• Title/Summary/Keyword: Ballistic

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Technological Review on the Development of Metallic Armor Materials (금속 장갑재료의 개발기술 및 발전전망)

  • Kim, Hong-Kyu;Hong, Sung-Suk;Shim, In-Ok
    • Composites Research
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    • v.24 no.2
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    • pp.46-50
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    • 2011
  • This paper describes the state of the art for the development of metallic armor materials which are mainly used as armor plates of the combat vehicles. Several important micro-structural features affecting ballistic properties of the metallic armor are discussed. Optimization of the strength and toughness balance of the metallic armor is necessary for the improvement of the ballistic performance resulting from maximizing the resistance to the penetration of the bullet and also to brittle failure of the plates. Understanding and control of the adiabatic shearing phenomenon developed remarkably during high strain rate deformation is needed to prevent brittle failure of the metallic armor materials.

Efficient Measurement System to Investigate Micro-Doppler Signature of Ballistic Missile

  • Choi, In-O;Kim, Kyung-Tae;Jung, Joo-Ho;Kim, Si-Ho;Park, Sang-Hong
    • International Journal of Aeronautical and Space Sciences
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    • v.17 no.4
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    • pp.614-621
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    • 2016
  • Micro-Doppler (MD) shift caused by the micro-motion of a ballistic missile (BM) can be very useful to identify it. In this paper, the MD signatures of three scale-model BMs are investigated using a portable measurement system. The measurement system consists of an X-band 2-by-2 phase comparison mono-pulse radar, and a mechanical device that can impart controlled spinning and coning motions simultaneously to a model to yield the MD signature that replicates the characteristic of each target and the corresponding micro-motion. The coning motion determined the overall period of MD, and the spinning motion increased its amplitude. MD was also dependent on aspect angle. The designed system is portable, and can implement many micro-motions; it will contribute to analysis of MD in various situations.

Penetration Mechanisms of Ceramic Composite Armor Made of Alumina/GFRP

  • Jung, Woo-Kyun;Lee, Hee-Sub;Jung, Jae-Won;Ahn, Sung-Hoon;Lee, Woo-Il;Kim, Hee-Jae;Kwon, Jeong-Won
    • International Journal of Precision Engineering and Manufacturing
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    • v.8 no.4
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    • pp.38-44
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    • 2007
  • Combat vehicles are frequently maneuvered in battlefields when the lives of combatants are being threatened. These vehicles are important elements that influence the consequences of a battle. Their armor must be lightweight and provide excellent protection to ensure successful operations. Ceramic composite armor has recently been developed by many countries to fulfill these requirements. We reviewed previous research to determine an effective armor design, and then fabricated a composite armor structure using $Al_2O_3$ and glass fiber-reinforced polymer. Specimens were manufactured under controlled conditions using different backing plate thicknesses and bonding methods for the ceramic layer and the backing plate. The penetration of an armor-piercing bullet was evaluated from ballistic protection tests. The bonding method between the ceramic layer and the fiber-reinforced polymer influenced the ballistic protection performance. A bonding layer using rubber provided the best protection.

Ballistic Performance Variation Prediction of Continuously Variable Thrust Solid Rocket Motor by the Linear Approximation (선형 근사화에 의한 가변추진시스템 내탄도 성능 변화 예측)

  • Kim, Joung-Keun;Park, Jong-Ho
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.36 no.1
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    • pp.79-85
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    • 2008
  • Generally Solid Rocket Motor(SRM) has advantages like this - safety, simplicity and flexibility in design and manufacturing process. However, once propellant grain shape and nozzle throat area are determined, modification of thrust magnitude is nearly impossible. Recently, methods for controlling the thrust magnitude of SRM are vigorously developed. This paper predicts internal ballistic performance variation, especially thrust of SRM by means of Linear Approximation according as chamber pressure or nozzle throat area is changed. The results predicted by the proposed method are good agreement with the those of exclusive Ballistic Performance Prediction Program(SPP).

Effect of Ignition Delay Time Gap on the Linked Pyrotechnic Thrusters (파이로추력기의 점화시간차 영향)

  • Kim, Ki-Un;Jeon, In-Soo;Ahn, Sung-Woo
    • Journal of the Korea Institute of Military Science and Technology
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    • v.14 no.1
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    • pp.154-159
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    • 2011
  • The effect of the ignition delay time gap is newly studied. The operational characteristics of the linked two pyrotechnic thrusters are affected by the time gap. Although two thrusters are simultaneously ignited, the time at which the pressure starts to rise in each thruster may not be synchronized. The characteristic of the system with the time gap is compared with that of the fully synchronized system without any time gap. Depending upon the magnitude of the time gap, the pressure-time profile and the ballistic performance are different. When two pyrotechnic thrusters have a time gap, the peak pressure of one thruster(in which the pressure is built up earlier) is increased and the other is decreased. As the time gap is increased, the peak pressure is converged into the maximum pressure. This maximum pressure can be obtained when only one thruster is activated. Because the maximum pressure is bounded, it is predicted that there isn't any catastrophic failures in the considered system. When the time gap is relatively small, the impulse of the combined force acting on the moving body is almost maintained. But the ballistic performance of the system with a large time gap should be carefully estimated because the reduction of the ballistic performance should not be easily neglected.

A Study on the Optimal Allocation of Korea Air and Missile Defense System using a Genetic Algorithm (유전자 알고리즘을 이용한 한국형 미사일 방어체계 최적 배치에 관한 연구)

  • Yunn, Seunghwan;Kim, Suhwan
    • Journal of the Korea Institute of Military Science and Technology
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    • v.18 no.6
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    • pp.797-807
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    • 2015
  • The low-altitude PAC-2 Patriot missile system is the backbone of ROK air defense for intercepting enemy aircraft. Currently there is no missile interceptor which can defend against the relatively high velocity ballistic missile from North Korea which may carry nuclear, biological or chemical warheads. For ballistic missile defense, Korea's air defense systems are being evaluated. In attempting to intercept ballistic missiles at high altitude the most effective means is through a multi-layered missile defense system. The missile defense problem has been studied considering a single interception system or any additional capability. In this study, we seek to establish a mathematical model that's available for multi-layered missile defense and minimize total interception fail probability and proposes a solution based on genetic algorithms. We perform computational tests to evaluate the relative speed and solution of our GA algorithm in comparison with the commercial optimization tool GAMS.

Analysis of Internal Ballistic Characteristics of Solid Rocket with Erosive Burning (침식연소에 따른 고체 로켓 내탄도 특성 변화 분석)

  • Cho, Mingyoung;Kim, Jinyong;Park, Sunghan
    • Journal of the Korean Society of Propulsion Engineers
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    • v.18 no.3
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    • pp.56-61
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    • 2014
  • Two erosive burning models were applied to compare analysis results of ballistic for the internal ballistics of solid rocket motors. By comparing motor tests with results of analysis, the variance of a grain shape was analyzed and coefficients of erosive burning were drawn. Results of comparison presents that the coefficient of erosive burning was proportional to the change of burning area, while inversely proportional to the change of cross area.

Ballistic impact analyses of triangular corrugated plates filled with foam core

  • Panigrahi, S.K.;Das, Kallola
    • Advances in Computational Design
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    • v.1 no.2
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    • pp.139-154
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    • 2016
  • The usage of sandwich structure is extensively increasing in lightweight protective structures due to its low density and other useful properties. Sandwich panels made of metal sheets with unfilled cellular cores are found to exhibit lower deflections by comparing to an equivalent monolithic plate of same metal and similar mass per unit density. However, the process of localized impact on solid structures involving plastic deformation, high strain rates, temperature effect, material erosion, etc. does not hold effectively as that of monolithic plate. In present work, the applications of the sandwich plate with corrugated core have been extended to develop optimized lightweight armour using foam as medium of its core by explicit finite element analysis (FEA). The mechanisms of hardened steel projectile penetration of aluminum corrugated sandwich panels filled with foams have been numerically investigated by finite element analysis (FEA). A comparative study is done for the triangular corrugated sandwich plate filled with polymeric foam and metallic foam with different densities in order to achieve the optimum penetration resistance to ballistic impact. Corrugated sandwich plates filled with metallic foams are found to be superior when compared to the polymeric one. The optimized results are then compared with that of equivalent solid and unfilled cores structure to observe the effectiveness of foam-filled corrugated sandwich plate which provides an effective resistance to ballistic response. The novel structure can be the alternative to solid aluminum plate in the applications of light weight protection system.

A Study on Intercept Probability and Cost based Multi-layer Defense Interceptor Operating Method using Mathematical Model (수리모형을 이용한 요격확률 및 비용 기반의 다층 방어 요격미사일 운용방법 연구)

  • Seo, Minsu;Ma, Jungmok
    • Journal of the Korea Society for Simulation
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    • v.29 no.2
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    • pp.49-61
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    • 2020
  • It is important to operate a limited number of interceptors effectively to counter ballistic missile threats. The existing interceptor operating method determines the number of interceptors according to the level of TBM (Theater Ballistic Missile) engagement effectiveness applied to a defended asset. It can cause either excessive interceptor waste compared to the intercept probability or the intercept probability decrease. Thus, interceptor operating method must be decided considering the number of ballistic missiles, intercept probability and cost. This study proposes a mathematical model to improve the existing interceptor operating method. In addition, the efficiency indicator is proposed for trade-off between intercept probability and cost. As a result of the simulations, the mathematical model-based interceptor operating method can achieve better results than the existing interceptor operating method.

A Change of U.S. Ballistic Missile Defense Strategy (미국 탄도미사일방어 전략의 변화)

  • Park, Tae-Yong
    • Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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    • 2017.05a
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    • pp.371-372
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    • 2017
  • The United States has built a missile defense system from the Cold War era, but since the end of the Cold War era, there have been many changes in international situation and threats. The forces of power divided between the United States and the Soviet Union have become increasingly threatened by China's willingness to expand its external influence, declaration of strong Russia and North Korea and Iran's nuclear armament and advanced ballistic missile technology. In response to this threat change, the Missile Defense Agency(MDA) has established strategies and policies, but its parent law has not been revised. United States changed to the FY2017 National Defense Authorization Act (FY2017 NDAA) including changed missile defense strategy. In this paper, I check US ballistic missile defense strategies included in the FY2017 NDAA and compare what changes have been made in existing strategies.

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