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dc.contributor.advisorJean F. Louis.en_US
dc.contributor.authorSong, Seung Jinen_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.date.accessioned2007-02-21T10:02:31Z
dc.date.available2007-02-21T10:02:31Z
dc.date.copyright1988en_US
dc.date.issued1988en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/35935
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.en_US
dc.descriptionBibliography: leaves 103-104.en_US
dc.description.statementofresponsibilityby Seung Jin Song.en_US
dc.format.extent104 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.titleA comparison of fluid and heat control concepts for a binary Rankine cycle solar dynamic space power systemen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc18367613en_US


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