A space shuttle booster/orbiter atmospheric ascent guidance algorithm is developed that will reduce the aerodynamically induced structural loads as compared to an open loop guidance algorithm.


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    Title :

    Structural load reduction of the space shuttle booster/orbiter configuration using a load relief guidance technique


    Contributors:

    Publication date :

    1973-04-05


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :