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dc.contributor.advisorJoyce M. Warmkessel and Daniel E. Hastings.en_US
dc.contributor.authorMunson, Jeffrey Eric, 1974-en_US
dc.contributor.otherMassachusetts Institute of Technology. Technology and Policy Program.en_US
dc.date.accessioned2013-11-18T18:55:09Z
dc.date.available2013-11-18T18:55:09Z
dc.date.copyright2001en_US
dc.date.issued2001en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/82210
dc.descriptionThesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics; and, (S.M.)--Massachusetts Institute of Technology, Technology and Policy Program, 2001.en_US
dc.descriptionIncludes bibliographical references (p. 163-166).en_US
dc.description.statementofresponsibilityby Jeffrey Eric Munson.en_US
dc.format.extent166 p.en_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.subjectTechnology and Policy Program.en_US
dc.titleThe impact of launch vehicle constraints on space system designen_US
dc.typeThesisen_US
dc.description.degreeS.M.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.contributor.departmentTechnology and Policy Program
dc.identifier.oclc49887333en_US


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