• Title/Summary/Keyword: Ballistic

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A Study on the ballistic impact resistance and dynamic failure behavior of aramid FRMLs by high velocity impact (고속충격에 의한 아라미드 섬유강화 금속적층재의 방탄성능 및 동적파손거동에 관한 연구)

  • 손세원;이두성;김동훈;홍성희
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2000.11a
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    • pp.527-532
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    • 2000
  • The armor composite material targets such as aramid FRMLs with different type and ply number of face material and different type of back-up material, were studied to determine ballistic impact resistance and dynamic failure behavior during ballistic impact. Ballistic impact resistance is determined by $\textrm{V}_{50}$ ballistic limit, a statical velocity with 50% probability for complete penetration, test method. Also dynamic failure behaviors are respectfully observed that result from $\textrm{V}_{50}$ tests. $\textrm{V}_{50}$ tests with $0^{\circ}$ obliquity at room temperature were conducted with projectiles that were able to achieve near or complete penetration during high velocity impact tests. As a result, ballistic impact resistance of anodized Al 5052-H34 alloy(2 ply) is better than that of anodized Al 5052-H34 alloy(1 ply), but Titanium alloy showed the similar ballistic impact resistance. In the face material, ballistic impact resistance of titanium alloy is better than that of anodized Al 5052-H34 alloy. In the back-up material, ballistic impact resistance of T750 type aramid fiber is better than that of CT709 type aramid fiber.

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A Requirement Assessment Algorithm for Anti-Ballistic Missile Considering Ballistic Missile's Flight Characteristics (탄도미사일의 비행특성을 고려한 요격미사일 소요 알고리즘)

  • Kim, Heung-Seob;Kim, Ki-Tae;Jeon, Geon-Wook
    • 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.

Experimental and numerical research on ballistic performance of carbon steels and cold worked tool steels with and without Titanium Nitride (TiN) coating

  • Ergul, Erdi;Doruk, Emre;Pakdil, Murat
    • Steel and Composite Structures
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    • v.23 no.2
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    • pp.153-160
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    • 2017
  • It is extremely important to be aware of the ballistic performances of engineering materials in order to be able to choose the lightest armor providing full ballistic protection in civil and military applications. Therefore, ballistic tests are an important part of armor design process. In this study, ballistic performance of plates made of carbon steel and cold worked tool steel against 7.62 mm AP (armor-piercing) bullets was examined experimentally and numerically in accordance with NIJ standards. Samples in different sizes were prepared to demonstrate the effect of target thickness on ballistic performance. Some of these samples were coated with titanium nitride using physical vapor deposition (PVD) method. After examining all successful and unsuccessful samples at macro and micro levels, factors affecting ballistic performance were determined. Explicit non-linear analyses were made using Ls-Dyna software in order to confirm physical ballistic test results. It was observed that the ballistic features of steel plates used in simulations comply with actual physical test results.

Investigation on the Non-linear Injection Characteristics of GDI injector using 1D Simulation (1D 시뮬레이션 기반 GDI 인젝터의 비선형적 분사 특성 해석에 대한 연구)

  • Jinwoo Lee;Seoksu Moon;Donghan Hur;Jinsuk Kang
    • Journal of ILASS-Korea
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    • v.28 no.4
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    • pp.169-175
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    • 2023
  • Multi-injection scheme is being applied to GDI combustion to reduce PM and PN emission to meet the EU7 regulation. However, very short injection duration encounters the ballistic injection region, which injection quantity does not increase linearly with injection duration when applying multi-injection. In this study, numerical studies were conducted to reveal the cause of ballistic injection and the effect of design parameters on ballistic region using 1-D simulation, AMESim. Injection rate and injection quantity were compared with experiment to validate the established model, which showed the accuracy with 10% error. The model revealed that the tendency of ballistic region coincides with the needle motion behavior, which means that parameters at the upper part of needle such as electro-magnetic force, needle spring force and needle friction force have dominant effect on ballistic injection. To figure out the effect of electro-magnetic and needle friction force on ballistic, those parameters were varied to plus and minus 10% with model. The result showed that those parameters clearly changed the ballistic region characteristics, however, the impact became insignificant for outside of ballistic region, which means that the ballistic injection is mainly influenced by initial motion of injector needle.

A Study on the Flight Trajectory Prediction Method of Ballistic Missiles - BM type by Adjusting the Angle of a Flight Path and a Range - (탄도미사일의 비행궤적 예측 방법 연구 - 탄종별 비행경로각과 사거리를 중심으로 -)

  • Yoo, Byeong Chun;Kim, Ju Hyun;Kwon, Yong Soo;Choi, Bong Wan
    • Journal of the Korean Society of Systems Engineering
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    • v.16 no.2
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    • pp.131-140
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    • 2020
  • The characteristics of ballistic missiles are changing rapidly but studies have mostly focused on fragmentary flight trajectory analysis estimating the changing characteristics of some types, while there is a lack of research on comprehensive and efficient ballistic search, detection and prediction for missiles including the new types that have been gaining attention lately. This paper analyzes the flight trajectory characteristics of ballistic missiles at various ranges considering flight path angle adjustment, specific impulse and drag force with altitude based on the optimized equations of motion reflecting the parameters of North Korea's general and new types of ballistic missiles. The flight trajectory characteristics of representative ranges for each ballistic missile were analyzed by adjusting the flight path angle in the minimum energy method, lofted method, and depressed method. In addition, High value target can attacked by ballistic missiles considering flight path angle adjustment at various points. It's expected to be used to Threat Evaluation and Weapon Allocation, and deployment of defense systems by interpreting the analysis of the latest Iskander-class ballistic missiles and the new multiple rocket launcher.

Tile Size Dependency of Ballistic Performance in Alumina (알루미나의 시편크기가 방탄거동에 미치는 영향)

  • ;S.J. Bless
    • Journal of the Korean Ceramic Society
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    • v.32 no.3
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    • pp.366-370
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    • 1995
  • The ballistic efficiency of alumina tiles with various sizes, shapes, and target configurations was measured by the thick backing plate technique. The ballistic efficiency of square tiles roughly 8 mm thick struck by 12.7mm diameter bullets rapidly increased with tile size up to about 100mm, then tended to saturate. Circular shape tiles had lower ballistic efficiencies than those of square shape tiles for the same width and thickness. Small tiles (50mm) that were recessed in aluminum wells had a significantly higher ballistic efficiency than tiles placed on a flat surface. However, the difference in the ballistic efficiency between the two target configurtions became small at larger tile sizes. All the results could be explained by the effect of reflected waves at edges and the propagation of resulting cracks on the penetration process.

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An Effectiveness Analysis of Anti-Ballisitic Missile Launcher Arrangement for the Lower Tier Defense against the Ballistic Missile (탄도미사일 하층 방어 수행을 위한 발사대 배치 효과도 분석)

  • Kwon, Hyuck-Hoon;Lee, Bum-Seok;Kim, Yoon-Hwan;Choi, Kwan-Bum
    • Journal of the Korea Institute of Military Science and Technology
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    • v.16 no.5
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    • pp.590-597
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    • 2013
  • For a lower tier defense, the distance between a launcher and an engagement control station is quite important to estimate the proper defense area and to effectively arrange missile launchers. In this paper, we have analyzed an effectiveness of anti-ballistic missile launcher arrangement for the lower tier defense against the ballistic missile. The operation concept, specific configuration and aerodynamic characteristics of the ballistic missile such as SCUD-B/C, Nodong are considered in order to develop a realistic engagement simulation. The diverse engagement results through numerical simulations are provided to conduct the effectiveness analysis of anti-ballistic missiles.

Ballistic Missile Tracking using Unscented Kalman Filter (Unscented Kalman Filter를 이용한 탄도 미사일 추적)

  • Park, Sang-Hyuk;Yun, Joong-Sup;Ryoo, Chang-Kyung
    • Journal of Institute of Control, Robotics and Systems
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    • v.14 no.9
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    • pp.898-903
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    • 2008
  • In most cases, the trajectory of a ballistic missile is well explained by the Kepler's laws. It implies that the remaining trajectory of the ballistic missile including its final destination can be easily predicted if the position and velocity vector of the ballistic missile at any point on its path can be exactly known. Hence, an effective tracking algorithm based on an exact radar measurement model is very important for developing Ballistic Missile Defense(BMD) system. In this paper, we address to design a nonlinear filter, Unscented Kalman Filter(UKF), to track the ballistic missile.

Development of Augmentation Method of Ballistic Missile Trajectory using Variational Autoencoder (변이형 오토인코더를 이용한 탄도미사일 궤적 증강기법 개발)

  • Dong Kyu Lee;Dong Wg Hong
    • Journal of the Korean Society of Systems Engineering
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    • v.19 no.2
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    • pp.145-156
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    • 2023
  • Trajectory of ballistic missile is defined by inherent flight dynamics, which decided range and maneuvering characteristics. It is crucial to predict range and maneuvering characteristics of ballistic missile in KAMD (Korea Air and Missile Defense) to minimize damage due to ballistic missile attacks, Nowadays, needs for applying AI(Artificial Intelligence) technologies are increasing due to rapid developments of DNN(Deep Neural Networks) technologies. To apply these DNN technologies amount of data are required for superviesed learning, but trajectory data of ballistic missiles is limited because of security issues. Trajectory data could be considered as multivariate time series including many variables. And augmentation in time series data is a developing area of research. In this paper, we tried to augment trajectory data of ballistic missiles using recently developed methods. We used TimeVAE(Time Variational AutoEncoder) method and TimeGAN(Time Generative Adversarial Networks) to synthesize missile trajectory data. We also compare the results of two methods and analyse for future works.