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