Use of restraint system in centrifuge program by Ames Research Center and Aviation Medical Acceleration Laboratory of Naval Air Development Center, to study ability of pilot in forward-facing position to control entry vehicle which employed lift; dynamics typical of entry vehicle were used and pilot was subjected to varied acceleration-time profiles which permitted thorough study of control problems.


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    Titel :

    Restraint system enabling pilot control under moderately high acceleration in varied acceleration field


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Smedal, H.A. (Autor:in) / Stinnett, G.W. (Autor:in) / Innis, R.C. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    19 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :