Determination of trajectory of rocket with constant acceleration assuming radial thrust of motor and based on initial conditions; deduced differential equation represents generalization of Binet's equation; finite equations of trajectory are determined by means of elliptic integrals of first and second kind.


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    Title :

    Considerations on rocket trajectories


    Additional title:

    Considerations sur la trajectoire des fusees


    Contributors:

    Published in:

    Publication date :

    1961


    Size :

    13 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    French




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