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Radiation Tolerant, FPGA-based SmallSat Computer System (RadSat)

Completed TRL 6 (started at 5, targeting 6)

Description

The goal of this project is to mature the technology readiness of a radiation tolerant smallsat computer system for a subsequent orbital flight demonstration. The system is implemented with commercial off-the-shelf (COTS) field-programmable gate arrays (FPGAs) to provide space-computing performance that improves upon existing radiation hardened processors. Commercial FPGAs are now yielding acceptable levels of total ionizing dose immunity due to the thinning of gate oxides and relative deepening of isolation trenches. If a single event effect mitigation strategy can be implemented on COTS FPGAs, then reliable, high performance space computing can be accomplished at a fraction of the cost of existing radiation hardened processors.

Benefits

This technology will increase on-board processing at a significantly reduced cost over existing systems.

Details

Technology areaFlight Computing and Avionics > Avionics Component Technologies > Radiation-Hardened Extreme-Environment Components and Implementations
ProgramSmall Spacecraft Technology (SST)
Lead organizationGoddard Space Flight Center, Greenbelt, MD
Start date2013-10-01
End date2016-04-30

Project contacts

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How to get involved

This is early/mid-stage (TRL 6) — the most realistic path in is NASA SBIR/STTR, which funds small businesses and research institutions to develop technology aligned with NASA's needs (equity-free, phased funding). Check whether a current SBIR/STTR solicitation topic overlaps with this project's technology area, or contact the project directly (above) to ask.

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