02327nam 2200601 450 991070735600332120160719140110.0(CKB)5470000002463958(OCoLC)953734717(EXLCZ)99547000000246395820160719j199606 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierValidation of high aspect ratio cooling in a 89 kN (20,000 lbf) thrust combustion chamber /Mary F. Wadel and Michael L. MeyerCleveland, Ohio :National Aeronautics and Space Administration, Lewis Research Center,June 1996.1 online resource (10 pages) illustrationsNASA technical memorandum ;107270Title 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."AIAA-96-2584."Includes bibliographical references (page 10).Validation of high aspect ratio cooling in a 89 kN Rocket enginesnasatCombustion chambersnasatThrust chambersnasatMass flownasatLiquid hydrogennasatCoolingnasatHigh aspect rationasatPerformance testsnasatRocket engines.Combustion chambers.Thrust chambers.Mass flow.Liquid hydrogen.Cooling.High aspect ratio.Performance tests.Wadel Mary F.1394787Meyer Michael L.Lewis Research Center,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910707356003321Validation of high aspect ratio cooling in a 89 kN (20,000 lbf) thrust combustion chamber3458806UNINA