LEADER 01628oam 2200505 450 001 9910715945803321 005 20210414135328.0 035 $a(CKB)5470000002516637 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