The patent relates to a method whereby the spin rate of a rocket missile is controlled by bevelling the inside of the leading edge of the missile fins. Altering the bevel angle controls the rate of spin. The spin rate is also controlled by sweeping back the leading edges of the fins.


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    Title :

    Method of Controlling the Spin Rate of Tube Launched Rockets


    Contributors:
    C. T. Orzechowski (author) / N. Seiden (author) / A. Mycka (author)

    Publication date :

    1974


    Size :

    3 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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