For abstract, see . The performance potential of ballistic flight mode is presented along with a study of alternate flight techniques. Orbit selection considerations are discussed in terms of the thermal environment of Mercury. Orbiter science experiments are summarized. Technology assessments were conducted for major subsystems appropriate to spin-stabilized and three-axis-stabilized spacecraft designs. Conclusions from this study are: ballistic mode Mercury orbiter missions offer adequate performance for effective follow-up of the MVM'73 science findings; the existing and programmed technology base is adequate for implementation of Mercury orbit spacecraft design; and when pending MVM flyby has been accomplished and the results analyzed, the data base will be adequate to support detailed orbiter spacecraft design efforts.


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    Title :

    Study of Ballistic Mode Mercury Orbiter Missions. Volume 2: Technical Report


    Contributors:
    W. S. Cook (author) / G. R. Hollenbeck (author) / P. S. Lewis (author) / D. G. Roos (author) / D. E. Wainwright (author)

    Publication date :

    1973


    Size :

    178 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English