Studies by NASA have shown feasibility of using Apollo spacecraft, Saturn launch vehicles, and operating techniques for missions far more complex than lunar landings; missions include cometary intercepts, probes to asteroids, solar probes, flights out of ecliptic, flights to earth-moon libration points, and probes out of solar system; with fourth stage Saturn V will carry 31,000 lb to intercept with comet Encke, 20,000 lb to asteroid Ceres, 10,000 lb on two-tenths AU solar probe, and 5000 lb on "fast" probe to 40 AU (Astronautical Unit).


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    Titel :

    High energy missions for Saturn


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Gordon, T.J. (Autor:in) / Wheeler, D.D. (Autor:in)

    Kongress:

    SAE Meeting ; 1966



    Erscheinungsdatum :

    1966


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    High Energy Missions for Saturn

    Wheeler, D. D. / Gordon, T. J. | SAE Technical Papers | 1966


    Saturn Escape Options for Cassini Encore Missions

    Kloster, K. / Yam, C. / Longuski, J. | British Library Conference Proceedings | 2008


    Saturn Escape Options for Cassini Encore Missions

    Kloster, K.W. | Online Contents | 2009


    Saturn Escape Options for Cassini Encore Missions

    Kloster, Kevin / Yam, Chit Hong / Longuski, James | AIAA | 2008


    Saturn Escape Options for Cassini Encore Missions

    Kloster, Kevin W. / Yam, Chit Hong / Longuski, James M. | AIAA | 2009