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
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