SURVEY OF PROCESSORS FOR SPACE

Processors for space are required to be tolerant to the following radiation and environmental effects: TID (100300 kRad for GEO and beyond, 10-50 kRad for some LEO missions), Latch-up, SEU, SET, SEFI, and temperature cycles. Another reliability issue is the complete and permanent failure of a processor or a critical sub-component. None of the methods surveyed here mitigate such failures, and the common mitigation method is based on deploying spare computers in combination with either a central reconfiguration circuit or a distributed recovery mechanism.

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