Voyager electrostatic discharge protection programTests and analysis indicated the need to protect the Voyager spacecraft from electrostatic discharges in the Jupiter energetic charged particle environment. This paper describes the identified problem areas, the test and analysis methods and results, the resultant design changes, and the final assessment of the design changes and verification methods.
Document ID
19790041318
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Whittlesey, A. C. (California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: International Symposium on Electromagnetic Compatibility