JPL Technical Report Server

Variable specific impulse high power ion thruster

Show simple item record Goebel, Dan M. Brophy, John R. Polk, James E. Katz, Ira Anderson, John 2005-10-13T22:17:49Z 2005-10-13T22:17:49Z 2005-07
dc.identifier.citation 2005 AIAA Joint Propulsion Conference en
dc.identifier.clearanceno 05-1818
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

Files in this item

This item appears in the following Collection(s)

Show simple item record



My Account