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035   $a(CKB)5470000002528997
035   $a(OCoLC)846128595
035   $a(EXLCZ)995470000002528997
100   $a20130602j199801    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aComparison of high aspect ratio cooling channel designs for a rocket combustion chamber with development of an optimized design /$fby Mary F. Wadel
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dJanuary 1998.
215   $a1 online resource (approximately 78 pages) $cillustrations
225 1 $aNASA/TM ;$v1998-206313
300   $a"January 1998."
320   $aIncludes bibliographical references (pages 67-69).
606   $aRocket engines$2nasat
606   $aAspect ratio$2nasat
606   $aCombustion chambers$2nasat
608   $aAcademic theses.$2fast
615  7$aRocket engines.
615  7$aAspect ratio.
615  7$aCombustion chambers.
700   $aWadel$b Mary F.$01394787
712 02$aLewis Research Center,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCL
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910717122203321
996   $aComparison of high aspect ratio cooling channel designs for a rocket combustion chamber with development of an optimized design$93452546
997   $aUNINA