Requirements placed on entry vehicles by advanced missions involving maneuvering entry from near-earth orbit and earth entry on return from manned Mars mission; vehicles with lift-drag ratios near unity are found attractive; results from studies of aerodynamic and heat-transfer characteristics of M-2 lifting body are applied to analysis of maneuverable entry vehicles; heat-shield studies are combined with other results to estimate effects of crew size and volume on entry-vehicle weight.


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    Titel :

    Some considerations of performance of maneuverable, lifting-body, entry vehicle


    Weitere Titelangaben:

    Am Astronautical Soc -- Advances Astronautical Sciences


    Beteiligte:
    Syvertson, C.A. (Autor:in) / Swenson, B.L. (Autor:in) / Anderson, J.L. (Autor:in) / Kenyon, G.C. (Autor:in)


    Erscheinungsdatum :

    1963


    Format / Umfang :

    21 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    SOME CONSIDERATIONS OF THE PERFORMANCE OF A MANEUVERABLE, LIFTING-BODY, ENTRY VEHICLE

    Anderson, J. L. / Kenyon, G. C. / Swenson, B. L. et al. | NTRS | 1963


    HIGHLY MANEUVERABLE VEHICLE

    MEAGER BENJAMIN | Europäisches Patentamt | 2023

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    HIGHLY MANEUVERABLE VEHICLE

    MEAGER BENJAMIN | Europäisches Patentamt | 2023

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    An entry monitor system for maneuverable vehicles.

    FRANK, A. J. / JOHNSON, B. C. | AIAA | 1966