A breadboard design for a Flight Model Discharge System (FMDS) to prevent charging of spacecraft in geosynchronous orbit has been performed. Operational characteristics of the entire system are presented, including the electrostatic analyzer, surface potential monitor, transient pulse monitor, plasma source, and microprocessor-based controller. Design considerations that led to the final system configuration are also presented.


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    Titel :

    Flight Model Discharge System


    Beteiligte:
    R. R. Robson (Autor:in) / W. S. Williamson (Autor:in)

    Erscheinungsdatum :

    1985


    Format / Umfang :

    100 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Flight Model Discharge System

    R. R. Robson / W. S. Williamson / J. Santoru | NTIS | 1987


    Flight Model Discharge System

    R. R. Robson / W. W. Williamson | NTIS | 1988


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