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.
Maneuver Design for the Juno Mission: Inner Cruise
AIAA Space 2014 ; 2014 ; San Diego, CA, United States
05.08.2014
Aufsatz (Konferenz)
Keine Angabe
Englisch
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