LEADER 02499nam 2200649I 450 001 9910707349003321 005 20160720135138.0 035 $a(CKB)5470000002464028 035 $a(OCoLC)953800161 035 $a(EXLCZ)995470000002464028 100 $a20160720j199608 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aMetallized gelled propellants $eoxygen/RP-1/aluminum rocket heat transfer and combustion measurements /$fBryan Palaszewski and James S. Zakany 210 1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dAugust 1996. 215 $a1 online resource (31 pages) $cillustrations 225 1 $aNASA technical memorandum ;$v107309 300 $aTitle from title screen (viewed July 20, 2016). 300 $a"August 1996"--Report documentation page. 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. 300 $a"AIAA-96-2622." 320 $aIncludes bibliographical references (pages 14-15). 517 $aMetallized gelled propellants 606 $aGelled propellants$2nasat 606 $aFlux quantization$2nasat 606 $aLiquid rocket propellants$2nasat 606 $aMetal propellants$2nasat 606 $aHeat transfer$2nasat 606 $aHeat flux$2nasat 606 $aMetal combustion$2nasat 606 $aTemperature profiles$2nasat 606 $aPropulsion system performance$2nasat 606 $aRocket engines$2nasat 615 7$aGelled propellants. 615 7$aFlux quantization. 615 7$aLiquid rocket propellants. 615 7$aMetal propellants. 615 7$aHeat transfer. 615 7$aHeat flux. 615 7$aMetal combustion. 615 7$aTemperature profiles. 615 7$aPropulsion system performance. 615 7$aRocket engines. 700 $aPalaszewski$b Bryan Alan Richard$01388221 702 $aZakany$b James S. 712 02$aLewis Research Center, 712 02$aUnited States.$bNational Aeronautics and Space Administration, 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910707349003321 996 $aMetallized gelled propellants$93481363 997 $aUNINA