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Radiation design considerations for advanced Jupiter spacecraftThis paper considers one aspect of the complex radiation design considerations for planetary spacecraft, namely the approach used for solving the effects of radiation on materials problems. An overview of the approach developed at JPL for Voyager, and currently being used on Galileo, is treated briefly. Examples of the postulated Jovian charged particle levels are given. The types of computer analyses codes used, the mass shielding techniques that evolved and the recommended shielding techniques for future planetary spacecraft are treated.
Document ID
19800035612
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Bouquet, F. L.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Koprowski, E. F.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Date Acquired
August 10, 2013
Publication Date
December 1, 1979
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
80A19782
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Other

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