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The effect of a plasma sheath on hypersonic flight communications

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dc.contributor.advisor Daniel E. Hastings. en_US
dc.contributor.author Taneda, Hiroshi en_US
dc.contributor.other Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. en_US
dc.date.accessioned 2008-09-03T15:39:41Z
dc.date.available 2008-09-03T15:39:41Z
dc.date.copyright 1990 en_US
dc.date.issued 1990 en_US
dc.identifier.uri http://hdl.handle.net/1721.1/42438
dc.description Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1990. en_US
dc.description Includes bibliographical references (leaves 63-64). en_US
dc.description.statementofresponsibility by Hiroshi Taneda. en_US
dc.format.extent 76 leaves en_US
dc.language.iso eng en_US
dc.publisher Massachusetts Institute of Technology en_US
dc.rights M.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.uri http://dspace.mit.edu/handle/1721.1/7582 en_US
dc.subject Aeronautics and Astronautics. en_US
dc.title The effect of a plasma sheath on hypersonic flight communications en_US
dc.type Thesis en_US
dc.description.degree M.S. en_US
dc.contributor.department Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. en_US
dc.identifier.oclc 23935056 en_US


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