Computation and analysis of satellite opportunities for the Mariner Jupiter/Saturn 1977 missionThe MJS77 mission provides the United States with the first opportunity to study the large satellites of Jupiter and Saturn at close range. Techniques are presented which allow the mission analyst to generate single and multiple satellite encounters at Jupiter and Saturn, and to incorporate satellite gravity assist into the targeting problem. These methods are applied to the MJS77 mission to generate, parametrically, the single and multiple satellite opportunities and characteristics at both flyby planets. An interesting consequence of this study is that a close encounter with a Galilean satellite increases the flexibility of a trajectory design which would otherwise require sizable post-Jupiter trajectory correction maneuvers to achieve the desired Saturn arrival date timing. In addition the Saturn studies revealed that as many as four satellites can be encountered on a single trajectory.
Document ID
19740034850
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Beerer, J. G.
Penzo, P. A.
Wallace, R. A. (California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Date Acquired
August 7, 2013
Publication Date
July 1, 1973
Subject Category
Space Sciences
Report/Patent Number
AAS PAPER 73-230Report Number: AAS PAPER 73-230
Meeting Information
Meeting: Astrodynamics Conference
Location: Vail, CO
Country: US
Start Date: July 16, 1973
End Date: July 18, 1973
Sponsors: American Astronautical Society, American Institute of Aeronautics and Astronautics