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.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

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


    Erscheinungsdatum :

    2016-01-01


    Format / Umfang :

    71 pages




    Medientyp :

    Standard


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Standard: Flight Dynamics Model Exchange Standard (ANSI/AIAA S-119-2011(2016))

    Bruce Hildreth / Bruce Jackson / Bimal Aponso et al. | AIAA | 2011



    Multipactor Breakdown Test Investigation for S-Band Spaceborne Components

    Qinfen, S. / Junye, C. | British Library Conference Proceedings | 2000