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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    Title :

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


    Additional title:

    NASA -- Tech Note


    Contributors:
    Smedal, H.A. (author) / Stinnett, G.W. (author) / Innis, R.C. (author)


    Publication date :

    1960


    Size :

    19 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :