The patent application relates to a device whereby the attitude of an airborne load is controlled by injecting fluid into the exhaust plume of a rocket motor which is attached to the load by gimbals and drives the load. In particular, it relates to apparatus and a method for controlling the attitude of a seat and a crew member sitting in the seat just after the seat and crew member have been ejected from an aircraft and before the crew member's parachute opens.


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    Title :

    Secondary Injection Actuated Gimbaled Motor


    Contributors:
    W. J. Stone (author)

    Publication date :

    1974


    Size :

    7 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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