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Galilean satellite mission conceptsPost-Galileo mission concepts considered possible for satellite-intensive investigations are presented, with consideration given to single and multiple target scenarios using orbiter and lander deployments. Candidate missions that satisfy the selected science objectives are identified, and specific scenario/target combinations which fall within performance constraints are chosen. The concepts are then developed into descriptive mission profiles. Also discussed are target encounter and deployment requirements, payload delivery, and operational considerations. Particular attention is given to Jupiter radiation effects and shielding requirements. A wide range of satellite-intensive missions is thought to be within the performance capabilities of earth-gravity-assisted ballistic trajectories and nuclear electric propulsion technology.
Document ID
19820056478
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Soldner, J. K.
(Science Applications, Inc. Schaumburg, IL, United States)
Stancati, M. L.
(Science Applications, Inc. Schaumburg, IL, United States)
Feingold, H.
(Science Applications, Inc. Schaumburg, IL, United States)
Date Acquired
August 10, 2013
Publication Date
August 1, 1982
Subject Category
Astronautics (General)
Report/Patent Number
AIAA PAPER 82-1460
Meeting Information
Meeting: Astrodynamics Conference
Location: San Diego, CA
Start Date: August 9, 1982
End Date: August 11, 1982
Sponsors: American Institute of Aeronautics and Astronautics and American Astronautical Society
Accession Number
82A40013
Funding Number(s)
CONTRACT_GRANT: NASW-3035
Distribution Limits
Public
Copyright
Other

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