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Experimental and computational investigation of the performance of a micro-ion thruster

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dc.contributor.author Wirz, R. en_US
dc.contributor.author Polk, J. en_US
dc.contributor.author Marrese, C. en_US
dc.contributor.author Mueller, J. en_US
dc.date.accessioned 2004-09-17T06:46:06Z
dc.date.available 2004-09-17T06:46:06Z
dc.date.issued 2002-07-09 en_US
dc.identifier.citation Joint Propulsion Conference en_US
dc.identifier.citation Indianapolis, IN, USA en_US
dc.identifier.clearanceno 02-1625 en_US
dc.identifier.uri http://hdl.handle.net/2014/9409
dc.description.abstract A micro-ion thruster assembly with a characteristic diameter of 3-cm has been developed at JPL for testing and optimization of various system parameters. en_US
dc.format.extent 2791475 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other micro-ion thruster ion propulsion electric propulsion en_US
dc.title Experimental and computational investigation of the performance of a micro-ion thruster en_US


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