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Development of a 2D Axisymmetric Electron Fluid Model in Hall Thrusters
dc.contributor.authorDragnea, Horatiu C.
dc.contributor.authorHara, Kentaro
dc.contributor.authorBoyd, Iain D.
dc.date.accessioned2018-04-11T19:04:28Z
dc.date.available2018-04-11T19:04:28Z
dc.date.issued2017
dc.identifier.citationDragnea, Horatiu C.; Hara, Kentaro; Boyd, Iain D. (2017). "Development of a 2D Axisymmetric Electron Fluid Model in Hall Thrusters." 53rd AIAA/SAE/ASEE Joint Propulsion Conference
dc.identifier.urihttps://hdl.handle.net/2027.42/143094
dc.publisherAmerican Institute of Aeronautics and Astronautics
dc.relation.ispartofseriesAIAA Propulsion and Energy Forum
dc.titleDevelopment of a 2D Axisymmetric Electron Fluid Model in Hall Thrusters
dc.typeConference Paperen_US
dc.subject.hlbsecondlevelAerospace Engineering
dc.subject.hlbtoplevelEngineering
dc.description.peerreviewedPeer Reviewed
dc.description.bitstreamurlhttps://deepblue.lib.umich.edu/bitstream/2027.42/143094/1/6.2017-4632.pdf
dc.identifier.doi10.2514/6.2017-4632
dc.identifier.source53rd AIAA/SAE/ASEE Joint Propulsion Conference
dc.owningcollnameAerospace Engineering, Department of


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