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Power subsystem approach for the Europa mission

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dc.contributor.author Ulloa-Severino, Antonio
dc.contributor.author Carr, Gregory A.
dc.contributor.author Clark, Douglas J.
dc.contributor.author Orellana, Sonny M.
dc.contributor.author Arrellano, Roxanne
dc.contributor.author Smart, Marshall C.
dc.contributor.author Bugga, Ratnakumar V.
dc.contributor.author Boca, Andreea
dc.contributor.author Dawson, Stephen F.
dc.date.accessioned 2019-06-06T19:38:41Z
dc.date.available 2019-06-06T19:38:41Z
dc.date.issued 2016-10-03
dc.identifier.citation European Space and Power Conference, Thessaloniki, Greece, October 3-7, 2016 en_US
dc.identifier.clearanceno 16-3998
dc.identifier.uri http://hdl.handle.net/2014/46212
dc.description.abstract NASA is planning to launch a spacecraft on a mission to the Jovian moon Europa, in order to conduct a detailed reconnaissance and investigation of its habitability. The spacecraft would orbit Jupiter and perform a detailed science investigation of Europa, utilizing a number of science instruments including an ice-penetrating radar to determine the icy shell thickness and presence of subsurface oceans. The spacecraft would be exposed to harsh radiation and extreme temperature environments. To meet mission objectives, the spacecraft power subsystem is being architected and designed to operate efficiently, and with a high degree of reliability. 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, 2016 en_US
dc.title Power subsystem approach for the Europa mission en_US
dc.type Preprint en_US


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