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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    Titel :

    Angular Momentum and the Aircraft-Store Separation Problem


    Beteiligte:
    P. Daniels (Autor:in) / T. A. Clare (Autor:in)

    Erscheinungsdatum :

    1972


    Format / Umfang :

    16 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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