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. (Author)


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    Title :

    Structural Load Reduction of the Space Shuttle Booster/Orbiter Configuration Using a Load Relief Guidance Technique


    Contributors:
    A. W. Deaton (author) / P. B. Kelley (author)

    Publication date :

    1973


    Size :

    34 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English