A high acceleration cockpit design test/evaluation program was conducted, using a full scale design aid. Alternate configurations were compared using this full scale design aid in a formally structured evaluation including mission related task elements. Test criteria considered evaluation of control/display and cockpit design options, including seat location, motion, and pilot anthropometry, with a balance between the physical and operational test measures and objectives using Air Force provided pilot subjects. (Author)


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    Title :

    High Acceleration Cockpits for Advanced Fighter Aircraft. Volume IV. Test Results


    Contributors:
    C. F. Asiala (author) / T. J. Quinn (author)

    Publication date :

    1974


    Size :

    94 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English