Model information and data from wind tunnel tests conducted on 0.04 scale 50 percent forebody models of the Space Shuttle Orbiter were presented. These tests were conducted using the phase change paint technique to determine aerodynamic heating rates due to various proturberances and recessions. Angles of attack from 20 deg through 45 deg were investigated at Mach 8.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Results of tests in the AEDC VKF Tunnel B using the phase change paint technique on 0.04 scale 50 percent forebody models (82-0) of the Rockwell space shuttle orbiter (OH50A)


    Contributors:
    Quan, M. (author)

    Publication date :

    1976-02-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English