An edition of 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) (1985)

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)

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Results of A M = 5.3 heat transfer test of th ...
by John Marroquin.
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January 19, 2010 | History
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An edition of 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) (1985)

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)

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Publish Date
Publisher
Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration
Language
English

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Subjects
Transmission, Hypersonic wind tunnels, Heat

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Edition Availability
Cover of: 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)
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)
1985, Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration
Microform in English
  • Not in Library
Cover of: 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)
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)
1985, Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration
Microform in English

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Book Details

Edition 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.

Published in
Houston, Tex
Series
NASA-CR -- 167,695., NASA contractor report -- NASA CR-167695.

The Physical Object

Format
Microform
Pagination
1 v.

ID Numbers

Open Library
OL16119769M

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January 19, 2010 Edited by WorkBot add subjects and covers
December 11, 2009 Created by WorkBot add works page