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Overview of the Cassini Extended Mission TrajectoryDue to the highly successful execution of the Cassini-Huygens prime mission and the estimated propellant remaining at the conclusion of the prime mission, NASA Headquarters allocated funding for the development of a 2-year long Cassini extended mission. The resultant extended mission, stemming from 1.5 years of development, includes an additional 26 targeted Titan flybys, 9 close flybys of icy satellites, and 60 orbits about Saturn. This paper describes, in detail, the different phases of the Cassini extended mission and the associated design methodology, which attempted to maximize the number and quality of high-priority scientific objectives while minimizing the total delta v expenditure and adhering to mission-imposed constraints.
Document ID
20150014793
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Buffington, Brent
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Strange, Nathan
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Smith, John
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 3, 2015
Publication Date
August 18, 2008
Subject Category
Administration And Management
Lunar And Planetary Science And Exploration
Astrodynamics
Meeting Information
Meeting: 2008 AIAA/AAS Astrodynamics Specialists Conference
Location: Honolulu, HI
Country: United States
Start Date: August 18, 2008
End Date: August 21, 2008
Sponsors: American Inst. of Aeronautics and Astronautics, American Astronautical Society
Distribution Limits
Public
Copyright
Other
Keywords
gravity assist
trajectory design
tour

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