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Maneuver design for the Juno mission: inner cruise

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dc.contributor.author Pavlak, Thomas A.
dc.contributor.author Frauenholz, Raymond B.
dc.contributor.author Bordi, John J.
dc.contributor.author Kangas, Julie A.
dc.contributor.author Helfrich, Clifford E.
dc.date.accessioned 2016-06-06T19:40:18Z
dc.date.available 2016-06-06T19:40:18Z
dc.date.issued 2014-08-05
dc.identifier.citation AIAA Space 2014, San Diego, California, August 5-7, 2014 en_US
dc.identifier.clearanceno 14-2698
dc.identifier.uri http://hdl.handle.net/2014/45612
dc.description.abstract The Juno spacecraft launched in August 2011 and, following a successful Earth flyby in October 2013, is on course for a nominal orbit insertion at Jupiter in July 2016. This paper examines the design and execution of deterministic and statistical trajectory correction maneuvers during the first approximately 27 months of post-launch operations that defined the "Inner Cruise" phase of the Juno mission. Topics of emphasis include the two deep space maneuvers, Earth flyby altitude biasing strategy, and the sequence of trajectory correction maneuvers executed in the weeks prior to the successful Earth gravity assist. 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, 2014 en_US
dc.title Maneuver design for the Juno mission: inner cruise en_US
dc.type Preprint en_US


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