Functional relations are developed for ablation, insulation, and structural weights for ballistic-type entry vehicles as functions of vehicle and atmospheric properties; by application of these relations to range of possible model atmospheres for Mars, effects of these uncertainties on vehicle design weights and sizes are determined.


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    Titel :

    Effects of Mars atmospheric uncertainties on entry vehicle design


    Weitere Titelangaben:

    Aerospace Eng


    Beteiligte:
    Spiegel, J.M. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1962


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




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