The development of a satellite design demonstration test program is described. The test approach is comprehensive in that it includes the effects from electrostatic discharge (ESD), system generated electromagnetic pulse (SGEMP), as well as dispersed electromagnetic pulses (DEMP). The comprehensive test concept is based on the similarity of the satellite's response to several environments.


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    Title :

    Qualification model spacecraft tests for DEMP, SGEMP, and ESD effects


    Contributors:


    Publication date :

    1977-02-24


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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