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Variable specific impulse high power ion thruster

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dc.contributor.author Goebel, Dan M.
dc.contributor.author Brophy, John R.
dc.contributor.author Polk, James E.
dc.contributor.author Katz, Ira
dc.contributor.author Anderson, John
dc.date.accessioned 2005-10-13T22:17:49Z
dc.date.available 2005-10-13T22:17:49Z
dc.date.issued 2005-07
dc.identifier.citation 2005 AIAA Joint Propulsion Conference en
dc.identifier.clearanceno 05-1818
dc.identifier.uri http://hdl.handle.net/2014/37815
dc.description.abstract The power, Isp and thrust of ion thrusters are constrained by ther fixed grid gap in the ion accellerator, which limits performance and life to a limited range in Isp and thrust. en
dc.description.sponsorship NASA en
dc.format.extent 1520058 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 electric propulsion en
dc.subject ion optics en
dc.title Variable specific impulse high power ion thruster en
dc.type Preprint en


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