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Comparison of optimal small spacecraft micro electric propulsion technologies for mission opportunities

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dc.contributor.author Spangelo, Sara
dc.date.accessioned 2017-08-08T21:33:09Z
dc.date.available 2017-08-08T21:33:09Z
dc.date.issued 2015-08-08
dc.identifier.citation 29th Annual AIAA/USU Conference on Small Satellites, Logan, Utah, August 8-13, 2015 en_US
dc.identifier.clearanceno 15-2361
dc.identifier.uri http://hdl.handle.net/2014/45832
dc.description.abstract The goal of this paper is to explore the mission opportunities that are uniquely enabled by U-class Solar Electric Propulsion (SEP) technologies. This paper aims to develop and apply a common system-level modeling framework to evaluate these thrusters for relevant upcoming mission scenarios. en_US
dc.description.sponsorship NASA/JPL en_US
dc.language.iso en_US en_US
dc.publisher Pasadena, CA: Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2015 en_US
dc.title Comparison of optimal small spacecraft micro electric propulsion technologies for mission opportunities en_US
dc.type Presentation en_US


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