Gorelov's solution for maximum time of active flight in horizontal plane at given finite mass is applied to particular problem where thrust applied during some parts of trajectory is used solely for sustaining constant altitude of flight.


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    Title :

    On problem of optimum rocket trajectories


    Additional title:

    K zadache ob optimal'nykh traektoriyakh rakety


    Contributors:

    Published in:

    Publication date :

    1964


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    Russian




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