Family of indirect transfer trajectories between circular orbits is used to evaluate mass ratio required to complete round-trip interplanetary missions; results indicate that trajectories yield substantial reductions in total time for low and high thrust vehicles, and that space vehicles propelled with electric rockets may produce greater reductions than high-thrust nuclear rockets.


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    Titel :

    Fast interplanetary missions with low-thrust propulsion systems


    Weitere Titelangaben:

    NASA -- Tech Report


    Beteiligte:
    Moeckel, W.E. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    56 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :