Load relief autopilot to minimize launch vehicle thrust vector deflection angle required for vehicle stability during flight through design winds


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    Title :

    Load relief autopilot analysis to minimize launch vehicle peak thrust vector deflection requirements


    Contributors:
    Scalzott, L. L. (author) / Teren, F. (author)

    Publication date :

    1968-09-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :