• Title/Summary/Keyword: Impact Fuze

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Measurement of the Impact Fuze Phenomena using the Underwater Explosion (수중폭발을 이용한 충격신관 작동 계측)

  • Choi, SiHong
    • Journal of the Korea Institute of Military Science and Technology
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    • v.17 no.4
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    • pp.479-484
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    • 2014
  • In this paper, This study shows the content on the impact fuze test and the measurement using underwater explosion phenomena. The impact fuze has both a delay function and a super quick. Up to now, nothing but the naked eye of the observer has been used to verify performance of the impact fuze. The observer has determined the performance by the shape of the plume created from the explosion phenomenon. However, it is extremely difficult to use that method at a long range. In order to solve the problem, the measurement using the underwater explosion phenomena was tried.

M&S and Experimental Comparison of Crush Switch Assembly for Operation Validation (크러시스위치 조립체의 작동신뢰성 확인을 위한 M&S와 시험 결과 비교)

  • Kim, Minkyum;Jung, Myung-suk;Uhm, Won-Young;Jang, Junyong
    • Journal of the Korea Institute of Military Science and Technology
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    • v.23 no.3
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    • pp.229-236
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    • 2020
  • A crush switch assembly(CSA) connected to an impact fuze provides electrical signal for detonation of the loaded main charge when an impact with the target is detected. Because the CSA experiences continuous changes in flight environment such as changes in velocity, vibration, and stresses, it is necessary to accurately predict the behavior of the fuze to maintain functionality during flight and to detonate when necessary. In this paper, random vibration analysis for flight environment and impact analysis on target hit are performed using FEA. Then, high speed impact tests are performed with the original and scaled down models to ensure operation validation of the manufactured products. The test results are then compared with M&S results to verify the capability of currently modeled CSA.

A Study on the Impact Sensing Device for Improving the Firing Function Reliability of ESAF (ESAF의 기폭 신뢰성 향상을 위한 충격감지장치 연구)

  • Jo, Seyoung
    • Journal of the Korea Institute of Military Science and Technology
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    • v.18 no.5
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    • pp.525-531
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    • 2015
  • In this paper, a novel impact sensing device for an ESAF(Electronic Safe and Arming Fuze) is presented. An impact sensing device is mounted in front of a weapon, and it detects an impact when it crashes against a target. There are two main design requirements to enhance the firing functional reliability of the ESAF; an operational reliability and a reduced latency, which is a delay time needed for sensing the impact. The design method of the contact-type impact sensing device, which employs an FPCB(Flexible Printed Circuit Board) so it can be used other weapons, is proposed. The tests demonstrated that the design described in this work show a reduced delay time with ensuring the operational reliability.

A Study of Failure Mechanism for Inclined Impact of PELE (PELE의 경사진 충격에 따른 파괴 메커니즘에 대한 연구)

  • Jo, Jong-Hyun;Lee, Young-Shin
    • Journal of the Korea Institute of Military Science and Technology
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    • v.15 no.5
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    • pp.712-719
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    • 2012
  • Penetrator with enhanced lateral effect(PELE) is a newconcept projectile, without dynamite and fuze. It consists of high-density jacket, closed at its rear end and filled with a low-density filling material. To study the explosion characteristics of PELE, by AUTODYN-3D code, the calculation models of projectile body and bullet target are established and the process of penetrating aluminum-2024 alloy target of PELE is simulated, and the scattering characteristics after penetrating aluminum-2024 alloy target of PELE are studied by different initial velocity. The explicit finite element analysis of PELE fragmentation was implemented with stochastic failure criterion in AUTODYN-3D code. As expansion of filling, the fragments were obtained velocities and dispersed laterally and further more enhancing the damage area largely. The number and shape of the PELE fragments were different depend on impact velocity and incidence angle of filling which fragment generated during penetration and lateral dispersion process.

Numerical Investigation for Multi-layer Shock Absorber to Improve Survivability of Fuze at High Impact (고충격에 신관의 생존성을 향상시키기 위한 다층 충격완충장치 전산해석 연구)

  • Soh, Kyoung Jae;Kim, Minkyum;Lee, Daehee
    • Journal of the Computational Structural Engineering Institute of Korea
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    • v.33 no.4
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    • pp.255-261
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    • 2020
  • This study proposes a method of constructing an effective shock absorber. The existing shock absorber is fabricated only with polyethylene; however, the new shock absorber comprises polyethylene on the outside and a high-density material on the inside. The shock was mostly reduced when the density difference between the inner and outer materials was large. Aluminum, titanium, and copper were chosen as the outer structure of two-layer. Shock reduction was most effective in copper with the highest density, and the maximum deceleration was reduced by 43% while the impulse was reduced by 51% in the proposed shock absorber than the traditional shock absorber. In the cases of four-layer and six-layer shock absorbers, the impulse was reduced, but the maximum deceleration was increased. The fuze must survive from the biggest shock and the remaining shock waves should not exceed the threshold. Thus, a two-layer structure shock absorber using polyethylene-copper was proposed.