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dc.contributor.authorShaw, Edward Eugene.en_US
dc.date.accessioned2025-01-28T21:09:54Z
dc.date.available2025-01-28T21:09:54Z
dc.date.copyright1964en_US
dc.date.issued1964en_US
dc.identifier.urihttps://hdl.handle.net/1721.1/158115
dc.descriptionThesis: M.S., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 1964en_US
dc.descriptionIncludes bibliographical references (leaves 63-64).en_US
dc.description.statementofresponsibilityby Edward Eugene Shaw.en_US
dc.format.extentix, 64 leavesen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsMIT theses may be protected by copyright. Please reuse MIT thesis content according to the MIT Libraries Permissions Policy, which is available through the URL provided.en_US
dc.rights.urihttp://dspace.mit.edu/handle/1721.1/7582en_US
dc.subjectAeronautics and Astronauticsen_US
dc.titleNonrigid single-axis space integrator dynamicsen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronauticsen_US
dc.identifier.oclc34305857en_US
dc.description.collectionM.S. Massachusetts Institute of Technology, Department of Aeronautics and Astronauticsen_US
dspace.imported2025-01-28T21:09:54Zen_US
mit.thesis.degreeMasteren_US


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