LEADER 01871nam  2200505   450 
001 9910708661203321
005 20170405145307.0
035   $a(CKB)5470000002470613
035   $a(OCoLC)981463550
035   $a(EXLCZ)995470000002470613
100   $a20170405j199706    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aComparison of high aspect ratio cooling channel designs for a rocket combustion chamber /$fMary F. Wadel
210  1$aCleveland, Ohio:$cNational Aeronautics and Space Administration, Lewis Research Center,$dJune 1997.
215   $a1 online resource (11 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v107473
300   $a"June 1997."
300   $a"Performing organization: National Aeronautics and Space Administration, Lewis Research Center" Report documentation page.
300   $a"Prepared for the 33rd Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE, Seattle, Washington, July 6-9, 1997."
300   $a"AIAA-97-2913."
320   $aIncludes bibliographical references (page 11).
606   $aCombustion chambers$2nasat
606   $aHigh aspect ratio$2nasat
606   $aCooling$2nasat
606   $aChannels$2nasat
606   $aComputer programs$2nasat
606   $aDesign$2nasat
615  7$aCombustion chambers.
615  7$aHigh aspect ratio.
615  7$aCooling.
615  7$aChannels.
615  7$aComputer programs.
615  7$aDesign.
700   $aWadel$b Mary F.$01394787
712 02$aLewis Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910708661203321
996   $aComparison of high aspect ratio cooling channel designs for a rocket combustion chamber$93530315
997   $aUNINA