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dc.contributor.advisorWalter M. Hollister.en_US
dc.contributor.authorRuss, David Phillipen_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.date.accessioned2007-01-10T15:50:55Z
dc.date.available2007-01-10T15:50:55Z
dc.date.copyright1988en_US
dc.date.issued1988en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/35340
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 David Phillip Russ.en_US
dc.format.extent70 leavesen_US
dc.format.extent2523039 bytes
dc.format.extent2695403 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.titleAnalysis of a heavy lift launch vehicle design using small liquid rocket enginesen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc19283930en_US


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