Theoretical NASA approach for rotationally constrained, prismatic bodies impacting smooth water is expanded to pitching, nonprismatic vehicle penetrating rough water; 2-re-entry vehicles are studied; with one, final descent is by parachute, whereas second impacts after subsonic glide; results for impacting in sea; normal load factors and rotational accelerations for variations in speed, descent path, and initial attitude; parachute vehicle seems better suited for rough water.


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    Titel :

    Water impact of manned spacecraft


    Weitere Titelangaben:

    ARS J


    Beteiligte:
    Mueller, W.H. (Autor:in) / Malakoff, J.L. (Autor:in)

    Erschienen in:

    ARS Journal ; 31 , n 12


    Erscheinungsdatum :

    1961


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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