Analysis of various transfer missions between parking orbits in cislunar space starting from initial 200 km parking orbit under optimum payload condition discloses interesting correlations between various systems of electric thrustors and missions performed; optimum payload can be calculated from basic formula for electric propulsion systems, which is given; calculated orbits can be correlated to different types of electric propulsion systems, with respect to exhaust velocity and total efficiency. In German with English and French abstracts.


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    Titel :

    Electric propulsion for cislunar missions


    Weitere Titelangaben:

    Elektrische Antriebe fuer cislunare Missionen


    Beteiligte:
    Au, G.F. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1966


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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