• Proceedings of the Korean Information Science Society Conference
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• 2002.10c
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• pp.571-573
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• 2002

복잡한 네트워크상의 지능적이고 다양한 방식의 사이버 태러로부터 안전하고 효율적으로 네트워크를 총체적으로 관리하기 위해서는 개별 네트워크 노드간의 정보 교환은 필수적이다. STEALTH 프로토콜이란 거대망에서 네트워크 노드들 사이에 안전한 정보 교환을 위한 일종의 보안 프로토콜로 기존의 보안 프로토콜이 지닌 트래픽의 속도 저하 및 암호화로 인한 네트워크의 과부하를 최소화한 프로토콜이다. 여기서는 기존의 보안 프로토콜에 대해서 그 종류와 기능을 살펴본 후, 제안하는 STEALTH프로토콜의 요구사항 및 기능에 대해서 다룬다. 마지막으로 STEALTH 프로토콜이 적용된 시나리오를 통해 이 프로토콜의 역할과 기능을 상세히 설명한다.

• Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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• 2013.10a
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• pp.165-168
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• 2013

The USA has declared the cyber space as the 5th battlefield following land, sea, air, and space. In contrast to physical wars, in national cyberwarfare differentiation between friend and foe is impossible, and the boundaries between the lines of attack and defense are obscure. Therefore, to perform national cyberwarfare, credibility of all command delivery information performed in the cyber space should be confirmed. In this paper, the authors have determined the commands performed in national cyberwarfare, granted authorized IPv6 in space including the earth, moon and Mars for information credibility, and used LINK joints loaded with stealth functions to secure the credibility of command information.

• Journal of the Korean Vacuum Society
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• v.17 no.6
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• pp.501-510
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• 2008

The stealth technology to conceal an aircraft from the vision of a radar have been accomplished by coating the surface with special paints absorbing the electromagnetic wave. Nowadays, researches to utilize characteristics of the plasma-wave interaction for realizing the stealth technology are actively progressed. In this paper, to investigate the physical feasibility of the plasma stealth, calculation results for the required conditions of the plasma cloaking on the aircraft flying in the air for showing the stealth function, using a flat non-magnetized non-uniform plasma model, are reported and discussed.

• Aerospace Industry
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• s.94
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• pp.46-49
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• 2007

레이더가 만들어지고 나서 항공전에는 적에게 노출이 도지 않는 은폐 기술 즉, 스텔스 성능을 군관계자들은 요구해 왔다, 이번호에는 최근 개발된 항공기에 보편화되고 있는 기능인 스텔스 성능은 무엇인지 알아본다.

• Journal of the Korea Institute of Information and Communication Engineering
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• v.25 no.8
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• pp.1110-1116
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• 2021

In this paper, we propose a conformal Ku-band data link antenna to ensure low RCS of stealth UAV. As a phased array antenna with electrical beam steering function, a transmitter and a receiver were designed and manufactured for FDD communication, respectively. Each antenna is designed as a 12*12 planar array antenna and has a function to form a uni-directional pattern and a bi-directional pattern through phase control of unit elements. The beam steering range is designed to be able to steer up to 60 degrees in theta direction and 360 degrees in the phi direction. As a result of manufacturing and measurement, the conformal type radome has low transmission loss and meets the required specifications including system performance. The feasibility of mounting the stealth UAV has been confirmed, and future research directions such as interworking of baseband devices and conversion to digital beam steering function are suggested.

• Proceedings of the Korea Committee for Ocean Resources and Engineering Conference
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• 2002.05a
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• pp.225-230
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• 2002

현재 미 해군에서 개발 중인 DD21은, 미 해군의 해상 전투력 구조의 핵심인 이지스급 함정을 제외한 DD-963급 구축함과 FFG-7급 프리깃 함의 교체함으로서, 연안전에 대한 새로운 특수 임무에 적응할 수 있게 많은 학자들에 의해 연구되고 있는 차세대 구축함이다. 즉, DD21은 기존 이지스 함정에 부가하여 대지전(Land Attack)과 대기뢰전을 포함한 다목적의 기능을 발휘하면서 전투원의 스마트(Smart), 배치와 장비와 기구의 자동화와 기계화를 통한 함정과 함체의 스텔스(Stealth)화로 유지비와 초기 투자비를 최소화시킨 함정이다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.33 no.4
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• pp.1-6
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• 2005

The ability to predict radar return from flying vehicles becomes a critical technology issue in the development of stealth configurations. Toward developing a CEM code based on Maxwell's equations for analysis of RCS reduction schemes, an explicit upwind scheme suitable for multidisciplinary design is presented. The DFFT algorithm is utilized to convert the time-domain field values to the frequency-domain. A Green's function based on near field-to-far field transformation is also employed to calculate the bistatic RCS. To verify the numerical calculation the two-dimensional field around a perfectly conducting cylinder is considered. Finally results are obtained for the scattering electromagnetic field around an airfoil in order to illustrate the feasibility of applying CFD based methods to CEM.

• Journal of the Korean Society of Propulsion Engineers
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• v.9 no.4
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• pp.112-120
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• 2005

The solid propellants have been most widely used for the military rockets or missiles all over the world and the efforts have been focused on the enhancement of propellant performance up to 1980s. lately in company with the distinguished development in the intelligence and communication technology, the more accurate guidance as well as maneuverability has been required in the military weapon system. To meet the requirements such as a high maneuverability, insensitiveness, or stealth of missile, the researches have been doing to develop the solid propellants which have a quality of ultra-fast burning rate, insensitiveness, low signature or the like.

• Journal of the Korean Society of Systems Engineering
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• v.4 no.2
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• pp.45-54
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• 2008

This paper describes an operational concept of the network based future airborne force power using a systems engineering approach. The battlefield is changing to new system of systems that command and control by the network based BM/C4ISR. Also, it is composed of various sensors and shooters in an single theater. Future threats may be characterized as unmanned moving bodies that the strategic effect is great such as UAVs, cruise missile and tactical ballistic missiles. New threats such as low altitude stealth cruise missile may also appear. The implementation of future airborne force power network systems against these future threats is required to complex and integrated approach based on systems engineering. This work developed the operational concepts of the future airborne network system, and then derived the requirements for performing missions effectively. In addition, the scheme of future airborne force power network systems is presented.

• Journal of IKEEE
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• v.23 no.4
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• pp.1473-1476
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• 2019

Accurate material information is very important in PCB (Printed Circuit Board) design. In an integrated mast of a battleship, heat reduction is essential for stealth functionality. So heat dissipation from internal control equipments should be reduced as much as possible. Control equipments mostly consist of PCBs, but it often suffers from impedance mismatching due to imprecise Dk (Dielectric Constant), which significantly increases heat dissipation. In this paper, measurement methods of Dk is investigated. Also, effects on impedance mismatch by Dk variation with operating frequency is investigated.