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Launch period development for the Juno mission to Jupiter

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dc.contributor.author Kowalkowski, Theresa D.
dc.contributor.author Johannesen, Jennie R.
dc.contributor.author Lam, Try
dc.date.accessioned 2015-07-14T18:02:16Z
dc.date.available 2015-07-14T18:02:16Z
dc.date.issued 2008-08-18
dc.identifier.citation AIAA/AAS Astrodynamics Specialist Conference, Honolulu, Hawaii, August 18-21, 2008 en_US
dc.identifier.clearanceno 08-2728
dc.identifier.uri http://hdl.handle.net/2014/45416
dc.description.abstract The Juno mission to Jupiter is targeted to launch in 2011 and would reach the giant planet about five years later. The interplanetary trajectory is planned to include two large deep space maneuvers and an Earth gravity assist a little more than two years after launch. In this paper, we describe the development of a 21-day launch period for Juno with the objective of keeping overall launch energy and delta-V low while meeting constraints imposed on Earth departure, the deep space maneuvers’ timing and geometry, and Jupiter arrival. 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, 2008 en_US
dc.subject mission design en_US
dc.title Launch period development for the Juno mission to Jupiter en_US
dc.type Preprint en_US


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