• 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