Results of A M = 5.3 heat transfer test of the integrated vehicle using phase-change paint techniques on the 0.0175-scale model 56-OTS in the NASA/AMES Research Center 3.5-foot hypersonic wind tunnel (IH-42)
By: by John Marroquin.
Contributors: Lyndon B. Johnson Space Center. Systems Engineering Division.; Chrysler Corporation. Electronics Products Division. Michoud Engineering Office. Data Management Services.
Series: NASA-CR -- 167,695.; NASA contractor report -- NASA CR-167695.
Publisher: Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration
Published: 1985
Place of publication: Houston, Tex
Language: eng
Format: Microform
Subjects: Hypersonic wind tunnels.; Heat -- Transmission.
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-2524."

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1985] 1 microfiche.