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Internal Charging(1) High energy (>100keV) electrons penetrate spacecraft walls and accumulate in dielectrics or isolated conductors; (2) Threat environment is energetic electrons with sufficient flux to charge circuit boards, cable insulation, and ungrounded metal faster than charge can dissipate; (3) Accumulating charge density generates electric fields in excess of material breakdown strenght resulting in electrostatic discharge; and (4) System impact is material damage, discharge currents inside of spacecraft Faraday cage on or near critical circuitry, and RF noise.
Document ID
20140010122
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Minow, Joseph I.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
July 24, 2014
Publication Date
March 31, 2014
Subject Category
Electronics And Electrical Engineering
Report/Patent Number
M14-3494
Report Number: M14-3494
Meeting Information
Meeting: CCMC Community Workshop (Coomunity Coordinated Modeling Center)
Location: Annapolis, MD
Country: United States
Start Date: March 31, 2014
End Date: April 4, 2014
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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