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Investigation and development of a high voltage propellant isolator for ion thrusters
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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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JPL TRS 1992+
JPL TRS 1992+
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