Derating Requirements Applicable to Electronic, Electrical, and Electro-Mechanical Components for ESA Space Systems

摘要

Derating requirements for electronic, electrical, and electromechanicalcomponents used in equipment for use on ESA spacecraft are presented. Suitable derating is decided on the analyses described. Tables contain: the derating to be applied to specified component parameters; the parameter degradations to be used for worst case analysis; and notes to the tables containing application rules for the components. Data is not supplied for radiation effects analysis as this varies widely and must be considered on a case by case basis.