A system for controlling the potential of a vehicle (rocket or satellite) in flight by use of an emitted current of low energy electrons is described. Diagnostic instruments for measuring the efficacy of such a system are discussed. Results of the use of such a system on a sounding rocket launched into the lower ionosphere are presented.


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    Titel :

    Vehicle Potential Control by Means of Electron Emission


    Beteiligte:
    C. Sherman (Autor:in)

    Erscheinungsdatum :

    1975


    Format / Umfang :

    32 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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