An investigation was undertaken to determine the effect of windblast on the A/P22S-4 High Altitude Flying Outfit during simulated pilot ejection at a maximum sea-level flight Mach number of 0.91 (600 Knots). Two A/P22S-4 Outfits were tested. The integrity of both outfits was satisfactorily demonstrated, although slight damage resulted. The test further demonstrated that velcro tape is a satisfactory substitute for the lacing cord currently used for fastening the exterior cover and restraint layer at the ventilation port, altimeter, and controller locations. (Author)


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    Title :

    Windblast Test of High-Altitude Flying Outfit A/P22S-4


    Contributors:

    Publication date :

    1970


    Size :

    49 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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