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Combined plasma and thermal hollow cathode insert model

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dc.contributor.author Katz, Ira
dc.contributor.author Polk, James E.
dc.contributor.author Mikellides, Ionnis G.
dc.contributor.author Goebel, Dan m.
dc.contributor.author Hornbeck, Sarah E.
dc.date.accessioned 2005-11-11T22:59:18Z
dc.date.available 2005-11-11T22:59:18Z
dc.date.issued 2005-10
dc.identifier.citation The 29th International Electric Propulsion Conference (IPEC), Princeton, NJ, October 31 - November 4, 2005 en
dc.identifier.clearanceno 05-2948
dc.identifier.uri http://hdl.handle.net/2014/38059
dc.description.abstract In this paper, we present the first results from a Hollow Cathode Thermal (HCThermal) model that uses the spatially distributed plasma fluxes calculated by the InsertRegion of an Orificed Cathode (IROrCa2D) code as the heat source to predict the hollow cathode and insert temperatures. en
dc.description.sponsorship NASA en
dc.format.extent 187141 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 hollow cathode en
dc.subject ion thruster life en
dc.title Combined plasma and thermal hollow cathode insert model en
dc.type Preprint en


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