Validation of high aspect ratio cooling in a 89 kN (20,000 lb[sub f]) thrust combustion chamber
By: Mary F. Wadel and Michael L. Meyer.
Contributors: Meyer, Michael L.; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 107270.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1996
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Rocket engines.; Combustion chambers.; Thrust chambers.; Mass flow.; Liquid hydrogen.; Cooling.; High aspect ratio.; Performance tests.
Notes: Shipping list no.: 98-0769-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.