The stability criterion of a missile containing an internal spinning fly wheel is derived and the effect of this fly wheel on the missile's launch disturbance is explained. (Author)


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    Title :

    Angular Momentum and the Aircraft-Store Separation Problem


    Contributors:
    P. Daniels (author) / T. A. Clare (author)

    Publication date :

    1972


    Size :

    16 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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