00821cam2 22002533 450 SOBE0007685420230728091122.020230728d2002 |||||ita|0103 baitaIT2Vittor Luigi CuneoMilanoGiuffrè2002P. 654-183524 cm001SOB0168642001 <<Le >>procedure concorsuali : natura, effetti, svolgimento / Vittor Luigi CuneoCuneo, Vittor LuigiAF00011079070229803ITUNISOB20230728RICAUNISOBUNISOB340110070SOBE00076854M 102 Monografia moderna SBNW340003732-2SI110070rovitoUNISOBUNISOB20230728091031.020230728091122.0rovito23403378UNISOB01601oam 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