General formulation of equations of motion for rocket consisting of 2 units rotating relative to each other about aerodynamic axis of symmetry; effects of rotation, and variation in gravitational field of Earth, as well as mass unbalance of rocket are taken into account.


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    Titel :

    Ballistic equations for seven degree of freedom rocket


    Weitere Titelangaben:

    Illinois Univ -- Dept Theoretical Applied Mechanics -- T A M Report


    Beteiligte:
    Wilms, E. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    77 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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