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Internal Electrostatic Discharge Monitor - IESDMA document discusses an innovation designed to effectively monitor dielectric charging in spacecraft components to measure the potential for discharge in order to prevent damage from internal electrostatic discharge (IESD). High-energy electrons penetrate the structural materials and shielding of a spacecraft and then stop inside dielectrics and keep accumulating. Those deposited charges generate an electric field. If the electric field becomes higher than the breakdown threshold (approx. =2 x 10(exp 5) V/cm), discharge occurs. This monitor measures potentials as a function of dielectric depth. Differentiation of potential with respect to the depth yields electric field. Direct measurement of the depth profile of the potential in a dielectric makes real-time electronic field evaluation possible without simulations. The IESDM has been designed to emulate a multi-layer circuit board, to insert very thin metallic layers between the dielectric layers. The conductors serve as diagnostic monitoring locations to measure the deposited electron-charge and the charge dynamics. Measurement of the time-dependent potential of the metal layers provides information on the amount of charge deposited in the dielectrics and the movement of that charge with time (dynamics).
Document ID
20110011958
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other - NASA Tech Brief
Authors
Kim, Wousik
(California Inst. of Tech. Pasadena, CA, United States)
Goebel, Dan M.
(California Inst. of Tech. Pasadena, CA, United States)
Jun, Insoo
(California Inst. of Tech. Pasadena, CA, United States)
Garrett, Henry B.
(California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 25, 2013
Publication Date
April 1, 2011
Publication Information
Publication: NASA Tech Briefs, April 2011
Subject Category
Technology Utilization And Surface Transportation
Report/Patent Number
NPO-47347
Distribution Limits
Public
Copyright
Public Use Permitted.
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