Evaluation of Lightning Induced Effects in a Graphite Composite Fairing StructureDefining the electromagnetic environment inside a graphite composite fairing due to lightning is of interest to spacecraft developers. This paper is the first in a two part series and studies the shielding effectiveness of a graphite composite model fairing using derived equivalent properties. A frequency domain Method of Moments (MoM) model is developed and comparisons are made with shielding test results obtained using a vehicle-like composite fairing. The comparison results show that the analytical models can adequately predict the test results. Both measured and model data indicate that graphite composite fairings provide significant attenuation to magnetic fields as frequency increases. Diffusion effects are also discussed. Part 2 examines the time domain based effects through the development of a loop based induced field testing and a Transmission-Line-Matrix (TLM) model is developed in the time domain to study how the composite fairing affects lightning induced magnetic fields. Comparisons are made with shielding test results obtained using a vehicle-like composite fairing in the time domain. The comparison results show that the analytical models can adequately predict the test and industry results.
Document ID
20100042559
Acquisition Source
Kennedy Space Center
Document Type
Conference Paper
Authors
Trout, Dawn H. (NASA Kennedy Space Center Cocoa Beach, FL, United States)
Stanley, James E. (Florida Inst. of Tech. Melbourne, FL, United States)
Wahid, Parveen F. (University of Central Florida Orlando, FL, United States)