• DocumentCode
    3201496
  • Title

    Isolated power supply for self-neutralization tests of a ferroelectric plasma thruster

  • Author

    Hutsel, B.T. ; Kovaleski, S.D. ; Kwon, J.W.

  • Author_Institution
    Dept. of Electr. & Comput. Eng., Univ. of Missouri, Columbia, MO, USA
  • fYear
    2009
  • fDate
    June 28 2009-July 2 2009
  • Firstpage
    1108
  • Lastpage
    1111
  • Abstract
    The ferroelectric plasma thruster (FEPT) is being developed for use in micro-spacecraft propulsion, large scale structure vibration damping, and proximity operations. An advantage of the FEPT over other thruster technologies such as colloid and field emission electric propulsion (FEEP) thrusters is that the FEPT operates with a single power supply. Additionally it is believed that the FEPT is self-neutralizing since both electrons and ions are accelerated to produce thrust. In order to test the self-neutralization capabilities of the FEPT, it must be operated with a power supply that is isolated from the ground of the vacuum chamber wall. Presented is the design of an isolated power supply to test the self-neutralization of the FEPT operating in a vacuum chamber.
  • Keywords
    aerospace propulsion; aerospace testing; electric propulsion; plasma applications; radiofrequency amplifiers; space vehicle power plants; colloid; ferroelectric plasma thruster; field emission electric propulsion thrusters; isolated power supply; large scale structure vibration damping; microspacecraft propulsion; proximity operation; radiofrequency amplifiers; self-neutralization tests; thruster technologies; Acceleration; Automatic testing; Damping; Electrons; Ferroelectric materials; Isolation technology; Large-scale systems; Plasmas; Power supplies; Propulsion;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Pulsed Power Conference, 2009. PPC '09. IEEE
  • Conference_Location
    Washington, DC
  • Print_ISBN
    978-1-4244-4064-1
  • Electronic_ISBN
    978-1-4244-4065-8
  • Type

    conf

  • DOI
    10.1109/PPC.2009.5386166
  • Filename
    5386166