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Galileo internal electrostatic discharge programThe Galileo spacecraft which will orbit Jupiter in 1988 will encounter a very harsh environment of energetic electrons. These electrons will have sufficient energy to penetrate the spacecraft shielding, consequently depositing charges in the dielectric insulating materials or ungrounded conductors. The resulting electric field could exceed the breakdown strength of the insulating materials, producing discharges. The transients produced from these Internal Electrostatic Discharges (IESD) could, depending on their relative location, be coupled to nearby cables and circuits. These transients could change the state of logic circuits or degrade or even damage spacecraft components, consequently disrupting the operation of subsystems and systems of the Galileo spacecraft during its expected mission life. An extensive testing program was initiated for the purpose of understanding the potential threats associated with these IESD events. Data obtained from these tests were used to define design guidelines.
Document ID
19850014193
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Leung, P. L.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Plamp, G. H.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Robinson, P. A., Jr.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 12, 2013
Publication Date
March 1, 1985
Publication Information
Publication: NASA. Lewis Research Center Spacecraft Environ. Interactions Technol., 1983
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
85N22504
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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