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Compact high-g, efficient folding wing for a cannon-launched reconaissance vehicle

dc.contributor.advisorCharles Boppe, Carlos E.S. Cesnik and Mark Drela.en_US
dc.contributor.authorCasiez, Thierry D. (Thierry Dominique), 1975-en_US
dc.date.accessioned2005-08-19T14:22:50Z
dc.date.available2005-08-19T14:22:50Z
dc.date.copyright1998en_US
dc.date.issued1998en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/9938
dc.descriptionThesis (M. Eng.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1998.en_US
dc.descriptionIncludes bibliographical references (p. 91).en_US
dc.description.statementofresponsibilityby Thierry D. Casiez.en_US
dc.format.extent104 p.en_US
dc.format.extent7575837 bytes
dc.format.extent7575596 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.titleCompact high-g, efficient folding wing for a cannon-launched reconaissance vehicleen_US
dc.typeThesisen_US
dc.description.degreeM.Eng.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc40160120en_US


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