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)
By: J. Marroquin.
Contributors: Lyndon B. Johnson Space Center. Systems Engineering Division.; Chrysler Corporation. Electronics Products Division. Michoud Engineering Office. Data Management Services.
Series: NASA-CR -- 167,693.; NASA contractor report -- NASA CR-167693.
Publisher: Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration
Published: 1985
Place of publication: Houston, Tex
Language: eng
Format: Microform
Subjects: Von Karman Institute for Fluid Dynamics.; Hypersonic wind tunnels.; Supersonic wind tunnels.
Notes: Distributed to depository libraries in microfiche.

"March 1985."

"Prepared under NASA contract number NAS9-17179 by Data Management Services, Chrysler Military-Public Electronic Systems, Michoud Engineering Office."

"Space shuttle aerothermodynamic data report"--Prelim. p. [1].

"DMS-DR-2520."

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1985] 2 microfiches.