Combined plasma and thermal hollow cathode insert model

Katz, Ira; Polk, James E.; Mikellides, Ionnis G.; Goebel, Dan m.; Hornbeck, Sarah E.

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