The problem of optimal correction is formulated so that still before realization of the trajectory there are selected optimum, in the mean, weight relationships and optimum programs of rocket acceleration which will ensure maximum of payload on whose delivery it is possible to count on.


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    Title :

    Optimal Program of Correction in the Problem of Motion in a Gravitational Field with Limited Power


    Contributors:

    Publication date :

    1965


    Size :

    2 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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