LEADER 02092nam  2200553   450 
001 9910707178803321
005 20160420131748.0
035   $a(CKB)5470000002461707
035   $a(OCoLC)946996679
035   $a(EXLCZ)995470000002461707
100   $a20160420j199608    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA performance comparison of two small rocket nozzles /$fLynn A. Arrington, Brian D. Reed, Angel Rivera, Jr
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dAugust 1996.
215   $a1 online resource (11 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v107285
300   $aTitle from title screen (viewed April 20, 2016).
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.
320   $aIncludes bibliographical references (pages 4-5).
606   $aConical nozzles$2nasat
606   $aRocket thrust$2nasat
606   $aRocket nozzles$2nasat
606   $aNozzle design$2nasat
606   $aReynolds number$2nasat
606   $aThrust chamber pressure$2nasat
606   $aFilm cooling$2nasat
615  7$aConical nozzles.
615  7$aRocket thrust.
615  7$aRocket nozzles.
615  7$aNozzle design.
615  7$aReynolds number.
615  7$aThrust chamber pressure.
615  7$aFilm cooling.
700   $aArrington$b Lynn A.$01386855
702   $aReed$b Brian D.
702   $aRivera$b Angel
712 02$aLewis Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707178803321
996   $aA performance comparison of two small rocket nozzles$93532049
997   $aUNINA