The patent relates to a rocket motor assembly for a rocket motor used for towing a load or extracting an aircrew member from an aircraft. The rocket motor is formed in two separate sections, a casing portion and a unitary nozzle igniter housing portion. The nozzle and igniter housing portion has a circumferential portion that mates with the internal surface wall of the casing portion. A seal and fastener holds the housing in place whenever the rocket motor is assembled. A shackle secured to the igniter mechanism is fastened to a tow line extending to a load to be towed.


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    Title :

    Rocket Nozzle Multi Function


    Contributors:
    J. A. Schmidt (author) / W. J. Stone (author)

    Publication date :

    1974


    Size :

    4 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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