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Cassini-Huygens maneuver experience: first year of the Equinox Mission

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dc.contributor.author Gist, Emily M.
dc.contributor.author Ballard, Christopher G.
dc.contributor.author Hahn, Yungsun
dc.contributor.author Stumpf, Paul W.
dc.contributor.author Wagner, Sean V.
dc.contributor.author Williams, Powtawche N.
dc.date.accessioned 2015-06-09T17:44:02Z
dc.date.available 2015-06-09T17:44:02Z
dc.date.issued 2009-08-09
dc.identifier.citation AAS/AIAA Astrodynamics Specialist Conference, Pittsburgh, Pennsylvania, August 9-13, 2009 en_US
dc.identifier.clearanceno 09-2845
dc.identifier.uri http://hdl.handle.net/2014/45271
dc.description.abstract The Cassini-Huygens spacecraft was launched in 1997 on a mission to observe Saturn and its many moons. After a seven-year cruise, it entered a Saturnian orbit for a four-year, prime mission. Due to the success of the prime mission, spacecraft health, and remaining propellant, a two-year extended mission, the Equinox Mission, was approved. Maneuver designs and analyses performed through the first year of the Equinox Mission are presented. Results for the 46 most recent maneuvers are given. A substantial contribution to the navigation success of the Cassini-Huygens spacecraft is the continued accurate performance, which has exceeded the pre-launch expectations and requirements. 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, 2009 en_US
dc.title Cassini-Huygens maneuver experience: first year of the Equinox Mission en_US
dc.type Preprint en_US


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