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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 John Marroquin.

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Format:
Book
Government document
Author/Creator:
Marroquin, J., author.
Contributor:
Lyndon B. Johnson Space Center. Systems Engineering Division, issuing body.
Chrysler Corporation. Electronics Products Division. Michoud Engineering Office. Data Management Services
Series:
NASA contractor report ; NASA CR-167695.
NASA/CR ; 167695
Language:
English
Genre:
Online resources.
Physical Description:
1 online resource (iii, 27 pages) : illustrations.
Place of Publication:
Houston, Texas : Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, March 1985.
Notes:
"DMS-DR-2524."
"March 1985."
Includes bibliographical references (page 15).
Description based on online resource, PDF version; title from title page (NASA, viewed Aug. 24, 2018).
Other Format:
Microfiche version: Marroquin, J. Results of A M.
OCLC:
1049803547

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