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Progress in NEXT Ion Optics ModelingResults are presented from an ion optics simulation code applied to the NEXT ion thruster geometry. The error in the potential field solver of the code is characterized, and methods and requirements for reducing this error are given. Results from a study on electron backstreaming using the improved field solver are given and shown to compare much better to experimental results than previous studies. Results are also presented on a study of the beamlet behavior in the outer radial apertures of the NEXT thruster. The low beamlet currents in this region allow over-focusing of the beam, causing direct impingement of ions on the accelerator grid aperture wall. Different possibilities for reducing this direct impingement are analyzed, with the conclusion that, of the methods studied, decreasing the screen grid aperture diameter eliminates direct impingement most effectively.
Document ID
20040110839
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Emhoff, Jerold W.
(Michigan Univ. Ann Arbor, MI, United States)
Boyd, Iain D.
(Michigan Univ. Ann Arbor, MI, United States)
Date Acquired
September 7, 2013
Publication Date
August 1, 2004
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA Paper 2004-3786
NASA/CR-2004-213224
E-14731
Meeting Information
Meeting: 40th Joint Propulsion Conference and Exhibit
Location: Fort Lauderdale, FL
Country: United States
Start Date: July 11, 2004
End Date: July 14, 2004
Sponsors: American Inst. of Aeronautics and Astronautics, American Society for Electrical Engineers, Society of Automotive Engineers, Inc., American Society of Mechanical Engineers
Funding Number(s)
WBS: WBS 22-800-50-01
CONTRACT_GRANT: NAG3-2497
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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