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035   $a(CKB)5470000002473619
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035   $a(OCoLC)995470000002473619
035   $a(EXLCZ)995470000002473619
100   $a20180730j198309    ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 00$aCombustion performance and heat transfer characterization of lox/hydrocarbon type propellants $efinal report, volume II
210  1$aHouston, Texas :$cNational Aeronautics and Space Administration, Lyndon B. Johnson Space Center,$dSeptember 1983.
215   $a1 online resource (xiv, 277 pages) $cillustrations
225 1 $aNASA/CR ;$v171714
300   $a"September 1983."
300   $a"15958T-1548-MA-129T-003F."
517   $aCombustion performance and heat transfer characterization of lox/hydrocarbon type propellants 
606   $aHeat transfer$2nasat
606   $aPerformance prediction$2nasat
606   $aThermal stability$2nasat
606   $aPressure gradients$2nasat
606   $aInjectors$2nasat
608   $aOnline resources.
615  7$aHeat transfer.
615  7$aPerformance prediction.
615  7$aThermal stability.
615  7$aPressure gradients.
615  7$aInjectors.
712 02$aLyndon B. Johnson Space Center,
712 02$aAerojet-General Corporation.$bLiquid Rocket Plant.
801  0$bGPO
801  1$bGPO
801  2$bMERUC
801  2$bGPO
906   $aBOOK
912   $a9910709863603321
996   $aCombustion performance and heat transfer characterization of lox$93269847
997   $aUNINA