The RadSat-g (Radiation Satellite), is an 3U CubeSat mission developed at the Montana State University as a technology demonstration of a new radiation tolerant computer system in a low earth orbit (LEO) satellite mission to demonstrate TRL-9 of the technology.
The computer system achieves radiation tolerance through a variety of fault mitigation approaches targeted at making commercial-off-the-shelf Field Programmable Gate Arrays less susceptible to single event effects. The computer system uses a novel fault mitigation strategy to recover from failures caused by high energy ionizing radiation.
The payload consists of a radiation tolerant computer system and a radiation sensor.
|Type / Application:||Technology|
|Operator:||Montana State University|
|Contractors:||Montana State University|
|Power:||Solar cells, batteries|
|Orbit:||400 km × 400 km, 51.6° (typical)|
|RadSat-g||1998-067||21.05.2018||WI LC-0A||Antares-230||with Cygnus CRS-9, CubeRRT, HaloSat, Radix, RainCube, TEMPEST-D, Lemur-2 78, ..., 81, AeroCube 12A, AeroCube 12B, EQUiSat, MemSat, EnduroSat One|