DocumentCode
1373265
Title
Can electric actuators meet missile requirements?
Author
Newton, G. C. ; Rasche, R. W.
Author_Institution
Massachusetts Institute of Technology, Cambridge, Mass.
Volume
80
Issue
5
fYear
1961
Firstpage
306
Lastpage
312
Abstract
ONE OF THE vital components of a missile is the device used to position the thrust directors or control surfaces. In addition to satisfying rather stringent dynamic performance requirements, this device must be highly reliable. Missile designers favor hydraulically operated actuators because of their high dynamic performance capabilities, relatively low weight, and small size.1 However, the hydraulic actuators have still not reached the desired reliability because of sensitivity to dirt particles and other factors.
Keywords
Actuators; Armature; Equations; Missiles; Permanent magnet motors; Servomotors; Torque;
fLanguage
English
Journal_Title
American Institute of Electrical Engineers, Part II: Applications and Industry, Transactions of the
Publisher
ieee
ISSN
0097-2185
Type
jour
DOI
10.1109/TAI.1961.6371761
Filename
6371761
Link To Document