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Characterization of an 8-cm Diameter Ion Source SystemResults of tests characterizing an 8-cm diameter ion source are presented. The tests were conducted in three separate vacuum test facilities at the University of Alabama-Huntsville, Colorado State University, and L3 Communications' ETI division. Standard ion optics tests describing electron backstreaming and total-voltage-limited impingement current behavior as a function of beam current were used as guidelines for selecting operating conditions where more detailed ion beam measurements were performed. The ion beam was profiled using an in-vacuum actuating probe system to determine the total ion current density and the ion charge state distribution variation across the face of the ion source. Both current density and ExB probes were utilized. The ion current density data were used to obtain integrated beam current, beam flatness parameters, and general beam profile shapes. The ExB probe data were used to determine the ratio of doubly to singly charged ion current. The ion beam profile tests were performed at over six different operating points that spanned the expected operating range of the DAWN thrusters being developed at L3. The characterization tests described herein reveal that the 8-cm ion source is suitable for use in (a) validating plasma diagnostic equipment, (b) xenon ion sputtering and etching studies of spacecraft materials, (c) plasma physics research, and (d) the study of ion thruster optics at varying conditions.
Document ID
20050207466
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Li, Zhongmin
(Alabama Univ. Huntsville, AL, United States)
Hawk, C. W.
(Alabama Univ. Huntsville, AL, United States)
Hawk, Clark W.
(Alabama Univ. Huntsville, AL, United States)
Buttweiler, Mark S.
(Colorado State Univ. Fort Collins, CO, United States)
Williams, John D.
(Colorado State Univ. Fort Collins, CO, United States)
Buchholtz, Brett
(Plasma Processes, Inc. Loveland, CO, United States)
Date Acquired
September 7, 2013
Publication Date
June 16, 2005
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AlAA Paper 2005-3882
Report Number: AlAA Paper 2005-3882
Meeting Information
Meeting: AIAA 41st Joint Propulsion Conference and Exhibit
Location: Tucson, AZ
Country: United States
Start Date: July 10, 2005
End Date: July 14, 2005
Funding Number(s)
CONTRACT_GRANT: NCC8-200
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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