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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    Title :

    Vehicle Potential Control by Means of Electron Emission


    Contributors:
    C. Sherman (author)

    Publication date :

    1975


    Size :

    32 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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