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dc.contributor.advisorJack L. Kerrebrock.en_US
dc.contributor.authorSedwick, Raymond John, 1970-en_US
dc.date.accessioned2005-08-18T23:39:53Z
dc.date.available2005-08-18T23:39:53Z
dc.date.copyright1998en_US
dc.date.issued1998en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/10016
dc.descriptionThesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1998.en_US
dc.descriptionIncludes bibliographical references (leaves 155-156).en_US
dc.description.statementofresponsibilityby Raymond John Sedwick.en_US
dc.format.extent156 leavesen_US
dc.format.extent12366708 bytes
dc.format.extent12366464 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.titleAnalysis of an open cycle gas core nuclear propulsion system using HD driven vortices for fuel containmenten_US
dc.typeThesisen_US
dc.description.degreePh.D.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc39032131en_US


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