• 항공우주시스템공학회지
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• 제4권3호
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• pp.24-28
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• 2010

The purpose of this study is to define available microwave absorbing structure for aircraft from in the X-band(8.2~12.4GHz) frequencies. The electromagnetic wave absorption or shielding techniques is an important issue not only for military purpose but also for commercial purposes. Aircraft Radar Absorbing Structure(RAS) is absorbed or scattered propagation waves from the enemy radar. There are absorbing technologies at shaping design techniques and using Radar Absorbing Materials(RAM). RAM is more important because shaping design can't include perfect radar absorbing performance. In this study, based on material properties was introduced RAM and to analyze the each characteristics. Finally, we comparison appropriate RAM for aircraft.

• 한국정보통신학회:학술대회논문집
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• 한국해양정보통신학회 2009년도 춘계학술대회
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• pp.555-558
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• 2009

본 논문은 상대방으로부터 탐지를 최소화시키는 스텔스 기술을 분석하고, 대부분의 레이더 반사 단면적 감소는 형상화로부터 기인되며, 특별한 부위에는 RAM을 이용하여 최소화 시키는 것을 확인하였다. 따라서 RF 스텔스를 위한 밀리미터파 대역의 레이더 반사 단면적을 최소화시키는 측면에서 94 GHz에서 전파흡수량 17 dB로 98 %를 흡수하는 RAM을 설계 및 제작하였다. 결과적으로 개발된 RAM을 플랫폼에 적용시 상대방으로부터 레이더 탐지거리를 62 % 축소시키는 효과를 얻을 수 있다.

• 한국정보통신학회논문지
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• 제21권11호
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• pp.2206-2212
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• 2017

현대 해상전에서 함정의 피탐지율은 생존성에 직접적인 요소이며, 레이다 반사면적(RCS; Radar Cross Section)은 피탐지율에 있어서 주요 변수 중 하나이다. 본 논문에서는 RCS 감소기법 중 하나인 레이다 신호를 흡수하는 특수 재질을 통한 RCS 감소 기법인 RAM(Radar Absorbing Materials) 방법을 이용하여 위협 주파수 대역의 RCS 해석을 수행하였다. 해석 모델은 모형선 모델을 이용하였고, RAM 기법에 적용될 전파흡수체는 최신 전파흡수체 기술인 광대역 메타물질을 적용하였다. 광대역 메타물질은 광대역에서 공진주파수를 갖는 MIK 공진구조와 유연성 기판을 이용하여 모델링을 수행하였고, 광대역 메타물질의 성능 분석을 위하여 전자기파의 흡수율과 반사율에 대한 모의실험을 수행하였다. 또한, 광대역 메타물질 적용에 따른 레이다 반사면적 감소효과를 분석하기 위하여 기존 전파흡수체와의 비교를 통하여 RCS 감소 효과를 분석하였다.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2002년도 춘계학술발표대회 논문집
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• pp.105-108
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• 2002

Materials, matrices mixed with various kinds of conductive or magnetic powder, such as ferrite, have been used as the electromagnetic wave absorbing ones, so called RAM(radar absorbing material). The structure that does not only have electromagnetic waves absorbing property like RAM but also supports loads is called RAS(radar absorbing structure). One of the existing manufacturing process of RAS is to compound with conductive powders the glass fiber-reinforced composite with good permeability and the ability to support loads. The process, however, causes a number of problems, such as the degradation in the mechanical properties of the composite, especially, interlamina shear strength. In this study, mechanical properties of glass fabric/epoxy composite containing 7wt% carbon black powders were measured and compared with pure glass fabric/epoxy composites.

• 전자공학회논문지A
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• 제32A권1호
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• pp.70-78
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• 1995

In order to implement broadband RAM's(Radar Absorbing Materials) made up of multiple dielectricl layers, the design variables such as the dielectrci constaints, the depths and the loss tangents of dielectric are optimized. The wave impedances regarding the reflective wave are found in dielectrics, input impedances and reflection coefficients with multiple dielectric layers are derived from the transmission line circuit theory. Finally, minimum average reflective power and optimum design variables are obtained by applying the numerical technique, called modified Powell method. In case of four dielectric layers with inequality constraints in design variables, a quite favourable and feasible result with the total depth of 1.1 cm, the average reflective power of 0.85% over the bradband frequency range is obtained for a specific example.

• 전자공학회논문지D
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• 제34D권3호
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• pp.17-24
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• 1997

Broad-band RAM's (Radar absorbing materials) are designed by multi-layered lossy dielectrics. The depth, the relative permittivity and the loss tangent of each layer are optimized in order to meet the required reflective power over the specified frequency range using a genetic algorithm. The reflection coefficients are calculated by the continued fraction method. A new population model of the partial initialization method during iterations is applied for the multi-modal functions to enhance the performance of the genetic algorithm. The optimal RAN's are designed by setting the relative permittivity and the loss tangent of the dielectrics as a funtion of the frequency over 5~20GHz.

• 한국군사과학기술학회지
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• 제1권1호
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• pp.114-127
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• 1998

A user friendly computer code(EMCOMST; Electro-Magnetic response for COMposite STructures) was developed which provides with computations of the response characteristics such as reflectance and transmittance to the incident wave angles, frequencies, composite thicknesses, ply orientations, and types of backplate as the linearly polarized transverse electro-magnetic wave is emitted to the advanced composite structures. In this investigation were reviewed the electromagnetic characteristics of the continuous orthotropic fiber-reinforced organic matrix composites with or without ferrite fillers, which are actively applied to low-weight and high-strength aircraft structures. Also were calculated the response of the three layered compound structures which have appropriately stacked above-mentioned materials as transmitting layer, absorbing layer, reflection layer, respectively under the specific thickness constraints for mechanical strength design requirements. For the composite structures presented in this study, minimum reflectance value less than -5㏈ can be obtained in the frequency range of 4 to 12 ㎓. In addition, analysis of structures attached isotropic radar absorbing materials(RAM) is facilitated by putting the material properties in the material input card entries adequately.