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Investigation and development of a high voltage propellant isolator for ion thrusters

Investigation and development of a high voltage propellant isolator for ion thrusters

Hart, Stephen L.; Tighe, William; Pearce, Charles; Goebel, Dan M.
URI: http://hdl.handle.net/2014/37751
Date: 2005-10
Keywords: ion thruster; electric propulsion; flow isolator
Publisher: Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2005.
Citation: 29th International Electric Propulsion Conference, Princeton, NJ, October 31 - November 4, 2005

Abstract:

We will report on the test apparatus, calibrations of the system, the test procedure used and results for 13, 20 and 30-segment isolators.

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