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dc.contributor.advisorJohn V. Harrington.en_US
dc.contributor.authorPeterson, Charles Alanen_US
dc.date.accessioned2005-08-15T15:00:35Z
dc.date.available2005-08-15T15:00:35Z
dc.date.issued1966en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/12946
dc.descriptionMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1966. M.S.en_US
dc.descriptionBibliography: leaf 42.en_US
dc.format.extentiv, 42 leavesen_US
dc.format.extent5052045 bytes
dc.format.extent5051804 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 Astronauticsen_US
dc.titleUse of thermal reradiative effects in spacecraft attitude control.en_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc26024673en_US


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