Analysis of Multi-Layer Composite Cavity Using FEKO

Authors

  • James E. Stanley Department of Electrical and Computer Engineering Florida Institute of Technology, Melbourne, FL 32901. USA
  • Susan K. Earles Department of Electrical and Computer Engineering Florida Institute of Technology, Melbourne, FL 32901. USA
  • Ivica N. Kostanic Department of Electrical and Computer Engineering Florida Institute of Technology, Melbourne, FL 32901. USA
  • Dawn H. Trout School of Electrical Engineering and Computer Science University of Central Florida, Orlando, FL 32816-2450, USA
  • Parveen F. Wahid School of Electrical Engineering and Computer Science University of Central Florida, Orlando, FL 32816-2450, USA

Keywords:

Analysis of Multi-Layer Composite Cavity Using FEKO

Abstract

Modeling of a large cavity containing multiple layers inside the structure has been studied using equivalent impedance approximations along with simplified single ray tracing analysis. This modeling effort investigates the effects of radiating with a source enclosed in a large vacant composite structure relative to a short wavelength. The development of the model involves the completion of a two step process. First, the heritage geometric reduction and approximation is investigated. This particular investigation involves an approach that is an application of Poynting’s Theorem. This work was performed by Hallett and Reddell at Goddard Space Flight Center in 1998. For this comparison, the Multi-Level Fast Multipole Method (MLFMM) available in the commercial tool FEKO, is used to model a generic multi-layer payload fairing (hollow cone connected to a hollow cylinder) with a radiating source to determine the resonant cavity effects within the fairing as another approximation baseline. The intent is to provide predictions for the electric field levels if a transmitter in the fairing either deliberately or unintentionally is activated. The results show a comparison with the heritage calculation and FEKO software tool. However, FEKO shows the electric field distributions within the composite fairing cavity instead of a single average value.

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References

Department of Defense (U.S.),

“Electromagnetic Emission and

Susceptibility Requirements for the Control

of Electro-magnetic Interference,” MIL-

STD-461C, 17 Feb 1996.

Department of Defense (U.S.),

“Electromagnetic Compatibility for Space

Systems,” MIL-STD-1541A, 30 Dec 1987.

C. R. Paul, Electromagnetics for Engineers

With Applications, John Wiley & Sons, New

York, NY, 2004.

M. Hallett and J. Reddell, "Technique for

Predicting the RF Field Strength Inside an

Enclosure," Technical Report NASA/TP-

-206864, NASA Aeronautics and Space

Database, Goddard Space Flight Center,

Greenbelt Maryland, 1998.

D.K. Cheng, Field and Wave

Electromagnetics, Second Edition, Addison

Wesley, Reading, MA, 1989.

V. Demir and A. Elsherbeni, "A Graphical

User Interface for Calculation of the

Reflection and Transmission Coefficients of

a Layered Medium," IEEE Antennas and

Propagation Magazine, Vol. 48, No. 1,

February 2006.

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Published

2022-06-17

How to Cite

[1]
J. E. . Stanley, S. K. . Earles, I. N. . Kostanic, D. H. . Trout, and P. F. . Wahid, “Analysis of Multi-Layer Composite Cavity Using FEKO”, ACES Journal, vol. 25, no. 1, pp. 69–74, Jun. 2022.

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General Submission