• DocumentCode
    855631
  • Title

    Earth-to-orbit railgun launcher

  • Author

    Brown, J.L. ; Jamison, K.A. ; Johnson, N.E. ; Rolader, G.E. ; Scanlon, J.J., III ; Coutee, P.W.

  • Author_Institution
    Science Applications Int. Corp., Shalimar, FL, USA
  • Volume
    29
  • Issue
    1
  • fYear
    1993
  • fDate
    1/1/1993 12:00:00 AM
  • Firstpage
    373
  • Lastpage
    378
  • Abstract
    An overview of a comprehensive study of the feasibility of launching relatively small payloads into orbit using electromagnetic launcher technology is provided. The specific question addressed was whether serious consideration should be given to hypervelocity gun launch to space as an alternative to conventional rocket powered launch vehicles. An overview of the concept developed is provided along with a discussion of the major subsystems. The above question is answered in the affirmative, because the mission can readily be accomplished using state-of-the-art technology; a considerable cost savings is offered with respect to conventional rocket launch systems; and a revolutionary launch frequency, comfortably placing six payloads in orbit each day, is possible, which greatly increases operation flexibility
  • Keywords
    electromagnetic launchers; Earth-to-orbit railgun launcher; electromagnetic launcher; hypervelocity gun launch; Batteries; Electromagnetic launching; Inductors; Packaging; Payloads; Pulsed power supplies; Railguns; Rockets; Space technology; Vehicles;
  • fLanguage
    English
  • Journal_Title
    Magnetics, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9464
  • Type

    jour

  • DOI
    10.1109/20.195603
  • Filename
    195603