Accession Number:

ADA059497

Title:

Heat Transfer Test on the NASA/Rockwell International Space Shuttle Orbiter at Mach number 8.0 in AEDC/VKF Tunnel B

Descriptive Note:

Final rept. 20 Feb-27 Apr 1978

Corporate Author:

ARO INC ARNOLD AFS TN

Personal Author(s):

Report Date:

1978-06-01

Pagination or Media Count:

66.0

Abstract:

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.

Subject Categories:

  • Thermodynamics
  • Unmanned Spacecraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE