LEADER 00967cam0-22003131i-450- 001 990000213170403321 005 20061102142015.0 035 $a000021317 035 $aFED01000021317 035 $a(Aleph)000021317FED01 035 $a000021317 100 $a20020821g19121913km-y0itay50------ba 101 0 $afre 102 $aFR 105 $aa-------001yy 200 1 $aTransport de force$ecalculs techniques et économiques des lignes de transport et de distribution d'énergie électrique$fCharles-Adolphe Le Roy 210 $aParis$cA. Hermann et fils$d1912-1913 215 $a2 v. (172; 143 p.)$cill.$d25 cm 610 0 $aEnergia elettrica$aDistribuzione 610 0 $aEnergia elettrica$aTrasporto 676 $a621.319 700 1$aLe Roy,$bCharles-Adolphe 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990000213170403321 952 $a13 L 03 08$b989$fFINBC 952 $a13 M 11 34$b990$fFINBC 959 $aFINBC 997 $aUNINA LEADER 02210nam 2200625I 450 001 9910707347903321 005 20160720144843.0 035 $a(CKB)5470000002464039 035 $a(OCoLC)953800695 035 $a(EXLCZ)995470000002464039 100 $a20160720j199701 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aRL10A-3-3A rocket engine modeling project /$fMichael Binder, Thomas Tomsik and Joseph P. Veres 210 1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dJanuary 1997. 215 $a1 online resource (176 pages) $cillustrations 225 1 $aNASA technical memorandum ;$v107318 300 $aTitle from title screen (viewed July 20, 2016). 300 $a"January 1997." 300 $a"Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page. 320 $aIncludes bibliographical references (pages 175-176). 606 $aRocket engines$2nasat 606 $aTurbomachinery$2nasat 606 $aPropulsion$2nasat 606 $aLaunch vehicles$2nasat 606 $aTitan launch vehicles$2nasat 606 $aAtlas launch vehicles$2nasat 606 $aCentaur launch vehicle$2nasat 606 $aComputerized simulation$2nasat 606 $aHeat of combustion$2nasat 606 $aHeat transfer$2nasat 615 7$aRocket engines. 615 7$aTurbomachinery. 615 7$aPropulsion. 615 7$aLaunch vehicles. 615 7$aTitan launch vehicles. 615 7$aAtlas launch vehicles. 615 7$aCentaur launch vehicle. 615 7$aComputerized simulation. 615 7$aHeat of combustion. 615 7$aHeat transfer. 700 $aBinder$b Michael$0374661 702 $aTomsik$b Thomas 702 $aVeres$b Joseph P. 712 02$aLewis Research Center, 712 02$aUnited States.$bNational Aeronautics and Space Administration, 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910707347903321 996 $aRL10A-3-3A rocket engine modeling project$93483163 997 $aUNINA