The integrated space shuttle vehicle was tested 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 points t = 0 sec, t = 1.25 sec, and t = 2 sec on the nominal SRB separation trajectory. (Author)


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    Title :

    Aerodynamic Results of Wind Tunnel Separation Tests on a 0.01-Scale Model (32-Ots) Space Shuttle Integrated Vehicle in the AEDC-Vkf-Swta (IA57)


    Contributors:

    Publication date :

    1974


    Size :

    574 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English