This document is intended to provide a standardized process for mitigation of multipactor breakdown within spacecraft components. It is directed toward component designers, satellite system engineers, as well as the customer community to provide worst-case conditions, margin requirements, and verification of those requirements using state-of-the-art methodologies. In addition, recommended methods are provided, with examples, to ensure proper requirement verification for all satellite RF components susceptible to RF breakdown.


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    Title :

    Standard/Handbook for Multipactor Breakdown Prevention in Spacecraft Components (ANSI/AIAA S-142-2016)


    Publication date :

    2016-01-01


    Size :

    71 pages




    Type of media :

    Standard


    Type of material :

    Electronic Resource


    Language :

    English




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