For abstract, see N76-16132.


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    Title :

    Results of an investigation of the 0.003-scale space shuttle external tank MSFC model 460 in the NASA/MSFC 14 x 14-inch Trisonic Wind Tunnel to determine static pressure distributions during reentry (TA2F), volume 5


    Contributors:

    Publication date :

    1975-11-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English