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dc.contributor.advisorWallace E. Vander Velde.
dc.contributor.authorMillers, Hans-Fredrik.en_US
dc.date.accessioned2022-10-17T20:01:28Z
dc.date.available2022-10-17T20:01:28Z
dc.date.copyright1964en_US
dc.date.issued1964en_US
dc.identifier.urihttps://hdl.handle.net/1721.1/145875
dc.descriptionThesis: M.S., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 1964en_US
dc.descriptionIncludes bibliographical references (leaves 88-89).en_US
dc.description.statementofresponsibilityby Hans-Fredrik Millers.en_US
dc.format.extentxi, 89 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.titleA re-entry control system using delta-modulated accelerometers and a DDA-computeren_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronauticsen_US
dc.identifier.oclc34233041en_US
dc.description.collectionM.S. Massachusetts Institute of Technology, Department of Aeronautics and Astronauticsen_US
dspace.imported2022-10-17T20:01:28Zen_US
mit.thesis.degreeMasteren_US


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