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The Jupiter Icy Moons Orbiter reference trajectoryThe proposed NASA Jupiter Icy Moons Orbiter (JIMO) mission would have used a single spacecraft to orbit Callisto, Ganymede, and Europa in succession. The enormous Delta-Velocity required for this mission (nearly [25 km/s]) would necessitate the use of very high efficiency electric propulsion. The trajectory created for the proposed baseline JIMO mission may be the most complex trajectory ever designed. This paper describes the current reference trajectory in detail and describes the processes that were used to construct it.
Document ID
20060043641
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Whiffen, Gregory J.
Lam, Try
Date Acquired
August 23, 2013
Publication Date
January 22, 2006
Subject Category
Lunar And Planetary Science And Exploration
Meeting Information
Meeting: 2006 AAS/AIAA SpaceFlight Mechanics Meeting
Location: Tampa, FL
Country: United States
Start Date: January 22, 2006
End Date: January 26, 2006
Distribution Limits
Public
Copyright
Other
Keywords
optimization
Ganymede
Europa
Jupiter
Prometheus
Callisto
low-thrust

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