Methods for determining optimum stage-weight distribution and ascending trajectory of multistage rockets have individually been described; these two problems are inherently inseparable and are not independent of each other; unified numerical method integrating these two optimization problems for satellite laucching vehicles is explained; also, numerical examples concerning finding of optimum vehicle to place 150 kg weight satellite into circular orbit at height of 1000 km are given. (In Japanese with English abstract) (Rec'd 1968)


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    Title :

    Optimization of staging and trajectory for satellite launching vehicles


    Additional title:

    Mitsubishi Heavy Industries, Ltd -- Tech Bul


    Contributors:
    Matsubara, H. (author) / Yamada, Y. (author) / Nakanishi, H. (author)


    Publication date :

    1966


    Size :

    18 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    Japanese


    Keywords :


    Optimization of staging and trajectory for satellite launching vehicles

    Matsubara, Hideo / Yamada, Yuji / Nakanishi, Hideki | TIBKAT | 1966


    Method of weight prediction of satellite launching vehicles

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    MSAT satellite launching

    Online Contents | 1995