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Optimization of electrostatic dual-grid beam-deflection systemTests were performed to minimize accelerator grid erosion of a 5-cm diameter Kaufman ion thruster due to direct beam impingement. Several different screen hole diameters, pillow-shape-square screen holes, and dished screen grids were tried. The optimization was accomplished by copper plating the accelerator grid before testing each grid configuration on a thruster for a 2-hour run. The thruster beam sputtered copper and molybdenum from the accelerator grid where the beam impinged. The observed erosion patterns and measured accelerator currents were used to determine how to modify the accelerator system. The lowest erosion was obtained for a 50-percent open area pillow-shape-square-aperture screen grid, dished 0.043 centimeter convex toward the accelerator grid, which was positioned with the center of the screen grid 0.084 centimeter from the accelerator grid. During this investigation the accelerator current was reduced from 120 to 55 microamperes and was also more uniformly distributed over the area of the accelerator grid.
Document ID
19720020174
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Hudson, W. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Lathem, W. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Power, J. L.
(NASA Lewis Research Center Cleveland, OH, United States)
Banks, B. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1972
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-68096
E-7012
Report Number: NASA-TM-X-68096
Report Number: E-7012
Accession Number
72N27824
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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