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dc.contributor.advisorPaul E. Sandorff.en_US
dc.contributor.authorPerkins, Charles Williamen_US
dc.date.accessioned2017-06-06T19:22:36Z
dc.date.available2017-06-06T19:22:36Z
dc.date.issued1960en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/109633
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1960.en_US
dc.descriptionIncludes bibliographical references (leaf 43).en_US
dc.description.statementofresponsibilityby Charles William Perkins.en_US
dc.format.extentvi, 43 leavesen_US
dc.language.isoengen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsMIT theses are protected by copyright. They may be viewed, downloaded, or printed from this source but further reproduction or distribution in any format is prohibited without written permission.en_US
dc.rights.urihttp://dspace.mit.edu/handle/1721.1/7582en_US
dc.subjectAeronautics and Astronauticsen_US
dc.titleOptimum retro-thrust trajectoriesen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronauticsen_US
dc.identifier.oclc32889615en_US


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