• Defense and Technology
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• no.2 s.252
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• pp.18-29
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• 2000

한국의 TMD 참여문제는 실효성 문제, 경제적인 문제, 기술적인 문제 등으로 볼 때 유보하는 것이 바람직하다고 생각된다. 따라서 북한의 탄도 미사일에 대한 방어체계 구축은 동맹국의 TMD 체계와 상호 운용성을 보장할 수 있으며, 주변국으로부터 군비 확충에 대한 의심을 불식시킴과 동시에 한국적 여건에 가장 적합한 미사일방어체계(KAMD:Korea Air and Missile Defense)에 대한 개념연구의 선행이 필요하다.

• Defense and Technology
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• no.10 s.92
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• pp.18-28
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• 1986

제 3세계에서는 현재 선진제국으로부터 무기수입이나 과학.기술협력 등에 의해 우주로케트.미사일계획을 추진하고 있다. 대립하는 나라들이 탄두미사일을 가짐으로 해서 거꾸로 재외미군에 대한 종심공격의 위협도 증대되어 있다. 이 글은 미의회도서관의 조사국요원이 이러한 제3세계으로의 탄도미사일 확산의 현황에 관해 분석한 보고의 전문을 번역한 것이다.

• The Korean Journal of Air & Space Law and Policy
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• v.11
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• pp.371-380
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• 1999

• Journal of the Korea Society for Simulation
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• v.30 no.1
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• pp.31-42
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• 2021

In order to respond to the ballistic missile threat of North Korea, the ROK military is constructing a multi-layered defense that can minimize the vulnerability of single-layered defense. Accordingly, it is necessary to study an operation plan which can maximize the intercept rate of a multi-layered defense system. And to study the operation plan of the Korean missile defense system, it must be considered that the operational environment of the Korean military and the effects of the strategic strike system. Therefore, this study proposes a simulation model that reflects the characteristics of the Korean missile defense system and analyzes four interceptor missile operation plans. The simulation result indicates that a high intercept rate can be achieved in various situations by comprehensively considering the ballistic missile threat estimate, interceptor missile reserve, and the strategic strike system effect.

• Proceedings of the Korea Information Processing Society Conference
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• 2014.11a
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• pp.634-635
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• 2014

가상 환경 기반의 시험 수요가 군사 무기체계 분야에서 지속적으로 증가하고 있다. 가상 환경 기반 기술의 증가 이유는 시험 및 평가에서 낮은 비용과 높은 효율을 달성할 수 있기 때문이다. 본 논문에서는 교전환경을 Modeling & Simulation기법으로 가상환경을 만들어 비용을 최소화하고 공간적 제약도 해결할 수 있다. 계측데이터 모의 소프트웨어는 플러그인 아키텍처에 기반을 두어 실 탄도탄 정보를 모의해 탄도탄 요격미사일 시험에 적합한 환경을 구성하도록 설계되었다. 각 기능을 컴포넌트 별로 분리하여 개발해 특정 모델을 Third party 형태로 개발할 때 유용한 구조임을 설명한다.

• Journal of the Korea Institute of Military Science and Technology
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• v.18 no.2
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• pp.173-180
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• 2015

North Korea has developed ballistic missiles over the past 30 years. It is believed that they have a variety of ballistic missiles more than 1,000. Because these ballistic missiles threaten South Korea directly, accurate analysis of them is essential. Flight trajectories of the ballistic missiles are generally changed by means of adjusting payload weight, Isp, flight path angle, and cut-off time. The flight path angle is widely used to control the missile range. However it is difficult to predict the missile trajectory exactly in real operational environment because the missile could be launched according to its intention and purpose. This work analyzed the 1,000 km range MRBM's trajectory characteristics from adjusting flight path angle which is depressed as well as lofted method. The analysis of missile trajectory characteristics is based on the simulation of the missile trajectory model developed by KNDU research team.

• Journal of the Korea Institute of Military Science and Technology
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• v.21 no.4
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• pp.551-561
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• 2018

Footprint is defined as ground area that is projected from the outer edges of the battle space protected by a defence system. This concept can be effectively used for making decisions on site selection of anti missile systems to defend against enemy's ballistic missiles. In this paper, simulations of ballistic missile trajectories based on various launch conditions are performed first and then the footprint is derived with engagement zone set as a boundary condition. Results of the simulation with various relative positions between the defense system and defended asset are also presented. The proposed method, in which the trajectories are generated based on launch point of the ballistic missile, has an advantage of approximating the defended area close to reality. Two applications are introduced in the present paper to describe how the derivation of defended area could be utilized in deployment decision of defense systems.

• Journal of the Korea Institute of Military Science and Technology
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• v.14 no.6
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• pp.1009-1017
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• 2011

A Ballistic Missile(BM) is a missile that follows a sub-orbital ballistic flightpath with the objective of delivering one or more wardheads to a predetermined target and An Anti-Ballistic Missile(ABM) is a missile designed to destroy a ballistic missile before reaching its target. The main objective of this study is to assess the requirement of ABM by considering both flight characteristic of the SCUD-B/C, Nodong missiles and intercept performance of ABM in the Lower tier Ballistic Missile Defense(BMD). The Ballistic Missile's flight characteristics, such as trajectory, velocity etc., are estimated by simulation using the physical motion equations. The requirement of ABM is calculated by evaluating whether the BMD forces can defend those when the ballistic missiles attack prime facilities.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.43 no.3
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• pp.272-281
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• 2015

Miniature smart-bullet is a human-carrying guided missile designed to hit a target easily while having a miniature size. Contrary to the normal missiles, miniature smart-bullet is highly expected to enhance the military strength and survival rate of troops by its compact size readily carriable to a single soldier. In this paper, previously developed techniques, activities and patents of miniature smart-bullet, particularly its structural shape and actuators are surveyed. Furthermore, analysis of required techniques to develop a miniature smart-bullet are also discussed for upcoming conceptual design.

• Defense and Technology
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• no.9 s.103
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• pp.36-43
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• 1987