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Author Perkins, H. Douglas, author.

Title Mach 5 to 7 RBCC propulsion system testing at NASA-LeRC HTF / H. Douglas Perkins, Scott R. Thomas, and William D. Pack.

Publication Info. Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, December 1996.

Copies

Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.15:107384    ---  Available
Description 1 online resource (13 pages) : illustrations.
text txt rdacontent
computer c rdamedia
online resource cr rdacarrier
Series NASA technical memorandum ; 107384
NASA technical memorandum ; 107384.
Note Title from title screen (viewed Aug. 3, 2016).
"December 1996"--Report documentation page.
"Prepared for the 35th Aerospace Sciences Meeting and Exhibit sponsored by the American Institute of Aeronautics and Astronautics, Reno, Nevada, January 6-10, 1997."
"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.
Engine tests.
Hypersonic speed.
Hypersonic wind tunnels.
Added Author Thomas, Scott R., author.
Pack, William D., author.
Lewis Research Center, issuing body.
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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