Title:
The effect of acceleration and deceleration on the dynamic stability of a missile

dc.contributor.advisor White, Frank M.
dc.contributor.author Steinmetz, William John en_US
dc.contributor.department Aeronautical Engineering en_US
dc.date.accessioned 2006-10-20T15:16:02Z
dc.date.available 2006-10-20T15:16:02Z
dc.date.issued 1962-12 en_US
dc.description.degree M.S.
dc.format.extent 243 bytes
dc.format.mimetype text/html
dc.identifier.bibid 784742 en_US
dc.identifier.uri http://hdl.handle.net/1853/12262
dc.language.iso en_US
dc.publisher Georgia Institute of Technology en_US
dc.subject.lcsh Guided missiles en_US
dc.subject.lcsh Stability en_US
dc.subject.lcsh Oscillations en_US
dc.title The effect of acceleration and deceleration on the dynamic stability of a missile en_US
dc.type Text
dc.type.genre Thesis
dspace.entity.type Publication
local.contributor.corporatename College of Engineering
local.contributor.corporatename Daniel Guggenheim School of Aerospace Engineering
local.relation.ispartofseries Master of Science in Aerospace Engineering
local.relation.ispartofseries Master of Science in Aerospace Engineering
relation.isOrgUnitOfPublication 7c022d60-21d5-497c-b552-95e489a06569
relation.isOrgUnitOfPublication a348b767-ea7e-4789-af1f-1f1d5925fb65
relation.isSeriesOfPublication 2fef2987-f871-4c1d-acfa-e642641793f5
relation.isSeriesOfPublication 09844fbb-b7d9-45e2-95de-849e434a6abc
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