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100   $a20161206j199706    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aMetallized gelled propellants$eoxygen/RP-1/aluminum rocket engine calorimeter heat transfer measurements and analysis /$fBryan Palaszewski
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dJune 1997.
215   $a1 online resource (19 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v107495
300   $a"June 1997"--Report documentation page.
300   $a"Prepared for the 33rd Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE Seattle, Washington, July 6-9, 1997."
300   $a"Performing organization: National Aeronautics and Space Administration Lewis Research Center"--Report documentation page.
300   $a"AIAA-97-2974."
320   $aIncludes bibliographical references (pages 7-9).
517   $aMetallized gelled propellants 
606   $aGelled rocket propellants$2nasat
606   $aHeat measurement$2nasat
606   $aHeat transfer$2nasat
606   $aHeat flux$2nasat
606   $aRocket engines$2nasat
606   $aCalorimeters$2nasat
606   $aMetal combustion$2nasat
615  7$aGelled rocket propellants.
615  7$aHeat measurement.
615  7$aHeat transfer.
615  7$aHeat flux.
615  7$aRocket engines.
615  7$aCalorimeters.
615  7$aMetal combustion.
700   $aPalaszewski$b Bryan Alan Richard$01388221
712 02$aLewis Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707878703321
996   $aMetallized gelled propellants$93481363
997   $aUNINA