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dc.contributor.advisorAlan H. Epstein.en_US
dc.contributor.authorGroshenry, Christopheen_US
dc.date.accessioned2005-08-18T20:12:53Z
dc.date.available2005-08-18T20:12:53Z
dc.date.copyright1995en_US
dc.date.issued1995en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/10386
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1995.en_US
dc.descriptionIncludes bibliographical references (p. 127-129).en_US
dc.description.statementofresponsibilityby Christophe Groshenry.en_US
dc.format.extent129 p.en_US
dc.format.extent5982607 bytes
dc.format.extent5982368 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.titlePreliminary design study of a micro-gas turbine engineen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc37545265en_US


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