Modern space missions increasingly rely on high-speed, deterministic data links to support advanced subsystems and payloads, including high-resolution imagers, high-bandwidth downlinks, and complex onboard processing. SpaceWire has become the standard for these requirements, providing high bandwidth, time synchronisation, and reliability across nanosatellite, small satellite, and larger spacecraft platforms.
The Craft Prospect SpaceWire Router is designed for missions that demand more capability than legacy data interfaces can provide. Its low-SWaP design is compatible with CubeSat constraints and supports data routing across up to 16 SpaceWire nodes, while also providing a bridge between the SpaceWire bus and UART-based devices.
This architecture simplifies the integration of diverse payloads and subsystems into a unified, high-speed onboard network, supporting scalable and flexible spacecraft system design.

High-performance
routing for up to 16 nodes.

SpaceWire bridge
to common UART
interfaces.

Reliable in-flight
updates via RMAP
protocol.
Technical Specifications
General
FPGA:
Microchip PolarFire
Storage:
16 MB MRAM
Configuration and firmware updates
Form factor:
PC/104 mounting hole locations
Connectors:
Power/data: Harwin Gecko
SpaceWire: Samtec ARF6
Operating Temperature:
-30°C to +70°C
Qualification
Thermal:
Full qualification: -40°C to +80°C
Vibration:
Full qualification:
Sine sweep (NASA GEVS)
Random vibration (NASA GEVS)
Interfaces
SpaceWire:
-
16x ports, 2x per ARF6
-
200 Mbps
-
Time-Codes supported
-
RMAP PnP for config, telemetry, firmware updates
SpaceWire-UART bridge:
-
RS-485 or 2.5 V LVCMOS
-
1Mbps
-
Hardware flow control (RTS/CTS)
-
HDLC-like protocol encapsulates SpaceWire packets
Size, weight, and power
Dimensions:
88 x 94 x 11.5 mm
Mass:
60 g
Power consumption:
Idle: 0.66 W
2x SpW active: 0.84 W
4x SpW active: 1.04 W
8x SpW active: 1.38 W
Input voltage:
6 - 10 V

