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dc.contributor.advisorDaniel E. Hastings.en_US
dc.contributor.authorTaneda, Hiroshien_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.date.accessioned2008-09-03T15:39:41Z
dc.date.available2008-09-03T15:39:41Z
dc.date.copyright1990en_US
dc.date.issued1990en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/42438
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1990.en_US
dc.descriptionIncludes bibliographical references (leaves 63-64).en_US
dc.description.statementofresponsibilityby Hiroshi Taneda.en_US
dc.format.extent76 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/1721.1/7582en_US
dc.subjectAeronautics and Astronautics.en_US
dc.titleThe effect of a plasma sheath on hypersonic flight communicationsen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc23935056en_US


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