Impact motion of sphere landing on surface of moon or other planets with payload centrally supported from spherical skin by numerous cords is determined on assumption of uniform isentropic gas compression during impact; landing capabilities are determined for system containing suspension cords of constant cross section; effects of deviations in impact velocity and initial gas temperature are studied.


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    Titel :

    Design study of inflated sphere landing vehicle, including landing performance and effects of deviations from design conditions


    Weitere Titelangaben:

    NASA -- Tech Notes


    Beteiligte:
    Martin, E.D. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    82 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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