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dc.contributor.advisorRichard H. Battin, Gilbert S. Stubbs.en_US
dc.contributor.authorCorvin, Michael Alexanderen_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.date.accessioned2005-08-09T16:53:59Z
dc.date.available2005-08-09T16:53:59Z
dc.date.copyright1988en_US
dc.date.issued1988en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/14371
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.en_US
dc.descriptionIncludes bibliographical references.en_US
dc.description.statementofresponsibilityby Michael Alexander Corvin.en_US
dc.format.extent108 p.en_US
dc.format.extent7732524 bytes
dc.format.extent7732286 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 Astronautics.en_US
dc.titleAscent guidance for a winged boost vehicleen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc20054837en_US


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