• DocumentCode
    1020232
  • Title

    EMET technology for rail launchers

  • Author

    Burton, R.L. ; Goldstein, S.A. ; Tidman, D.A. ; Wang, S.Y. ; Winsor, N.K. ; Witherspoon, F.D.

  • Author_Institution
    GT-Devices, Alexandria, VA
  • Volume
    22
  • Issue
    6
  • fYear
    1986
  • fDate
    11/1/1986 12:00:00 AM
  • Firstpage
    1410
  • Lastpage
    1415
  • Abstract
    The EMET concept is a marriage of electrothermal plasma jet technology with rail accelerators using plasma armatures. By injecting a structured plasma immediately behind a moving projectile prior to the current pulse, the plasma armature properties can be highly controlled. Parameters of interest are the armature mass and length, molecular weight, specific heat ratio gamma, and temperature. Proper control of these parameters leads to control of problems facing rail launchers such as wall ablation and viscous wall drag. In support of EMET, a Material Test Facility (MTF) has been developed for performing basic physics and materials research on hypervelocity launchers, by making direct measurements of the plasma pressure and jet velocity in a 1 cm bore. These measurements are then compared with theoretical models for various types of plasmas, in order to understand and eliminate barrel ablation. The paper discusses measurement techniques used on MTF, and the approaches being taken to develop EMET in the laboratory.
  • Keywords
    Electromagnetic propulsion; Electrothermal materials/devices; Electrothermal effects; Performance evaluation; Plasma accelerators; Plasma materials processing; Plasma measurements; Plasma properties; Plasma temperature; Projectiles; Rails; Test facilities;
  • fLanguage
    English
  • Journal_Title
    Magnetics, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9464
  • Type

    jour

  • DOI
    10.1109/TMAG.1986.1064670
  • Filename
    1064670