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Modeling Neutral Densities Downstream of a Gridded Ion ThrusterThe details of a model for determining the neutral density downstream of a gridded ion thruster are presented. An investigation of the possible sources of neutrals emanating from and surrounding a NEXT ion thruster determined that the most significant contributors to the downstream neutral density include discharge chamber neutrals escaping through the perforated grids, neutrals escaping from the neutralizer, and vacuum facility background neutrals. For the neutral flux through the grids, near- and far-field equations are presented for rigorously determining the neutral density downstream of a cylindrical aperture. These equations are integrated into a spherically-domed convex grid geometry with a hexagonal array of apertures for determining neutral densities downstream of the ion thruster grids. The neutrals escaping from an off-center neutralizer are also modeled assuming diffuse neutral emission from the neutralizer keeper orifice. Finally, the effect of the surrounding vacuum facility neutrals is included and assumed to be constant. The model is used to predict the neutral density downstream of a NEXT ion thruster with and without neutralizer flow and a vacuum facility background pressure. The impacts of past simplifying assumptions for predicting downstream neutral densities are also examined for a NEXT ion thruster.
Document ID
20110000536
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Soulas, George C.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 25, 2013
Publication Date
December 1, 2010
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA Paper 2010-216930
E-17507
NASA/TM-2010-216930
Report Number: AIAA Paper 2010-216930
Report Number: E-17507
Report Number: NASA/TM-2010-216930
Meeting Information
Meeting: 49th Joint Propulsion Conference and Exhibit
Location: Nashville, TN
Country: United States
Start Date: July 25, 2010
End Date: July 28, 2010
Sponsors: American Inst. of Aeronautics and Astronautics, American Society of Mechanical Engineers, American Society for Electrical Engineers, Society of Automotive Engineers, Inc.
Funding Number(s)
WBS: WBS 346620.04.08.02.02.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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