• 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