RADIATION-INDUCED VOLTAGE ON SPACECRAFT INTERNAL SURFACES

The charging of surfaces of insulators beneath the thermal control bla nkets on spacecraft has been numerically simulated. Such insulators ar e found on wiring harnesses, bulkhead feed-throughs, component mountin g hardware, tie; wraps, thermal sensors, etc. These insulators are shi elded from the low energy space plasma by the grounded solar blankets. It is determined that the surfaces of these insulators rise to many t ens of kV in the Earth's electron belts unless sufficient conduction t o the spacecraft frame is established. Secondary electron emission is not sufficient to hold the potential to low values. The dependence of charging upon insulator thickness, electron energy spectra, and materi al properties is investigated. This phenomena is posited as an explana tion for the Spacecraft Anomalies seen on many spacecraft, and on the CRRES satellite in particular.