HARDWARE / PRODUCTAdded 17 Aug 2026

OBC-Cube-Polar

CAVU Aerospace
OBC-Cube-Polar

CubeSat OBC based on PolarFire FPGA

Technical specifications

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
Interfaces
Digital I/O: 20-60
Interfaces (2)
ADC: 8/16CH with 12-bit or 16-bit resolution
Interfaces (3)
Space Wire: 1 or 2
Interfaces (4)
1G Ethernet: 1 or 2
Interfaces (5)
SerDes: Via GSN Connector for PCIE, JESD, etc.
Interfaces (6)
CAN2.0: 4
Interfaces (7)
RS422 and RS485: 2 to 8
Interfaces (8)
I2C: 2 to 4
Interfaces (9)
SPI: 2 to 4
Operating temperature
-40°C to +85°C @ 10-8 bar
Mass
80gr

About

The OBC-Polar is a cutting-edge onboard computer specifically designed for Cubesat missions. Leveraging the powerful and reliable Microchip PolarFire SoC FPGA technology, this Cubesat OBC provides exceptional performance and versatility for space applications. Whether your mission involves scientific research, Earth observation, or commercial satellite deployment, the OBC-Polar ensures optimal performance and reliability in the harsh conditions of space.

Documentation

Need the full ICD, test reports or a specific revision? Ask the supplier directly.

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