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Ring cusp/hollow cathode discharge chamber performance studiesAn experimental study was performed to determine the effects of hollow cathode position, anode position, and ring cusp magnetic field configuration and strength on discharge chamber performance. The results are presented in terms of comparative plasma ion energy cost, extracted ion fraction, and beam profile data. Such comparisons are used to demonstrate whether changes in performance are caused by changes in the loss rate of primary electrons to the anode or the loss rate of ions to discharge chamber walls or cathode and anode surfaces. Results show: (1) the rate of primary electron loss to the anode decreases as the anode is moved downstream of the ring cusp toward the screen grid; (2) the loss rate of ions to hollow cathode surfaces are excessive if the cathode is located upstream of a point of peak magnetic flux density at the discharge chamber centerline; and (3) the fraction of the ions produced that are lost to discharge chamber walls and ring magnet surfaces is reduced by positioning of the magnet rings so the plasma density is uniform over the grid surface, and adjusting their strength to a level where it is sufficient to prevent excessive ion losses by Bohm diffusion.
Document ID
19890018377
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Vaughn, J. A.
(Colorado State Univ. Fort Collins, CO, United States)
Wilbur, Paul J.
(Colorado State Univ. Fort Collins, CO, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1988
Publication Information
Publication: DGLR, DGLR(AIAA)JSASS 20th International Electric Propulsion Conference: Proceedings
Subject Category
Spacecraft Propulsion And Power
Accession Number
89N27748
Funding Number(s)
CONTRACT_GRANT: NGR-06-002-112
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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