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Comparison of 2-D and 3-D models of grid erosion in an ion thrusterNumerical results of particle-in-cell/Monte Carlo calculations of accelerator grid erosion in an ion thruster are presented. Specifically, it is shown that a three-dimensional model is required to account for the experimentally observed pitting of the accelerator grid between grid apertures. Some comparisons with earlier two-dimensional, axisymmetric model are made, and it is shown that, for identical operating conditions of the thruster, the wear-through time in the three-dimensional model is about two to three times higher than that obtained previously with the two-dimensional model, namely on the order of 10,000 hours for sample calculation.
Document ID
19910059508
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Peng, Xiaohang
(Tennessee Univ. Tullahoma, TN, United States)
Ruyten, Wilhelmus M.
(Tennessee Univ. Tullahoma, TN, United States)
Keefer, Dennis
(Tennessee, University Tullahoma, United States)
Date Acquired
August 15, 2013
Publication Date
June 1, 1991
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 91-2120
Accession Number
91A44131
Funding Number(s)
CONTRACT_GRANT: NAGW-1195
Distribution Limits
Public
Copyright
Other

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