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dc.contributor.advisorManuel Martinez-Sanchez.en_US
dc.contributor.authorBrenizer, David Marshall, 1976-en_US
dc.contributor.otherMassachusetts Institute of Technology. Department of Aeronautics and Astronautics.en_US
dc.date.accessioned2013-09-12T19:16:31Z
dc.date.available2013-09-12T19:16:31Z
dc.date.copyright2000en_US
dc.date.issued2000en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/80648
dc.descriptionThesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2000.en_US
dc.descriptionIncludes bibliographical references (p. 111-112).en_US
dc.description.statementofresponsibilityby David Marshall Brenizer.en_US
dc.format.extent128 p.en_US
dc.language.isoengen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsM.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission.en_US
dc.rights.urihttp://dspace.mit.edu/handle/1721.1/7582en_US
dc.subjectAeronautics and Astronautics.en_US
dc.titleHybrid-PIC modeling of Hall thruster plumesen_US
dc.typeThesisen_US
dc.description.degreeS.M.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc48384777en_US


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