• DocumentCode
    1244482
  • Title

    Electromagnetic aircraft launch system-EMALS

  • Author

    Doyle, M.R. ; Samuel, D.J. ; Conway, T. ; Klimowski, R.R.

  • Author_Institution
    Aircraft Div., Naval Air Warfare Center, Lakehurst, NJ, USA
  • Volume
    31
  • Issue
    1
  • fYear
    1995
  • Firstpage
    528
  • Lastpage
    533
  • Abstract
    With the proliferation of electromagnetic launch systems presently being designed, built, or studied, there appears to be no limit to their application. One of the intriguing applications is electromagnetically catapulting aircraft from the deck of an aircraft carrier. The US Navy had foreseen the substantial capabilities of an electromagnetic catapult in the 1940s and built a prototype. However, it was not until the recent technical advances in the areas of pulsed power, power conditioning, energy storage devices, and controls gave credence to a fieldable electromagnetic aircraft launch system. This paper presents the U.S. Navy´s Electromagnetic Aircraft Launch System (EMALS) being developed in partnership with Kaman Electromagnetics (Hudson, MA). It addresses the EMALS´s present design and the technologies involved, as well as the ship and operational impacts, advantages, disadvantages, and compatibility issues for today´s and tomorrow´s carriers.<>
  • Keywords
    aerospace propulsion; aircraft; capacitor storage; cycloconvertors; electromagnetic launchers; military aircraft; military equipment; pulsed power technology; ships; EMALS; US Navy; aircraft carrier; applications; catapulting; controls; design; electromagnetic aircraft launch system; energy storage devices; power conditioning; pulsed power; technologies; Aerospace control; Control systems; EMP radiation effects; Electromagnetic devices; Electromagnetic fields; Electromagnetic launching; Energy storage; Military aircraft; Power conditioning; Prototypes;
  • fLanguage
    English
  • Journal_Title
    Magnetics, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9464
  • Type

    jour

  • DOI
    10.1109/20.364638
  • Filename
    364638