Wind tunnel test results from shuttle solid rocket booster (SRB) sting interference tests were evaluated, yielding the general influence of the sting on the normal force and pitching moment coefficients and the side force and yawing moment coefficients. The procedures developed to determine the sting interference, the development of the corrected aerodynamic data, and the development of a new SRB aerodynamic mathematical model are documented.


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    Title :

    Space Shuttle Solid Rocket Booster Sting Interference Wind Tunnel Test Analysis


    Contributors:
    B. Conine (author) / W. Boyle (author)

    Publication date :

    1981


    Size :

    235 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English