A helicopter construction is provided in which conventional vertical upward occupant-seat ejection apparatus may be used for ejecting the pilot. A hatch or door is provided in the fuselage above the pilot's seat. Explosive charges are provided so that the hub and its associated rotating blades may be rapidly removed to provide clearance for ejection through the door.


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    Title :

    Emergency Removal of Aircraft Sustaining Means


    Contributors:

    Publication date :

    1966


    Size :

    1 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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