Basic development and test missions for Apollo manned lunar exploration program will be conducted on Saturn C-1 and C-5 launch vehicles; design of each vehicle is optimized for its mission objectives; Saturn C-1 objective is to place Apollo test command module in earth orbit; Saturn C-5 objective is to accomplish manned lunar-landing via rendezvous of 2 launches, then return to earth.


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    Titel :

    Launch vehicle design


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Pedigo, G.P. (Autor:in) / Orillion, A.G. (Autor:in)

    Kongress:

    SAE Meeting ; 1962 Design



    Erscheinungsdatum :

    1962


    Format / Umfang :

    34 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Launch Vehicle Design

    D. L. Dumbacher / S. R. Davis | NTIS | 2007


    Launch-vehicle design procedures.

    Hammock, D. M. | NTRS | 1964


    Launch Vehicle Systems Design Analysis

    RYAN, ROBERT / VERDERAIME, V.I. | AIAA | 1993


    Reusable launch vehicle design flexibility

    Allen, B. / Sauvageau, D. / Joyner, C. | AIAA | 1994


    Launch vehicle systems design analysis

    Ryan, Robert / Verderaime, V. | NTRS | 1993