• Title/Summary/Keyword: ballistic analysis

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An Experimental Study on the Ballistic Accuracy by Air Guide Grooves (공기안내홈이 탄도 정확도에 미치는 실험적 연구)

  • Kim, Junkyu;Kim, Hyungse;Lee, Moonhwan
    • Journal of the Korea Institute of Military Science and Technology
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    • v.19 no.2
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    • pp.195-201
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    • 2016
  • An experimental study has been found the air guide grooves for reducing drag. When a bullet is fired and move in the air, the drag is generated. The vortex which is one of the types of drag hinders the movement of the bullet. To solve this phenomenon, cut a negative grooves that we are called the air guiding grooves at the back of bullet. The grooves bullet has identified that the drag compared to conventional ammunition(KM80 and K193) is reduced to 4.480 and 4.054 : 10 % through a Finite Analysis Program($Ansys^{TM}$). Even pressure center was retreating 0.72 % compared to a Bullet(KM80 and K193). Effect obtained with these results is the accuracy of the grooves bullet in a shooting test was improved by over 32 %(KM80: 2.86, air guide grooves : 1.94) compared to conventional ammunition(KM80 and K193). In addition, muzzle velocity is increased 73 m/s. This is expected to be extended the velocity and effective range of bullet. Also, the velocity of the grooves bullet is increased when moving in the air while the velocity of the bullet(KM80 and K193) is reduced. The gas ejected from the muzzle to be balanced and stable flight of the Bullet. Given these effects, we can reckon the air guide grooves have positive influence.

Dynamic Modeling and Characteristics Analysis of Solid Rocket Motor with Multi Axis Pintle Nozzles (다축 핀틀 노즐을 장착한 고체 추진기관의 동적 모델링 및 특성 분석)

  • Ki, Taeseok;Hong, Seokhyun;Park, Ik-soo
    • Journal of the Korean Society of Propulsion Engineers
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    • v.19 no.3
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    • pp.20-28
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    • 2015
  • Performance parameters of solid rocket motor with multi axis pintle nozzles were analyzed theoretically and modeled. For figuring out the governed variable of dynamic characteristics of system, dynamic analysis was done by using established model. To present characteristics of this system, the model should include not only internal ballistics of propulsion unit but also actuating system to move pintle. For solid rocket motor with multi axis pintle nozzles, not only performance of steady state but also dynamic characteristic of transient state is important design parameter to precise thrust control. Therefore, response time of open-loop system was analyzed by using established model and requirement about response time was satisfied by controlling pressure.

A Network Analysis of Ballistic Helmet Technology Keyword (방탄헬멧 기술분야 키워드에 대한 네트워크 분석)

  • Kang, Jinwoo;Park, Jaewoo;Kim, Jihoon
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.18 no.4
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    • pp.311-316
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    • 2017
  • The network analysis method has emerged as a new methodology for various disciplines, due to its ability to provide a representative knowledge network of references, co-authors and keywords. Bulletproof technology is an interdisciplinary field involving various disciplines, such as material mechanics, structural mechanics, and ballistics, so it is essential to keep up with the recent trends in technological research. In this research, the recent R&D trends in the field of bulletproof materials were analyzed using keyword based network analysis. From the results, the core keywords were identified as 'Composite', 'Model' and 'Head' using the scholar search engine, google scholar. The centrality analysis for the core keywords showed that bulletproof technology has developed in 3 different areas, viz. material, structure and effects. To the best of our knowledge, this is the first application of (network analysis?) to bulletproof technology. Moreover, we are also convinced that the results of this study will be useful for defense technology planning and determining the direction of R&D in the field of bulletproof technology.

China's Satellite Research and Development to Collect Electronic Signals for Marine Reconnaissance to Surrounding Nations (중국의 주변국 해양감시를 위한 전자신호 수집위성 연구개발)

  • Lee, Yongsik;Aom, Sangho;Lim, Jaesung
    • Journal of Satellite, Information and Communications
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    • v.12 no.3
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    • pp.54-62
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    • 2017
  • China has invested for military satellite technology development to construct the space-based surveillance system from existing land-based and aerostat surveillance system since 1960s to react rapidly for deployment of marine force of United States and surrounding nations in west Pacific, south China sea and Indian ocean. China has also launched about 40 the Yaogan military intelligence satellites series for EO, SAR and ELINT fields since 2006 after the required technique with several technical experiment satellites launch and operational test. ELINT satellites transmit data from satellite to earth station in real time with construction space-based network around it. Those data are simultaneously delivered to Anti-Ship Ballistic Missile(ASBM) connected land-based C4ISR network for marine target attack. Therefore China has enhanced surveillance and attack capability to the surrounding marine nations with space-based network around it. In the future, It is considered that China will increase accurate location search, signal processing and analysis ability through a further study on its technology.

Design, manufacturing and performance test of restorated airplane of Buhwal (부활호 복원 설계, 제작 및 성능 연구)

  • Park, Chanwoo;Kim, Byungsoo;Cho, Taehwan;Cho, Hwankee;Ok, Ju Seon
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.41 no.7
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    • pp.552-560
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    • 2013
  • Airplane Buhwal is the first light airplane which is designed and made in South Korea. Restoration of airplane Buhwal is designed based on the one made by Korean Airforce in 2004 but there are some changes also. It uses aluminum main wing, electronic indicator, BRS(Ballistic recovery parachute) and black box for improved performance. In this paper, for the restorated Buhwal, major design changes are introduced, structure, aerodynamic and stability analysis are reviewed and improved performances which is proven through flight test are shown. This study will be a big help for domestic light airplane development.

North Korean Submarine-Launched Ballistic Missile (SLBM) and Reaction of Republic of Korea Navy (북한 SLBM 평가와 한국 해군의 대응방안)

  • Yoon, Sukjoon
    • Strategy21
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    • s.39
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    • pp.47-81
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    • 2016
  • This paper has attempted to examine the political and operational contexts within which North Korea's latest acts of nuclear blackmail, its test-firing of an SLBM on April 23rd 2016 and its fourth nuclear test on January 6th 2016, should be understood. Analysis of the KN-11 SLBM and the Sinpo-class SSB is based on official South Korean, US and others sources, especially the ROK MND, as well as other resources from South Korea, US and others. Unfortunately, the results of this exploration are inconclusive: there is simply not enough evidence available at present to either confirm or refute the existence of a functional North Korean SLBM and SSB. Nevertheless, the North Korean determination to possess such assets should not be taken lightly. But even accepting North Korea's claims about its SLBMs at face value, which is undermined by news of apparently unsuccessful follow-up test-firings in November, and probably December 2015, there is little proof that North Korea has yet succeeded in miniaturizing its nuclear warhead, so the most extravagant fears are not yet justified. Taken together with North Korea's latest announcement of a supposed successful SLBM ejection-test, on March 23th 2016, the KN-11 SLBM claims should probably be seen as primarily about proving North Korea's status as a nuclear power, both to exert external political pressure and to bolster internal political support for Kim Jong-un's rule. In conclusion, this paper recommends formulating a preemptive anti-access strategy for the ROKN, proposes acquiring an ASW CV and SSNs to implement submarine strategic deterrent patrols, and urges extending the existing limited AORs to facilitate the preemptive anti-access strategy. Other deterrence options may be suggested, but it is surely significant that the ROKN has recently publically referred to the deployment of an ASW CV and SSNs for the first time.

Analysis of Unsteady Combustion Performance in Solid Rocket Motor with Pintle (핀틀을 장착한 고체추진기관의 비정상 연소 성능 분석)

  • Ki, Taeseok;Ha, Dongsung;Jin, Jungkun;Lee, Hosung;Yoon, Hyungull
    • Journal of the Korean Society of Propulsion Engineers
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    • v.19 no.1
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    • pp.68-75
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    • 2015
  • In this paper, unsteady characteristics of pressure in solid rocket motor were analyzed by using response of pintle actuation, pressure and thrust data from ground test. Pressure and thrust in solid rocket motor can be controlled in real time by varying nozzle throat area with pintle, installed in the valve. Unsteady characteristics of pressure can be observed in this system occurred by various reasons. Two critical reasons, error of pintle actuation and ablation of center tube, are found and effects of each reason can be analyzed individually by re-prediction of pressure with response of pintle actuation and analyzing thrust to pressure ratio.

Energy Absorption Characteristics of Z-shape Fabric under High Velocity Impact (Z형 직물의 고속 충격 에너지 흡수 특성)

  • Choi, Chunghyeon;Park, Yurim;Kim, YunHo;Noh, Jae-young;Kim, Chun-Gon
    • Composites Research
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    • v.28 no.4
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    • pp.176-181
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    • 2015
  • In this study, the Z-shape fabric design is proposed as the way to enhance the ballistic performance of fabrics which are used as the intermediate layer of stuffed Whipple shield configurations. The Z-shape fabric employs a different boundary condition from those of conventional configurations of fabrics which include 4 edge fixed. Impact analysis on Z-shape aramid yarns and fabrics using LS-DYNA software was performed and the results were compared with 2 edge fixed and 4 edge fixed fabrics to identify the high velocity impact energy absorption characteristics of the Z-shape fabric. It was revealed that the Z-shape showed different impact behavior and higher energy absorption performance than 2 and 4 edge fixed fabrics.

Computational Analysis of Heracron Fabric at High-velocity Impact (Heracron 직물의 고속 충돌 해석)

  • Kim, YunHo;Choi, Chunghyeon;Kumar, Sarath Kumar Sathish;Cha, JiHun;Kim, Chun-Gon
    • Composites Research
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    • v.32 no.2
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    • pp.120-126
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    • 2019
  • Advanced fiber fabrics have been utilized in not only anti-stabbing and bullet-proofing for body armor but also various industrial fields including vehicular armor and spacecraft structure. Furthermore, there have been a number of research to improve the ballistic performance of advanced fabrics introducing many computational approaches. In our research, an advanced fabric, Heracron manufactured in South Korea was modelled firstly using Autodyn, a commercial software specializing in impact and explosion phenomenon. The sensitivity of the input parameters was also confirmed by conducting simulations. To verify the numerical modelling, we measured and compared the simulation results with velocity decrements after impact involving one, three, and five layers of Heracron under 200-500 m/s impacts by an aluminum spherical projectile. The Heracron fabric was successfully modelled using Autodyn.

Analysis of Human Casualties on the Ground in Urban Area due to UAM Crash (UAM 추락 시 인구 밀접 지역 지상 인명피해 분석)

  • Kim, Youn-sil;Choi, In-ho
    • Journal of Advanced Navigation Technology
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    • v.26 no.5
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    • pp.281-288
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    • 2022
  • This study quantitatively analyzed the human casualties that can occur when a multicopter-type Urban Air Mobility (UAM) with a weight of about 1 ton and a speed of about 100 km/h falls in an urban area. Based on the population density and building database in Seoul, the population exposed to collisions in the event of a UAM crash was derived. Through the ballistic descent model, the accident impact radius of the UAM fall was calculated. In addition, the change in human casualties on the ground was analyzed when the accident impact radius increased. Finally, the ground risk map was created for Seoul, and it was confirmed that about 1 to 10 people could be injured when a UAM crash.