01601oam 2200469 450 991071712220332120220214112426.0(CKB)5470000002528997(OCoLC)846128595(EXLCZ)99547000000252899720130602j199801 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierComparison of high aspect ratio cooling channel designs for a rocket combustion chamber with development of an optimized design /by Mary F. WadelCleveland, Ohio :National Aeronautics and Space Administration, Lewis Research Center,January 1998.1 online resource (approximately 78 pages) illustrationsNASA/TM ;1998-206313"January 1998."Includes bibliographical references (pages 67-69).Rocket enginesnasatAspect rationasatCombustion chambersnasatAcademic theses.fastRocket engines.Aspect ratio.Combustion chambers.Wadel Mary F.1394787Lewis Research Center,OCLCEOCLCEOCLCQOCLCOOCLOCLCQGPOBOOK9910717122203321Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber with development of an optimized design3452546UNINA