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Attitude control system for the high energy transient experiment small satellite

dc.contributor.advisorAndreas von Flotow.en_US
dc.contributor.authorChang, Daniel Hen_US
dc.date.accessioned2008-09-03T15:49:56Z
dc.date.available2008-09-03T15:49:56Z
dc.date.copyright1991en_US
dc.date.issued1991en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/42493
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.en_US
dc.descriptionIncludes bibliographical references (p. 207-208).en_US
dc.description.statementofresponsibilityby Daniel H. Chang.en_US
dc.format.extent261 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 Astronauticsen_US
dc.titleAttitude control system for the high energy transient experiment small satelliteen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc25601150en_US


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