Hardware

• 1.4 GHz ARM® 64-bit quad-core Cortex® processor

• Traffic routing and encryption without loading the cores

• Encryption options include AES-256-GCM

• Integrated security engine

• 2GB SDRAM with ECC

• 30GB non-volatile eMMC storage with pSLC mode enabled

• Other storage sizes available upon request

• 256KB high-endurance FRAM memory

• Redundant 32MB boot flash with automatic failover

• Single power input required (12V nominal, ±20%)

• Onboard telemetry: temperature, uptime, and output voltage and current

Software

• Linux support:

• Ubuntu-based OS with GNU toolchain

• Option for Yocto-based OS

• Option for VxWorks®

• NASA cFS (core Flight System) support

Mechanical

• Compact 50mm x 84mm x 13mm packaged form factor

• Thermal pillars bring heat to flat surface

• Rugged, MIL-spec Nano-D connectors

• Suitable for military and commercial use on LEO satellites and airborne platforms

Ethernet

• 2x 1000BASE-T (capacitively coupled)

• 2x 10GBASE-KR (configurable as SGMII)

• 1x SGMII

Serial, configurable as

• 3x RS-485 (half-duplex) + 1x RS-422 (full-duplex), OR

• 2x RS-485 + 2x RS-422, OR

• 3x RS-422

Programming (lab use)

• 1x JTAG