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Jupiter icy moons orbiteer mission design overview

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dc.contributor.author Sims, Jon A.
dc.date.accessioned 2006-02-13T22:19:57Z
dc.date.available 2006-02-13T22:19:57Z
dc.date.issued 2006-01
dc.identifier.citation AAS/AIAA Space Flight Mechanics Meeting, Tampa, FL, January 22-26, 2006 en
dc.identifier.clearanceno 05-2875
dc.identifier.uri http://hdl.handle.net/2014/38571
dc.description.abstract An overview of the design of a mission to three large moons of Jupiter is presented. the Jupiter Icy Moons Orbiter (JIMO) mission uses ion thrusters powered by a nuclear reactor to transfer from Earth to Jupiter and enter a low-altitude science orbit around each of the moons. en
dc.description.sponsorship NASA en
dc.format.extent 2971541 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US en
dc.publisher Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2006. en
dc.subject mission design en
dc.subject low-thrust trajectory design en
dc.title Jupiter icy moons orbiteer mission design overview en
dc.type Preprint en


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