Next launch vehicle after Saturn C-5 should be capable of sizable increase in payload, reduction in direct operating costs, or both; survey of vehicles which possess this inherent potential; chemical and nuclear propelled vehicles are discussed for 1 or 2-stage-to-orbit applications, and winged fly-back boosters; paper shows that high chamber pressure LO2/LH2 engines of altitude compensating design present dramatic improvement over conventional engines; mixture ratio of 7 to 1 is economically superior to current ratio of 5 to 1. (See also ASME -- Paper 63-AHGT-89 for meeting Mar 3-7 1963 13 p)


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    Titel :

    Advanced launch vehicle concepts


    Weitere Titelangaben:

    Am Astronautical Soc -- Advances Astronautical Sci


    Beteiligte:
    Bono, P. (Autor:in)


    Erscheinungsdatum :

    1963


    Format / Umfang :

    25 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Advanced launch vehicle concepts

    Bono, P. | Engineering Index Backfile | 1963


    Advanced concepts for launch vehicle control

    Sifer, J.F. / Prouty, S.J. / Mak, P.H. | Tema Archiv | 1991


    Advanced concepts for launch vehicle control

    Sifer, J.F. / Prouty, S.J. / Mak, P.H. | IEEE | 1991


    Advanced concepts for launch vehicle control

    Sifer, J.F. / Prouty, S.J. / Mak, P.H. | Tema Archiv | 1990