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Characterization of Downstream Ion Energy Distributions From a High Current Hollow Cathode in a Ring Cusp Discharge ChamberThe presence of energetic ions produced by a hollow cathodes operating at high emission currents (greater than 10 Angstroms) has been documented in the literature. As part of an ongoing effort to uncover the underlying physics of the formation of these ions, ion efflux from a high current hollow cathode operating in an ion thruster discharge chamber was investigated. Using a spherical sector electrostatic energy analyzer located downstream of the discharge cathode, the ion energy distribution over a 0 to 60 eV energy range was measured. The sensitivity of the ion energy distribution function to zenith angle was also assessed at 3 different positions: 0, 15, and 25 degrees. The measurements suggest that the majority of the ion current at the measuring point falls into the analyzer with an energy approximately equal to the discharge voltage. The ion distribution, however, was found to be quite broad. The high energy tail of the distribution function tended to grow with increasing discharge current. Sensitivity of the profiles to flow rate at fixed discharge current was also investigated. A simple model is presented that provides a potential mechanism for the production of ions with energies above the discharge voltage.
Document ID
20040000779
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)
Date Acquired
September 7, 2013
Publication Date
October 1, 2003
Subject Category
Plasma Physics
Report/Patent Number
E-14146
AIAA Paper 2003-4865
NASA/TM-2003-212589
Report Number: E-14146
Report Number: AIAA Paper 2003-4865
Report Number: NASA/TM-2003-212589
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 Society of Mechanical Engineers, American Society for Electrical Engineers, Society of Automotive Engineers, Inc., American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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