LEADER 02070nam  2200613 a 450 
001 9910696936103321
005 20230902161808.0
035   $a(CKB)5470000002383532
035   $a(OCoLC)637173269
035   $a(EXLCZ)995470000002383532
100   $a20100604d2009      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aIntegrated high payoff rocket propulsion technology (IHPRPT) SiC recession model$b[electronic resource] /$fE.J. Opila
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2009]
215   $a1 online resource (45 pages) $cillustrations
225 1 $aNASA TM- ;$v2009-215650
300   $aTitle from title screen (viewed on June 3, 2010).
300   $a"December 2009."
410  0$aNASA technical memorandum ;$v2009-215650.
517   $aIntegrated high payoff rocket propulsion technology 
606   $aSilicon dioxide$2nasat
606   $aRocket engines$2nasat
606   $aCombustion$2nasat
606   $aThermochemistry$2nasat
606   $aLaminar boundary layer$2nasat
606   $aPropulsion$2nasat
606   $aThrust chambers$2nasat
606   $aGas viscosity$2nasat
606   $aGas transport$2nasat
606   $aFlow velocity$2nasat
606   $aCeramic matrix composites$2nasat
615  7$aSilicon dioxide.
615  7$aRocket engines.
615  7$aCombustion.
615  7$aThermochemistry.
615  7$aLaminar boundary layer.
615  7$aPropulsion.
615  7$aThrust chambers.
615  7$aGas viscosity.
615  7$aGas transport.
615  7$aFlow velocity.
615  7$aCeramic matrix composites.
700   $aOpila$b E$g(Elizabeth)$01405832
712 02$aNASA Glenn Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910696936103321
996   $aIntegrated high payoff rocket propulsion technology (IHPRPT) SiC recession model$93483116
997   $aUNINA