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.rights	Access restricted to authorized Georgia Tech users only.	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