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Experimental and theoretical analysis for designing a grid clearing system for the NEXT ion propulsion system

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dc.contributor.author Anderson, John R.
dc.contributor.author Vaughan, David
dc.contributor.author Fitzgerald, Dennis
dc.date.accessioned 2005-10-13T21:36:13Z
dc.date.available 2005-10-13T21:36:13Z
dc.date.issued 2005-07
dc.identifier.citation 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Tucson, AZ, July 10-13, 2005 en
dc.identifier.clearanceno 05-1792
dc.identifier.uri http://hdl.handle.net/2014/37802
dc.description.abstract Screen to accelerator grid shorts have occurs on two NASA spacecraft using ion propulsion systems. This resulted in loss of thrusting capabilities on one of the spacecraft. en
dc.description.sponsorship NASA en
dc.format.extent 770764 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US en
dc.publisher Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2005. en
dc.subject ion thruster en
dc.subject ion optics en
dc.subject grid clear circuits en
dc.title Experimental and theoretical analysis for designing a grid clearing system for the NEXT ion propulsion system en
dc.type Preprint en


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