Two programs, Hiltop I and Hiltop II, generate optimum trajectory data for electric propulsion missions of interest in exploration of solar system. Propulsion-system logic is activated by single program-input key; program modifications retain Hiltop I within framework of logic, so that Hiltop I input files, will run Hiltop II version and produce identical results as before.


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    Titel :

    Spacecraft trajectory


    Beteiligte:
    Horsewood, J. L. (Autor:in) / Mann, F. J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1980-06-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


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