Saturn IB/Centaur- and Atlas/Centaur-launched electric propulsion vehicles employing near-future-solar cell power supplies (50 to 100 lb/kwe) are shown to be attractive systems for performing close solar probe emission; performance calculations include optimization of launch vehicle burnout velocity, electric stage specific impulse and power level, and thrust orientation for constant specific impulse thrusters; results obtained for constant-power operation of thrusters and solar-cell-powered electric systems.


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    Titel :

    Solar-electric propulsion system performance for close solar probe mission


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Strack, W.C. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1967


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :