Results of aeroheating DFI and ET design-data test on a 0.0175-scale model 60-OTS conducted in the Von Karman gas dynamics facility (VKF) 40-inch supersonic and the 50-inch hypersonic wind tunnels A & C (IH-97A/B/C) /

Bibliographic Details

Main Author:	Marroquin, J. (Author)
Corporate Author:	Chrysler Corporation. Electronics Products Division. Michoud Engineering Office. Data Management Services
Format:	Government Document eBook
Language:	English
Published:	Houston, Texas : Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, March 1985.
Series:	NASA contractor report ; NASA CR-167693.
Subjects:	Von Karman Institute for Fluid Dynamics. Wind tunnel tests. Aerodynamic heating. External tanks. Space shuttles. Mach number.
Online Access:	https://purl.fdlp.gov/GPO/gpo107994