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035   $a(OCoLC)995470000002473616
035   $a(EXLCZ)995470000002473616
100   $a20180730j198304    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 00$aCombustion performance and heat transfer characterization of lox/hydrocarbon type propellants $efinal report, volume I
210  1$aHouston, Texas :$cNational Aeronautics and Space Administration, Lyndon B. Johnson Space Center,$dApril 1983.
215   $a1 online resource (viii, 134 pages) $cillustrations
225 1 $aNASA/CR ;$v171713
300   $a"April 1983."
300   $a"15958T-1548-MA-129T-003."
517   $aCombustion performance and heat transfer characterization of lox/hydrocarbon type propellants 
606   $aHeat transfer coefficients$2nasat
606   $aLiquid oxygen$2nasat
606   $aEthyl alcohol$2nasat
606   $aSpace shuttles$2nasat
606   $aLow Earth orbits$2nasat
615  7$aHeat transfer coefficients.
615  7$aLiquid oxygen.
615  7$aEthyl alcohol.
615  7$aSpace shuttles.
615  7$aLow Earth orbits.
712 02$aLyndon B. Johnson Space Center,
712 02$aAerojet-General Corporation.$bLiquid Rocket Plant.
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910709863903321
996   $aCombustion performance and heat transfer characterization of lox$93269847
997   $aUNINA