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dc.contributor.advisorManuel Martinez-Sanchez.en_US
dc.contributor.authorRobertson, Darrel Kim, 1974-en_US
dc.date.accessioned2010-01-07T20:34:13Z
dc.date.available2010-01-07T20:34:13Z
dc.date.copyright1998en_US
dc.date.issued1998en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/50388
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1998.en_US
dc.descriptionIncludes bibliographical references (p. 158-162).en_US
dc.description.statementofresponsibilityby Darrel Kim Robertson.en_US
dc.format.extent162 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 Astronauticsen_US
dc.titleA two-dimensional, non-equilibrium numerical model of an alkali seeded hydrogen arcjet thrusteren_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc40170151en_US


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