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An inertially guided missile with mid-course re-alignment

dc.contributor.advisorWalter Wrigley.en_US
dc.contributor.authorLindsay, Thomas Leighen_US
dc.contributor.authorPeterson, Carl Brynolfen_US
dc.date.accessioned2005-09-26T18:45:01Z
dc.date.available2005-09-26T18:45:01Z
dc.date.issued1961en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/28149
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1961.en_US
dc.descriptionIncludes bibliographical references (leaves 90-93).en_US
dc.description.statementofresponsibilityby Thomas Leigh Lindsay and Carl Brynolf Peterson.en_US
dc.format.extentvi, 93 leavesen_US
dc.format.extent5994255 bytes
dc.format.extent6005346 bytes
dc.format.mimetypeapplication/pdf
dc.format.mimetypeapplication/pdf
dc.language.isoen_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.titleAn inertially guided missile with mid-course re-alignmenten_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc33064748en_US


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