Plotted and tabulated aerodynamic coefficient data from a wind tunnel test of the integrated space shuttle vehicle are presented. The primary test objective was to determine proximity force and moment data for the orbiter/external tank and solid rocket booster (SRB) with and without separation rockets firing for both single and dual booster runs. Data were obtained at three points (t = 0, 1.25, and 2.0 seconds) on the nominal SRB separation trajectory. (Author)


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    Title :

    Aerodynamic Results of Wind Tunnel Tests on a 0.010-Scale Model (32-Qts) Space Shuttle Integrated Vehicle in the AEDC Vkf-40-Inch Supersonic Wind Tunnel (IA61)


    Contributors:

    Publication date :

    1976


    Size :

    642 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English