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Evaluation of Lightning Induced Effects in a Graphite Composite Fairing StructureDefining the electromagnetic environment inside a graphite composite fairing due to near-by lightning strikes is of interest to spacecraft developers. This effort develops a transmission-line-matrix (TLM) model with a CST Microstripes to examine induced voltages. on interior wire loops in a composite fairing due to a simulated near-by lightning strike. A physical vehicle-like composite fairing test fixture is constructed to anchor a TLM model in the time domain and a FEKO method of moments model in the frequency domain. Results show that a typical graphite composite fairing provides adequate shielding resulting in a significant reduction in induced voltages on high impedance circuits despite minimal attenuation of peak magnetic fields propagating through space in near-by lightning strike conditions.
Document ID
20110014829
Acquisition Source
Kennedy Space Center
Document Type
Preprint (Draft being sent to journal)
Authors
Trout, Dawn H.
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Stanley, James E.
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Wahid, Parveen F.
(University of Central Florida Orlando, FL, United States)
Date Acquired
August 25, 2013
Publication Date
January 1, 2011
Subject Category
Composite Materials
Report/Patent Number
KSC-2011-050R
KSC-2011-252
KSC-2011-050RR
Report Number: KSC-2011-050R
Report Number: KSC-2011-252
Report Number: KSC-2011-050RR
Meeting Information
Meeting: Applied Computational Electromagnetics Society
Location: Williamsburg, VA
Country: United States
Start Date: March 27, 2011
End Date: March 31, 2011
Distribution Limits
Public
Copyright
Public Use Permitted.
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