LEADER 00811nam0 2200265 450 001 000025931 005 20090525125411.0 010 $a88-256-0935-3 100 $a20090525d1996----km-y0itay50------ba 101 0 $aita 102 $aIT 105 $ay-------001yy 200 1 $aUsare Java$fTim Ritchey 210 $aMilano$cJackson libri$d1996 215 $aXI, 329 p.$d24 cm$e1 CD-ROM 500 10$aJava$m$942882 610 1 $aElaboratori elettronici$aLinguaggio Java 610 1 $aWorld Wide Web 676 $a005.133$v20$9Specifici linguaggi di programmazione per elaboratori elettronici 700 1$aRitchey,$bTim$062495 801 0$aIT$bUNIPARTHENOPE$c20090525$gRICA$2UNIMARC 912 $a000025931 951 $cDSA$aM 005.133/93$bM 1319$d2009 996 $aJava$942882 997 $aUNIPARTHENOPE LEADER 01877nam 2200457 450 001 9910706207603321 005 20171106074509.0 035 $a(CKB)5470000002456366 035 $a(OCoLC)1009505919 035 $a(EXLCZ)995470000002456366 100 $a20171106j200011 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aMission advantages of constant power, variable Isp electrostatic thrusters /$fSteven R. Oleson 210 1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dNovember 2000. 215 $a1 online resource (9 pages) $cillustrations 225 1 $aNASA/TM ;$v2000-210477 300 $a"November 2000." 300 $a"Prepared for the 36th Joint Propulsion Conference and Exhibition sponsored by the American Institute of Aeronautics and Astronautics, Huntsville, Alabama, July 17-19, 2000." 300 $a"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page. 300 $a"AIAA-2000-3413." 320 $aIncludes bibliographical references (page 9). 606 $aElectrostatic propulsion$2nasat 606 $aSpecific impulse$2nasat 606 $aPropulsion system performance$2nasat 606 $aTrajectory planning$2nasat 615 7$aElectrostatic propulsion. 615 7$aSpecific impulse. 615 7$aPropulsion system performance. 615 7$aTrajectory planning. 700 $aOleson$b Steven R$g(Steven Robert),$f1964-$01391501 712 02$aNASA Glenn Research Center, 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910706207603321 996 $aMission advantages of constant power, variable Isp electrostatic thrusters$93541530 997 $aUNINA