Heat Transfer Test on the NASA/Rockwell International Space Shuttle Orbiter at Mach number 8.0 in AEDC/VKF Tunnel B
Final rept. 20 Feb-27 Apr 1978
ARO INC ARNOLD AFS TN
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Heat-transfer data were obtained on a 0.0175-scale and on a 0.04- scale model of the NASARockwell International Space Shuttle Orbiter. The data were obtained at mach 8 in the AEDCVKF Tunnel B at angles of attack from 25 to 42.5 deg and at several free-stream Reynolds numbers from 500,000 to 3,700,000 per ft.
- Unmanned Spacecraft