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
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