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Discharge Characterization of 40 cm-Microwave ECR Ion Source and NeutralizerDischarge characteristics of a 40 cm, 2.45 GHz Electron Cyclotron Resonance (ECR) ion thruster discharge chamber and neutralizer were acquired. Thruster bulk discharge plasma characteristics were assessed using a single Langmuir probe. Total extractable ion current was measured as a function of input microwave power and flow rate. Additionally, radial ion current density profiles at the thruster.s exit plane were characterized using five equally spaced Faraday probes. Distinct low and high density operating modes were observed as discharge input power was varied from 0 to 200 W. In the high mode, extractable ion currents as high as 0.82 A were measured. Neutralizer emission current was characterized as a function of flow rate and microwave power. Neutralizer extraction currents as high as 0.6 A were measured.
Document ID
20040000780
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Foster, John E.
(NASA Glenn Research Center Cleveland, OH, United States)
Patterson, Michael J.
(NASA Glenn Research Center Cleveland, OH, United States)
Britton, Melissa
(QSS Group, Inc. Cleveland, OH, United States)
Date Acquired
August 21, 2013
Publication Date
October 1, 2003
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA Paper 2003-5012
NASA/TM-2003-212590
E-14147
NAS 1.15:212590
Report Number: AIAA Paper 2003-5012
Report Number: NASA/TM-2003-212590
Report Number: E-14147
Report Number: NAS 1.15:212590
Meeting Information
Meeting: 39th Joint Propulsion Conference and Exhibit
Location: Huntsville, AL
Country: United States
Start Date: July 20, 2003
End Date: July 23, 2003
Sponsors: American Inst. of Aeronautics and Astronautics, American Society for Electrical Engineers, American Society of Mechanical Engineers, Society of Automotive Engineers, Inc.
Funding Number(s)
WBS: WBS 22-755-70-04
Distribution Limits
Public
Copyright
Public Use Permitted.
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