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Cassini - A mission to the Saturnian systemThis international (NASA/ESA) mission, planned for a Titan IV/Centaur G-prime launch in the 1995-1997 era, consists of a Saturn Orbiter (a U.S. Mariner Mark II spacecraft) and a Titan Atmospheric Entry Probe (an ESA product). The mission profile is highly sophisticated in its astrodynamic aspects - a deep space Delta-V maneuver, followed by earth and Jupiter gravity assist flybys, with asteroid encounter(s) along the way. Saturn arrival is characterized by further multiple maneuvers resulting in the Titan probe delivery and a close orbiter flyby, to be followed by a 4-year Saturn system tour. Details of the trajectory design process are discussed.
Document ID
19890025269
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sergeyevsky, Andrey B.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Kerridge, Stuart J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Stetson, Douglas S.
(California Institute of Technology Jet Propulsion Laboratory, Pasadena, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Subject Category
Astronautics (General)
Report/Patent Number
AAS PAPER 87-423
Report Number: AAS PAPER 87-423
Meeting Information
Meeting: AAS/AIAA Astrodynamics Conference
Location: Kalispell, MT
Country: United States
Start Date: December 6, 1987
End Date: December 9, 1987
Sponsors: AAS, AIAA
Accession Number
89A12640
Distribution Limits
Public
Copyright
Other

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