Tabulated pressure data are presented on the right upper wing surface, right lower wing surface, and SRM booster of the integrated space shuttle vehicle configuration.


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    Title :

    Results of a Pressure Loads Investigation on a 0.030-Scale Model (47-Ots) of the Integrated Space Shuttle Vehicle Configuration 5 in the NASA Ames Research Center 11 X 11 Foot Leg of the Unitary Plan Wind Tunnel (Ia81a), Volume 6


    Contributors:
    E. Chee (author)

    Publication date :

    1975


    Size :

    775 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English