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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    Title :

    Ballistic equations for seven degree of freedom rocket


    Additional title:

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


    Contributors:
    Wilms, E. (author)


    Publication date :

    1961


    Size :

    77 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English




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