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Integrated vehicle and trajectory design of small spacecraft with electric propulsion for Earth and interplanetary missions

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dc.contributor.author Spangelo, Sara
dc.contributor.author Dalle, Derek
dc.contributor.author Longmier, Benjamin
dc.date.accessioned 2017-08-08T21:35:08Z
dc.date.available 2017-08-08T21:35:08Z
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 15-2910
dc.identifier.uri http://hdl.handle.net/2014/45844
dc.description.abstract This paper investigates the feasibility of Earth-transfer and interplanetary mission architectures for miniaturized spacecraft using emerging small solar electric propulsion technologies. 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 Integrated vehicle and trajectory design of small spacecraft with electric propulsion for Earth and interplanetary missions en_US
dc.type Presentation en_US


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