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dc.contributor.authorSteinmetz, William Johnen_US
dc.date.accessioned2006-10-20T15:16:02Z
dc.date.available2006-10-20T15:16:02Z
dc.date.issued1962-12en_US
dc.identifier.urihttp://hdl.handle.net/1853/12262
dc.format.extent243 bytes
dc.format.mimetypetext/html
dc.language.isoen_US
dc.publisherGeorgia Institute of Technologyen_US
dc.rightsAccess restricted to authorized Georgia Tech users only.en_US
dc.subject.lcshGuided missilesen_US
dc.subject.lcshStabilityen_US
dc.subject.lcshOscillationsen_US
dc.titleThe effect of acceleration and deceleration on the dynamic stability of a missileen_US
dc.typeThesis
dc.description.degreeM.S.
dc.contributor.departmentAeronautical Engineeringen_US
dc.description.advisorFrank M. White, Jr.
dc.identifier.bibid784742en_US


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