Several closed form trajectory solutions have been developed for low-thrust interplanetary flight and used with patched conics for analysis of combined propulsion systems. The solutions provide insight into alternative types of Mars missions, and show considerable mass savings for fast crewed missions with outbound trip times on the order of 90--100 days. 7 refs.


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    Titel :

    Closed form low-thrust trajectories for Mars missions


    Beteiligte:
    J. W. Purvis (Autor:in)

    Erscheinungsdatum :

    1992


    Format / Umfang :

    4 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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