Pilot/copilot protected crash-safety seat was designed and manufactured. Optimum seat and torso protection was attempted. Detail load and stress analysis for accelerations of 20 g vertically and 45 g longitudinally and laterally was made. By using crushable honeycomb type material, an improved torso restraint system and a variable attenuation mechanism were adopted. The feasibility of using protection media as a load bearing structure was demonstrated. (Author)


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    Titel :

    Armor Protection for Pilot/Copilot Seat with Crash Safety Features for CH-47a Helicopter


    Beteiligte:
    D. F. Thompson (Autor:in) / P. Harper (Autor:in)

    Erscheinungsdatum :

    1964


    Format / Umfang :

    2 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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