An aircraft is provided with an ejectable encapsulated individual seat and a rocket structure for separating it from the aircraft. The rocket structure includes two coaxially aligned rocket tubes containing rocket propellant. A housing carries the nozzles. The rockets are fired by firing pins responsive to generated gas pressure.


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    Title :

    Ejection Apparatus


    Contributors:
    A. M. Stott (author)

    Publication date :

    1966


    Size :

    1 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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