For abstract, see N76-16132.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Results of an investigation of the 0.003-scale space shuttle external tank MSFC model 460 in NASA/MSFC 14 x 14-inch trisonic wind tunnel to determine static pressure distributions during reentry (TA2F), volume 4


    Contributors:

    Publication date :

    1975-11-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English