For abstract, see N76-11223.


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    Title :

    An Investigation in the NASA Msfc 14-Inch Trisonic Wind Tunnel to Determine the Pressure Distribution over the Components of a 0.004 Scale Version of the Rockwell Mcr 0074 Baseline Shuttle Ascent Configuration (Ia32f), Volume 2


    Contributors:

    Publication date :

    1975


    Size :

    704 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English