Results of mission and trajectory design for the Venus Orbiting Imaging Radar are presented. Because of the application of the aerobraking technique, for the first time to a planetary mission, the conventional mission design criteria in the selection of the launch/arrival dates must be modified and new mission constraints must be imposed. Venus itself poses an interesting aspect in trajectory design for an orbiting spacecraft due to its dense lower atmosphere and its slow retrograde rotation. Some recent results in the method of averaging applied to an orbiting spacecraft about this unique planet are given.


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    Titel :

    Mission and trajectory design for the Venus orbiting imaging radar


    Beteiligte:
    Kwok, J. H. (Autor:in)


    Erscheinungsdatum :

    01.01.1983


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    The Venus Orbiting Imaging Radar Mission

    Dallas, S. S. / Kwok, J. H. | NTRS | 1981


    The Venus Orbiting Imaging Radar /VOIR/ mission

    Gardner, J. A. / James, W. W. | NTRS | 1980


    Manned Venus Orbiting Mission

    Willis, E. A., Jr. | NTRS | 1967


    Manned Venus Orbiting Mission

    E. A. Willis | NTIS | 1967