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HiPEP Ion Optics System Evaluation Using GridletsExperimental measurements are presented for sub-scale ion optics systems comprised of 7 and 19 aperture pairs with geometrical features that are similar to the HiPEP ion optics system. Effects of hole diameter and grid-to-grid spacing are presented as functions of applied voltage and beamlet current. Recommendations are made for the beamlet current range where the ion optics system can be safely operated without experiencing direct impingement of high energy ions on the accelerator grid surface. Measurements are also presented of the accelerator grid voltage where beam plasma electrons backstream through the ion optics system. Results of numerical simulations obtained with the ffx code are compared to both the impingement limit and backstreaming measurements. An emphasis is placed on identifying differences between measurements and simulation predictions to highlight areas where more research is needed. Relatively large effects are observed in simulations when the discharge chamber plasma properties and ion optics geometry are varied. Parameters investigated using simulations include the applied voltages, grid spacing, hole-to-hole spacing, doubles-to-singles ratio, plasma potential, and electron temperature; and estimates are provided for the sensitivity of impingement limits on these parameters.
Document ID
20060006336
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Willliams, John D.
(Colorado State Univ. Fort Collins, CO, United States)
Farnell, Cody C.
(Colorado State Univ. Fort Collins, CO, United States)
Laufer, D. Mark
(Colorado State Univ. Fort Collins, CO, United States)
Martinez, Rafael A.
(Colorado State Univ. Fort Collins, CO, United States)
Date Acquired
September 7, 2013
Publication Date
July 13, 2004
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA Paper 2004-2814
NASA/CR-2006-213298
E-14745
Report Number: AIAA Paper 2004-2814
Report Number: NASA/CR-2006-213298
Report Number: E-14745
Meeting Information
Meeting: 40th AIAA Joint Propulsion Conference
Location: Ft. Lauderdale, FL
Country: United States
Start Date: July 11, 2004
End Date: July 14, 2004
Sponsors: American Inst. of Aeronautics and Astronautics, American Society of Mechanical Engineers, American Society for Engineering Education, Society of Automotive Engineers, Inc.
Funding Number(s)
CONTRACT_GRANT: NNC04GB20G
WBS: WBS 22-319-20-B2
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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