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 :
بازگشت