The invention consists of a spin nozzle system for imparting a thrust to pre-spin a missile prior to launching. This system includes locating the spin nozzles within the outside diameter of the main missile motor. Also the nozzle exhaust gases are exited into the main motor exhaust cone to thereby augment the total missile thrust.


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    Title :

    Spin Nozzle and Thrust Augmentor Mechanism


    Contributors:

    Publication date :

    1975


    Size :

    3 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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