SERT-I spacecraft, in final stage of development, will provide measurements of thrustor electrical parameters and thrust during 1 hr ballistic flight; tests to be carried out will determine validity of ion thrustor performance data, obtained in vacuum chambers; spacecraft, to carry two thrustors of different construction, will be launched into ballistic trajectory by NASA Scout vehicle; ion thrustor design and principle of operation; essential components are subsystems for propellant feed, ionization, accelerating electrode, and beam neutralization; instrumentation and telemetry; structural details of spacecraft.


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    Titel :

    Spacecraft for ion thruster flight tests


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Gold, H. (Autor:in)

    Kongress:

    SAE Meeting ; 1964 Power supply



    Erscheinungsdatum :

    1964


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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