A survey of Saturn orbiter transfer optionsThis paper is a description of recent work to categorize and enumerate the various options available for transfer from earth to Saturn orbit. The fundamental period of investigation is the 20-year synodic period of Jupiter and Saturn which permits a scenario of Jupiter gravity assist trajectories for various trip times. Against the background of the Jupiter swingby trajectories are compared a number of other options including Delta V-EGA and VEGA trajectories, direct earth-Saturn transfers, and solar and nuclear electric propulsion options. All are compared and contrasted in the context of expected launch vehicle capabilities and realistic transfer times.
Document ID
19800062363
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Uphoff, C. (California Institute of Technology, Jet Propulsion Laboratory, Mission Design Section, Pasadena Calif., United States)
Date Acquired
August 10, 2013
Publication Date
August 1, 1980
Subject Category
Astrodynamics
Report/Patent Number
AIAA PAPER 80-1700Report Number: AIAA PAPER 80-1700
Meeting Information
Meeting: Astrodynamics Conference
Location: Danvers, MA
Start Date: August 11, 1980
End Date: August 13, 1980
Sponsors: American Institute of Aeronautics and Astronautics and American Astronautical Society