The feasibility of a personnel escape capsule system for helicopters is shown. This feasibility was demonstrated by incorporating an escape system into an UH-25B helicopter and conducting tie-down, drop, and drone tests. The present status of designing this type of system into an operational helicopter such as the CH-46 and UH-1 helicopter is outlined.


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    Titel :

    Helicopter Personnel Escape and Survival System


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    National Aeronautic and Space Engineering and Manufacturing Meeting ; 1970



    Erscheinungsdatum :

    01.02.1970




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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