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dc.contributor.advisorRudrapatna V. Ramnath.en_US
dc.contributor.authorLe Fur, Philippeen_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.date.accessioned2008-02-04T20:50:01Z
dc.date.available2008-02-04T20:50:01Z
dc.date.copyright1989en_US
dc.date.issued1989en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/40134
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.en_US
dc.descriptionIncludes bibliographical references (leaves 96-97).en_US
dc.description.statementofresponsibilityby Philippe Le Fur.en_US
dc.format.extent102 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.titleAn asymptotic approach in the preliminary design of a launch vehicle control systemen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc20404668en_US


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