OBC & Avionics — Space Hardware Marketplace

SpaceTech Remote Terminal Unit (RTU)

• ProcessorDual Core LEON3 processor, also usable for data pre-processing
• Onboard connectionCAN-Bus or SpaceWire
• IO architectureStandardized IO-module based on cPCI-Serial-Space standard

cPCI-Serial-Space based Remote Terminal Unit collecting data from avionic sensors and controlling avionic actuators.

RK410 High Reliability Space OCXO

• Package size (LxWxH)99 x 88 x 54 mm
• Nominal frequency5 to 10 MHz
• Stability class10^-10

MIL/ECSS-qualified space oscillator with 10^-10 stability class, used operationally by international space agencies for decades.

On-board computer

• Dimensions, mm171 x 111 x 51 (without fasteners)
• Mass, kg0.86
• Power voltage, V22-34, galvanic isolation 500V

A radiation-tolerant, dual-redundant onboard computer (SX-SBOX-OBC-01) built on a SPARC v8 Leon4FT processor with CAN, SpaceWire and 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…

Payload baseboard for platforms SXC1/3

• ModelSPUTNIX SXC-MBB-03
• Featureapproved MCU with CAN bus design
• Featureuser area with 2.54mm pitch

A PC/104-compatible breadboard carrier for developing payloads and other systems that need access to the satellite's CAN bus.

Scalable Compute Platform (SCP)

Flight-proven GPU-accelerated edge-compute payload providing a full Linux HPC environment for spacecraft, TRL 9 with Gen 3 in…

Fortis VPX Operational Suite

• System componentsSSBC (Quad-Core ARM, rad-hard PolarFire FPGA, 8GB DDR4), PNT module, SDR (S/X-band), FeatherEdge AI/ML module (NVIDIA Jetson AGX Orin Industrial), microcontroller I/O card, power card
• I/OLVDS 4x SpaceWire + Camera Link, Ethernet 4x 1GbE + 2x 10GbE, USB 3.1 Gen1, UART 14x RS-422 + 2x RS-232
• Power input28VDC/12A, 330W max

Rugged 3U OpenVPX/SOSA-aligned command-and-data-handling system for space, defense, and unmanned platforms.

NANOif-2

• StandardISO 19683, IPC Class 3+
• TRL9
• MAITIn-house

Intelligent remote terminal unit with unified TM/TC interface for satellite sensors, instruments and payloads.

picoRTU system

• StandardISO 19683, IPC Class 3+
• TRL7
• MAITIn-house

Highly modular remote terminal unit system for LEO small and micro satellite missions.

NANOhpc-AI

High-performance, power-efficient AI accelerator extension for NANOhpc-obc using dual Hailo-8 accelerators.

NANOhpc-DPU

• StandardISO 19683, IPC Class 3+
• TRL5
• MAITIn-house

High-performance reconfigurable data processing unit extension for NANOhpc-obc, built around AMD Zynq UltraScale+ MPSoC.

NANOhpm-obc

• StandardISO 19683, IPC Class 3+
• TRL9
• MAITIn-house

High-performance MCU-based fault-tolerant on-board computer.

NANOhpc-obc

64-bit high-performance multicore RISC-V on-board computer for AI@Edge and demanding LEO applications.

NANOobc-2

• StandardISO 19683, IPC Class 3+
• TRL9
• MAITIn-house

Fault-tolerant second-generation on-board computer for mission-critical satellite operation.

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.

SC-OBC Module V1

• SoCAMD Versal AI Edge VE2302
• ProcessingArm Cortex-A72 + Cortex-R5F, AI Engine, programmable logic (PL)
• Safety processorMicrochip IGLOO2

High-end small satellite onboard computer built on an AMD Versal AI Edge VE2302 SoC with Arm processing, AI…

SC-OBC Module A1

CubeSat onboard computer built on a Xilinx Artix-7 FPGA running Zephyr RTOS.

Eddie

• Operating temperature-40 C to +85 C
• Dimensions67 x 42 x 7.5 mm
• Mass25 g

Flight-proven on-board computer for command and data handling and payload processing in small satellite missions.