Concept of Saturn V derivative launch vehicle systems, their performance capabilities, and their ability to perform orbital and high-energy missions at minimum total program cost; these derivative configurations have payload capability range extending from that of Saturn IB to postulated manned planetary vehicle requirements which might include placing larger nuclear modules/ stages in rendezvous compatible orbits about earth; vehicle and facilities design commonality and impact are summarized.


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    Titel :

    Saturn V derivatives


    Weitere Titelangaben:

    SAE -- Proc


    Beteiligte:
    Scott, R.D. (Autor:in) / Corcoran, W.L. (Autor:in)

    Kongress:

    Proceedings of Space Technology Conference ; 1968 Launching


    Erschienen in:

    Erscheinungsdatum :

    1968


    Format / Umfang :

    15 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Saturn V Derivatives

    Scott, Ronald D. / Corcoran, William L. | SAE Technical Papers | 1968


    Saturn V derivatives.

    Corcoran, W. L. / Scott, R. D. | NTRS | 1968



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