Results of study examining all emergency conditions and formulation of escape and rescue techniques; investigation is based on hypothetical vehicle capable of circular orbits from 200 to 19,350 nautical mi altitude and mission duration of 28 days; concepts considered are nose capsule re-entry escape vehicle for entire crew; spacecraft escape plus individual re-entry escape units; spacecraft escape plus ejection seats and space rescue by rendezvous; nose capsule re-entry escape vehicle concept is considered to be best overall system.


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    Titel :

    Emergency escape from multicrew earth orbital vehicles


    Weitere Titelangaben:

    Can Aeronautics Space J


    Beteiligte:
    Mavriplis, F. (Autor:in)


    Erscheinungsdatum :

    1963


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Emergency Earth Orbital Escape Device Patent Application

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