The effect of acceleration and deceleration on the dynamic stability of a missile
dc.contributor.author | Steinmetz, William John | 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.identifier.uri | http://hdl.handle.net/1853/12262 | |
dc.format.extent | 243 bytes | |
dc.format.mimetype | text/html | |
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 | Thesis | |
dc.description.degree | M.S. | |
dc.contributor.department | Aeronautical Engineering | en_US |
dc.description.advisor | Frank M. White, Jr. | |
dc.identifier.bibid | 784742 | en_US |
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Georgia Tech Theses and Dissertations [23403]
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School of Aerospace Engineering Theses and Dissertations [1409]
Original work by students of Aerospace Engineering