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dc.contributor.advisorManuel Martinez-Sanchez.en_US
dc.contributor.authorRen, Chiang-Hwaen_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.date.accessioned2007-09-28T13:34:23Z
dc.date.available2007-09-28T13:34:23Z
dc.date.copyright1989en_US
dc.date.issued1989en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/39017
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.en_US
dc.descriptionIncludes bibliographical references (leaves 73-74).en_US
dc.description.statementofresponsibilityby Chiang-Hwa Ren.en_US
dc.format.extent141 leavesen_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/1721.1/7582
dc.subjectAeronautics and Astronautics.en_US
dc.titleA computer based model for the performance analysis of a SCRAMJET propulsion systemen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc20404694en_US


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