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Author

Title Validation of high aspect ratio cooling in a 89 kN (20,000 lbf) thrust combustion chamber / Mary F. Wadel and Michael L. Meyer.

Publication Info.

Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, June 1996.

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Connect to http://purl.fdlp.gov/GPO/gpo69478

Location	Call No.	OPAC Message	Status
Axe Federal Documents Online	NAS 1.15:107270	---	Available

Description	1 online resource (10 pages) : illustrations.
	text txt rdacontent
	computer c rdamedia
	online resource cr rdacarrier
Series	NASA technical memorandum ; 107270
	NASA technical memorandum ; 107270.
Note	Title from title screen (viewed July 19, 2016).
	"June 1996"--Report documentation page.
	"Prepared for the 32nd Joint Propulsion Conference cosponsored by AIAA, ASME, SAE, and ASEE, Lake Buena Vista, Florida, July 1-3, 1996."
	"Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
Bibliography	Includes bibliographical references (page 10).
Funding	Sponsored by the National Aeronautics and Space Administration WU-242-20-06 E-10337
Note	"AIAA-96-2584."
Subject	Rocket engines.
	Combustion chambers.
	Thrust chambers.
	Mass flow.
	Liquid hydrogen.
	Cooling.
	High aspect ratio.
	Performance tests.
Added Author	Meyer, Michael L., author.
	Lewis Research Center, issuing body.
	United States. National Aeronautics and Space Administration, sponsoring body.
Gpo Item No.	0830-H-15 (online)
Sudoc No.	NAS 1.15:107270