…

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…

CFC-400XS Compact Flight Computer

CubeSat compact flight computer with defense-grade Xilinx UltraScale+ MPSoC, CyberDog software suite and Linux reference design, flying since…

Core Drive Electronics (CODE)

• TypeTwo-axis stepper motor controller, modular and stackable
• Motors per moduleTwo bipolar stepper motors, independently controlled
• RedundancyTwo modules stacked vertically, cold redundancy

Compact, lightweight two-axis stepper motor controller for small satellite mechanisms, built as stackable modules.

CODE+ Software Defined Drive Electronics

• ArchitectureFully software-defined, radiation-tolerant microcontroller
• Command interfaceDual UART; CCSDS command and telemetry packets
• Optional extension boardsSignal multiplexing, MIL-STD-1553B communication interface

Software-defined drive electronics with a radiation-tolerant microcontroller, expanded sensing and in-orbit software patching.

FoX Electronics Platform

• Form factor3U SpaceVPX modular platform
• Target orbitsLEO, MEO, GEO and cislunar
• CommunicationEthernet-based, supporting redundancy and high data rates

3U SpaceVPX modular avionics platform (Flexible On-board avioniX) of off-the-shelf modules for LEO, MEO, GEO and cislunar missions.

Multi-Purpose Drive Electronics (MPDE)

• TypeTwo-axis stepper motor controller
• RedundancyTwo electrically identical units for cold redundancy
• Command interfaceMIL-STD-1553 TC/TM (replaceable to suit platform concept)

High-performance two-axis stepper motor controller for satellite mechanisms, optimized for low micro-vibration operation.

Remote Terminal Unit (RTU)

• RedundancyFully redundant
• FunctionBridge between OBC and platform/payload electronic interfaces
• Supported functionsStandard I/O, AOCS, propulsion

Fully redundant remote terminal unit bridging the on-board computer and platform and payload electronic interfaces.