Spacecraft luminous emittance. Radiant power of the outer surfaces under the action of accelerated electrons and protons on GEO
The results of calculations and experimental measurements of radiation power of different outer structures (solar arrays, antenna-feeder devices, white glass-fiber clothes, radiators of thermal control systems) as well as space vehicle in whole under the both separate and simultaneous action of accelerated electrons and protons at GEO have been presented. The predictions of the changes of different structural element radiant power are made for the period of 30 years.