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Reconstruction of the Voyager Saturn Encounter orbits in the ICRF system

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dc.contributor.author Jacobson, R. A. en_US
dc.date.accessioned 2004-09-16T21:13:38Z
dc.date.available 2004-09-16T21:13:38Z
dc.date.issued 2003-02-09 en_US
dc.identifier.citation 13th AAS/AIAA Space Flight Mechanics Meeting en_US
dc.identifier.citation Ponce, Puerto Rico en_US
dc.identifier.clearanceno 03-0282 en_US
dc.identifier.uri http://hdl.handle.net/2014/6435
dc.description.abstract We obtain Voyager trajectories in the International Celestial Reference Frame, and we revise the gravity field taking advantage of improvements made in modelling and data processing since the previous work. We also incorporate a full dynamical model for the Saturnian satellites into the analysis for the first time. en_US
dc.format.extent 3612031 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other Voyager Saturn en_US
dc.title Reconstruction of the Voyager Saturn Encounter orbits in the ICRF system en_US


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