Wind tunnel tests to determine subsonic stability and control effectiveness of straight and delta wing configurations on space shuttle booster


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    Title :

    Space shuttle: General Dynamics/Convair space shuttle booster. Investigation of subsonic stability and control effectiveness


    Contributors:
    Zombek, W. (author)

    Publication date :

    1970-11-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :