LEADER 02327nam  2200601   450 
001 9910707356003321
005 20160719140110.0
035   $a(CKB)5470000002463958
035   $a(OCoLC)953734717
035   $a(EXLCZ)995470000002463958
100   $a20160719j199606    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aValidation of high aspect ratio cooling in a 89 kN (20,000 lbf) thrust combustion chamber /$fMary F. Wadel and Michael L. Meyer
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dJune 1996.
215   $a1 online resource (10 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v107270
300   $aTitle from title screen (viewed July 19, 2016).
300   $a"June 1996"--Report documentation page.
300   $a"Prepared for the 32nd Joint Propulsion Conference cosponsored by AIAA, ASME, SAE, and ASEE, Lake Buena Vista, Florida, July 1-3, 1996."
300   $a"Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
300   $a"AIAA-96-2584."
320   $aIncludes bibliographical references (page 10).
517   $aValidation of high aspect ratio cooling in a 89 kN 
606   $aRocket engines$2nasat
606   $aCombustion chambers$2nasat
606   $aThrust chambers$2nasat
606   $aMass flow$2nasat
606   $aLiquid hydrogen$2nasat
606   $aCooling$2nasat
606   $aHigh aspect ratio$2nasat
606   $aPerformance tests$2nasat
615  7$aRocket engines.
615  7$aCombustion chambers.
615  7$aThrust chambers.
615  7$aMass flow.
615  7$aLiquid hydrogen.
615  7$aCooling.
615  7$aHigh aspect ratio.
615  7$aPerformance tests.
700   $aWadel$b Mary F.$01394787
702   $aMeyer$b Michael L.
712 02$aLewis Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707356003321
996   $aValidation of high aspect ratio cooling in a 89 kN (20,000 lbf) thrust combustion chamber$93458806
997   $aUNINA