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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    Titel :

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


    Beteiligte:
    V. V. Tokarev (Autor:in)

    Erscheinungsdatum :

    1965


    Format / Umfang :

    2 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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