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001 9910715945803321
005 20210414135328.0
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035   $a(OCoLC)760943043
035   $a(EXLCZ)995470000002516637
100   $a20111114j196807    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAnalysis of several methane-fueled engine cycles for Mach 3.0 flight /$fby Brent A. Miller
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dJuly 1968.
215   $a1 online resource (ii, 33 pages) $cillustrations
225 1 $aNASA/TN ;$vD-4699
300   $a"July 1968."
320   $aIncludes bibliographical references (page 33).
606   $aPropulsion system configurations$2nasat
606   $aTurbojet engines$2nasat
606   $aAirplanes$xFuel$2fast
606   $aAirplanes$xTurbojet engines$2fast
606   $aMethane$2fast
615  7$aPropulsion system configurations.
615  7$aTurbojet engines.
615  7$aAirplanes$xFuel.
615  7$aAirplanes$xTurbojet engines.
615  7$aMethane.
700   $aMiller$b Brent A.$01401342
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCO
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910715945803321
996   $aAnalysis of several methane-fueled engine cycles for Mach 3.0 flight$93469993
997   $aUNINA