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dc.contributor.advisorManuel Martinez-Sanchez.en_US
dc.contributor.authorQarnain, Salma, 1974-en_US
dc.date.accessioned2005-08-19T14:25:17Z
dc.date.available2005-08-19T14:25:17Z
dc.date.copyright1998en_US
dc.date.issued1998en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/9943
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1998.en_US
dc.descriptionIncludes bibliographical references (leaves 68-70).en_US
dc.description.statementofresponsibilityby Salma Qarnain.en_US
dc.format.extent70 leavesen_US
dc.format.extent4514397 bytes
dc.format.extent4514153 bytes
dc.format.mimetypeapplication/pdf
dc.format.mimetypeapplication/pdf
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/1721.1/7582
dc.subjectAeronautics and Astronauticsen_US
dc.titleIssues regarding a complete computational model of a Hall thruster from the acceleration channel through the plumeen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc40253138en_US


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