Cockpit Protection Analysis against High Power Microwave

Author

Huang, Jun ; Hu, Yun-an ; Zhang, Hao-ran ; Jin, Yan

Author_Institution

Grad. Students´´ Brigade, Naval Aeronaut. Eng. Inst., Yantai, China

fYear

2010

fDate

10-12 Dec. 2010

Firstpage

1

Lastpage

4

Abstract

A model of high power microwave (HPM) with multiple parameters is brought forward, a calculation method of electromagnetic transmission rate and reflectivity is proposed, a finite-difference time-domain (FDTD) film algorithm is set forth, a shielded cockpit glass construction is designed by a new flow, and protective effect analysis on military aircraft´s cockpit against HPM is carried out on a 3D plane, airborne equipments and pilot model with a scale of 1:1. The simulation tests show the soft kill protective efficiency in the range of carrier frequencies and protective limits of the glass construction with incident angles.

Keywords

aircraft communication; electromagnetic wave transmission; protection; calculation method; carrier frequencies; cockpit glass construction; cockpit protection analysis; electromagnetic transmission rate; finite difference time domain film algorithm; high power microwave; multiple parameters; protective effect analysis; reflectivity; Atmospheric modeling; Attenuation; Finite difference methods; Glass; Reflectivity; Time domain analysis;

fLanguage

English

Publisher

ieee

Conference_Titel

Computational Intelligence and Software Engineering (CiSE), 2010 International Conference on

Conference_Location

Wuhan

Print_ISBN

978-1-4244-5391-7

Electronic_ISBN

978-1-4244-5392-4

Type

conf

DOI

10.1109/CISE.2010.5676773

Filename

5676773