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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    Titel :

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


    Beteiligte:
    J. R. Hochwalt (Autor:in)

    Erscheinungsdatum :

    1970


    Format / Umfang :

    49 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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