A preliminary investigation of lower cost Mars missions which perform useful exploration objectives after the Viking/75 mission was conducted. As a study guideline, it was assumed that significant cost savings would be realized by utilizing Pioneer hardware currently being developed for a pair of 1978 Venus missions. This in turn led to the additional constraint of a 1979 launch with the Atlas/Centaur launch vehicle which has been designated for the Pioneer Venus missions. Two concepts, using an orbiter bus platform, were identified which have both good science potential and mission simplicity indicative of lower cost. These are: (1) an aeronomy/geology orbiter, and (2) a remote sensing orbiter with a number of deployable surface penetrometers.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Pioneer Mars 1979 mission options


    Beteiligte:

    Erscheinungsdatum :

    1974-01-29


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Pioneer MARS 1979 Mission Options

    A. L. Friedlander / W. K. Hartmann / J. C. Niehoff | NTIS | 1974


    Pioneer Mars 1979 Mission Options

    John C. Niehoff / Alan L. Friedlander | AIAA | 1975


    Pioneer Mars 1979 mission options

    Niehoff, J. C. / Friedlander, A. L. | NTRS | 1974


    Pioneer Mars 1979 mission options

    NIEHOFF, J. / FRIEDLANDER, A. | AIAA | 1974


    Solar Pioneer Mission Options

    Kerridge, S. R. / Evans, M. / Tsurutani, B. | NTRS | 1993