01992nam 2200505 450 991070656940332120171122081458.0(CKB)5470000002456752(OCoLC)1012609278(EXLCZ)99547000000245675220171122j200103 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierThermal characterization of a NASA 30-cm ion thruster operated up to 5 kW /Timothy R. Sarver-Verhey, Matthew T. Domonkos, and Michael J. PattersonCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,March 2001.1 online resource (9 pages) illustrationsNASA/TM ;2001-210696"March 2001.""Prepared for the 36th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE, Huntsville, Alabama, July 16-19, 2000.""Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page."AIAA-2000-3816."Includes bibliographical references (page 5).Ion propulsionnasatRare earth elementsnasatElectromagnetsnasatIon enginesnasatThermodynamic propertiesnasatIon propulsion.Rare earth elements.Electromagnets.Ion engines.Thermodynamic properties.Sarver-Verhey Timothy R.1393050Domonkos Matthew T.Patterson Michael J.1959-NASA Glenn Research Center,GPOGPOBOOK9910706569403321Thermal characterization of a NASA 30-cm ion thruster operated up to 5 kW3532495UNINA