Description |
1 online resource (13 pages) : illustrations. |
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text txt rdacontent |
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computer c rdamedia |
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online resource cr rdacarrier |
Series |
NASA technical memorandum ; 107384 |
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NASA technical memorandum ; 107384.
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Note |
Title from title screen (viewed Aug. 3, 2016). |
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"December 1996"--Report documentation page. |
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"Prepared for the 35th Aerospace Sciences Meeting and Exhibit sponsored by the American Institute of Aeronautics and Astronautics, Reno, Nevada, January 6-10, 1997." |
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"Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page. |
Bibliography |
Includes bibliographical references (pages 6-7). |
Type Of Report |
Technical memorandum. |
Funding |
Sponsored by the National Aeronautics and Space Administration WU-505-70-6B E-10577 |
Note |
"AIAA-97-0565." |
Subject |
Flexibility.
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Engine tests.
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Hypersonic speed.
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Hypersonic wind tunnels.
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Added Author |
Thomas, Scott R., author.
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Pack, William D., author.
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Lewis Research Center, issuing body.
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Added Title |
Mach five to seven rocket based combined cycle propulsion system testing at NASA Lewis Research Center hypersonic tunnel facility |
Other Form: |
Microfiche version: Perkins, H. Douglas. Mach 5 to 7 RBCC propulsion system testing at NASA-LeRC HTF (OCoLC)39728845 |
Gpo Item No. |
0830-H-15 (online) |
Sudoc No. |
NAS 1.15:107384 |
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