DocumentCode
928247
Title
Electromagnetic Earth-to-space launch
Author
Fair, Harry D. ; Coose, Phil ; Meinel, Carolyn P. ; Tidman, Derek A.
Author_Institution
Texas Univ., Austin, TX, USA
Volume
25
Issue
1
fYear
1989
fDate
1/1/1989 12:00:00 AM
Lastpage
89002
Abstract
The authors review several of the previous electromagnetic and electrothermal launch concepts and discuss the critical related technologies which are essential for the development of practical Earth-to-space launch systems. Selected missions and their requirements are discussed. Launcher concepts are briefly examined, and specific examples are given to demonstrate significant recent progress in hypervelocity atmospheric transit and hardening of launch vehicle components to withstand higher launch accelerators by several orders of magnitude. It is noted that these recent advances have significant impact on the payload which can be placed in orbit and have a major influence on the onboard propulsion requirements for orbit insertion. Based on technical achievements in all the critical supporting technologies, it is concluded that it is now feasible to demonstrate a credible electromagnet Earth-to-space launch system
Keywords
electromagnetic launchers; propulsion; Earth-to-space launch; electromagnetic launchers; electrothermal launch; hypervelocity atmospheric transit; launch accelerators; launch vehicle components; missions; onboard propulsion requirements; orbit insertion; payload; Chemical technology; Costs; Earth; Electromagnetic forces; Electromagnetic launching; Electrothermal launching; Road transportation; Space exploration; Space stations; Space technology;
fLanguage
English
Journal_Title
Magnetics, IEEE Transactions on
Publisher
ieee
ISSN
0018-9464
Type
jour
DOI
10.1109/20.22628
Filename
22628
Link To Document