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)