2 options
Validation of high aspect ratio cooling in a 89 kN (20,000 lbf) thrust combustion chamber / Mary F. Wadel and Michael L. Meyer.
- Format:
- Book
- Government document
- Author/Creator:
- Wadel, Mary F., author.
- Meyer, Michael L., author.
- Series:
- NASA technical memorandum ; 107270.
- NASA technical memorandum ; 107270
- Language:
- English
- Subjects (All):
- Rocket engines.
- Combustion chambers.
- Liquid hydrogen.
- Cooling.
- cooling.
- Genre:
- technical reports.
- Technical reports
- Technical reports.
- Physical Description:
- 1 online resource (10 pages) : illustrations.
- Place of Publication:
- Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, June 1996.
- Notes:
- 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.
- Includes bibliographical references (page 10).
- "AIAA-96-2584."
- Other Format:
- Microfiche version: Wadel, Mary F. Validation of high aspect ratio cooling in a 89 kN (20,000 lb[sub f] thrust combustion chamber
- OCLC:
- 953734717
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