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Space plasma charging - Lessons from VoyagerThe Voyager spacecraft to Jupiter and beyond was designed with the intent that it would be immune to the deleterious effects of space plasma charging. Such effects include electrostatic fields disrupting science data, external electrostatic discharge (ESD) events, and also internal ESDs. This paper describes the design features incorporated into the Voyager spacecraft, the rationale for those features, the results in the Jovian environment, and present thinking about appropriate design to avoid ESD problems caused by space charging.
Document ID
19870035384
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Whittlesey, A.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Leung, P.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena CA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 87-0474
Report Number: AIAA PAPER 87-0474
Accession Number
87A22658
Distribution Limits
Public
Copyright
Other

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