Theory and Application of Shaped Charges
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Final Report for SERDP WP-2209 Replacement Melt-Castable Formulations for Composition B
LA-UR-17-24143 Approved for public release; distribution is unlimited. Title: Final report for SERDP WP-2209 Replacement melt-castable formulations for Composition B Author(s): Leonard, Philip Francois, Elizabeth Green Intended for: Report Issued: 2017-05-19 Disclaimer: Los Alamos National Laboratory, an affirmative action/equal opportunity employer, is operated by the Los Alamos National Security, LLC for the National Nuclear Security Administration of the U.S. Department of Energy under contract DE-AC52-06NA25396. By approving this article, the publisher recognizes that the U.S. Government retains nonexclusive, royalty-free license to publish or reproduce the published form of this contribution, or to allow others to do so, for U.S. Government purposes. Los Alamos National Laboratory requests that the publisher identify this article as work performed under the auspices of the U.S. Department of Energy. Los Alamos National Laboratory strongly supports academic freedom and a researcher's right to publish; as an institution, however, the Laboratory does not endorse the viewpoint of a publication or guarantee its technical correctness. Final report for SERDP WP-2209 Replacement melt-castable formulations for Composition B Elizabeth Francois; Philip Leonard, M-7 Los Alamos National Laboratory With technical contributions from Philip Samuels, ARDEC Contents List of Tables .................................................................................................................. ii List of Figures ................................................................................................................ -
Explosives and Terminal Ballistics
AND TERMINAL BALLISTICS A REPORT PREPARED FOR THE AAF SCIEN'rIFIC ADVISORY GROUP By D. P. MAC DOUGALL Naval Ordnance Laboratory, Washington, D. C. N. M. NEWMARK Department oj Civil Engineering, University oj Illinois • PMblished May, 1946 by HEADQUARTERS AIR MATERIEL COMMAND PUBLICATIONS BRANCH, INTEJtJYiE~9) '1001 WRIGHT FIELD, DAYTON, OHIO V-46579 The AAF Scientific Advisory Group was activated late in 1944 by General of the Army H. H. Arnold. He se cured the services of Dr. Theodore von Karman, re nowned scientist and consultant in aeronautics, who agreed to organize and direct the group. Dr. von Karman gathered about him a group of Ameri can scientists from every field of research having a bearing on air power. These men then analyzed im portant developments in the basic sciences, both here and abroad, and attempted to evaluate the effects of their application to air power. This volume is one of a group of reports made to the Army Air Forces by the Scientific Advisory Group. Thil document contolnl Information affecting the notional defenle of the United Statel within the meaning of the Espionage Ad, SO U. S. C., 31 and 32, 01 amended. Its tronsmiulon or the revelation of Its contents In any manner to on unauthorized person II prohibited by low. AAF SCIENTIFIC ADVISORY GROUP Dr. Th. von Karman Director Colonel F. E. Glantzberg Dr. H. L. Dryden Deputy Director, Military Deputy Director, Scientific Lt Col G. T. McHugh, Executive Capt C. H. Jackson, Jr., Secretary CONSULTANTS Dr. C. W. Bray Dr. A. J. Stosick Dr. L. A. -
Comparison of Dynamic Tensile Extrusion Behaviour of Wcu Composites Made by Different Processes
EPJ Web of Conferences 183, 03004 (2018) https://doi.org/10.1051/epjconf/201818303004 DYMAT 2018 Comparison of dynamic tensile extrusion behaviour of WCu composites made by different processes Leeju Park1,2,*,Sanghyun Woo1,2, Yerim Lee1 , Keunho Lee1 , and Young Sun Yi 1 1The 4th Research and Development Institute, Agency for Defence Development, 34186 Daejeon, Republic of Korea 2Weapon Systems Engineering, Korea University of Science and Technology, 34113 Daejeon, Republic of Korea Abstract. Composites with 60~90% of tungsten are used in liners of some specialty shaped charges. The penetration is enhanced by a factor against copper for homogeneous steel target. Tungsten powder based shaped charge liners are also especially suitable for oil well completion. In this study, WCu composites manufactured by different process are used for testing of dynamic tensile extrusion (DTE) behaviour. One samples were made by copper infiltrated method. The other samples were manufactured by metal injection molding methods with reduced tungsten copper composite powder. DTE tests were carried out by launching the sphere samples (Dia. 7.62mm) to the conical extrusion die at a speed of ~375m/s. The DTE fragmentation behaviour of tungsten copper composites after soft-recovered were examined and compared with each other. 1 Introduction to each other through DTE test. Tungsten–copper (WCu) is a mixture of tungsten and copper. As tungsten and copper are not mutually soluble, 2 Experimental the material is composed of distinct particles of copper There are many methods making tungsten copper dispersed in a matrix of tungsten. So, we are called a tungsten copper composite instead of a tungsten copper composite. -
MAGTF Antiarmor Operations
MCWP 3-15.5 (CD) MAGTF Antiarmor Operations Chapter 3 MAGTF Antiarmor Weapons and Techniques The MAGTF possesses a vast array of weapons systems with anti armor capabilities. While later chapters will address the proper integration of these weapons systems in a combined arms role, it is imperative that the reader understand the capabilities and limitations of each weapon system against a tank or other types of armored vehicles. Since improvement of weapon capabilities and armor is ongoing and information is often classified, the reader should consult the unit S-2 for timely updates on this subject matter. Section I. Antiarmor Weapons Systems 3101. Weapons Systems The M1A1 main battle tank is powered by a gas turbine engine rated at 1,500 hp, with a 23.8 hp/ton ratio. This MBT has a maximum speed of 42 mi/h and a cruising range of 275 miles. The MlA1 has a laser range finder, optical day sight, and a thermal imaging night sight. With the fording kit, it is capable of moving in water at turret roof depth. The M1A1 fires only Sabot (kinetic energy round) and the high explosive antitank (HEAT) (high explosive [HE] shaped charge), and the Mult-purpose Anti-Tank (MPAT) which is an air/ground fused version of the HEAT round. Crew 4 Weight 67.59 tons Armament 120mm smoothbore tank gun MER for HEAT, APFSDS, and MPAT range 4000m .50 cal M2 MG tank commanders Maximum effective range 1830 m 7.62 mm Coax MG and 7.62 mm Coax MG Maximum effective range 900 m Basic Load 44 rounds main gun Figure 3-1. -
Shaped Charges Having a Porous Tungsten Liner-An Experimental and Theoretical Study of Metal Compression, Jet Formation and Penetration Mechanics
New Jersey Institute of Technology Digital Commons @ NJIT Dissertations Electronic Theses and Dissertations Fall 1-31-1997 Shaped charges having a porous tungsten liner-an experimental and theoretical study of metal compression, jet formation and penetration mechanics Brian Edward Fuchs New Jersey Institute of Technology Follow this and additional works at: https://digitalcommons.njit.edu/dissertations Part of the Mechanical Engineering Commons Recommended Citation Fuchs, Brian Edward, "Shaped charges having a porous tungsten liner-an experimental and theoretical study of metal compression, jet formation and penetration mechanics" (1997). Dissertations. 1055. https://digitalcommons.njit.edu/dissertations/1055 This Dissertation is brought to you for free and open access by the Electronic Theses and Dissertations at Digital Commons @ NJIT. It has been accepted for inclusion in Dissertations by an authorized administrator of Digital Commons @ NJIT. For more information, please contact [email protected]. Copyright Warning & Restrictions The copyright law of the United States (Title 17, United States Code) governs the making of photocopies or other reproductions of copyrighted material. Under certain conditions specified in the law, libraries and archives are authorized to furnish a photocopy or other reproduction. One of these specified conditions is that the photocopy or reproduction is not to be “used for any purpose other than private study, scholarship, or research.” If a, user makes a request for, or later uses, a photocopy or reproduction for purposes in excess of “fair use” that user may be liable for copyright infringement, This institution reserves the right to refuse to accept a copying order if, in its judgment, fulfillment of the order would involve violation of copyright law. -
Chapter 2 EXPLOSIVES
Chapter 2 EXPLOSIVES This chapter classifies commercial blasting compounds according to their explosive class and type. Initiating devices are listed and described as well. Military explosives are treated separately. The ingredi- ents and more significant properties of each explosive are tabulated and briefly discussed. Data are sum- marized from various handbooks, textbooks, and manufacturers’ technical data sheets. THEORY OF EXPLOSIVES In general, an explosive has four basic characteristics: (1) It is a chemical compound or mixture ignited by heat, shock, impact, friction, or a combination of these conditions; (2) Upon ignition, it decom- poses rapidly in a detonation; (3) There is a rapid release of heat and large quantities of high-pressure gases that expand rapidly with sufficient force to overcome confining forces; and (4) The energy released by the detonation of explosives produces four basic effects; (a) rock fragmentation; (b) rock displacement; (c) ground vibration; and (d) air blast. A general theory of explosives is that the detonation of the explosives charge causes a high-velocity shock wave and a tremendous release of gas. The shock wave cracks and crushes the rock near the explosives and creates thousands of cracks in the rock. These cracks are then filled with the expanding gases. The gases continue to fill and expand the cracks until the gas pressure is too weak to expand the cracks any further, or are vented from the rock. The ingredients in explosives manufactured are classified as: Explosive bases. An explosive base is a solid or a liquid which, upon application or heat or shock, breaks down very rapidly into gaseous products, with an accompanying release of heat energy. -
Improvement of Penetration Performance of Linear Shaped Charges
Projectile Impacts: modelling techniques and target performance assessment 87 Improvement of penetration performance of linear shaped charges H. Miyoshi1, H. Ohba2, H. Kitamura2, T. Inoue2 & T. Hiroe3 1Project Division, Chugoku Kayaku Co., Ltd., Japan 2Yoshii Plant, Chugoku Kayaku Co., Ltd., Japan 3Department of Mechanical Engineering and Materials Science, Kumamoto University, Japan Abstract Experiments with and simulations of linear shaped charges (LSCs) have been conducted to improve the penetration performance and minimize collateral damage by fragments. Annealed tough pitch copper was selected for an appropriate liner material. The penetration depth increased by 50%, compared to current LSCs. The detonation effects of the explosive change the liner into jet and slug. However, the case is also transformed into fragments, which creates undesirable collateral damage. Polyvinyl chloride was adopted as the case material to reduce damage by fragments. No fragments were generated when the newly-designed LSCs were shot. For the simulation of the jet formation and target penetration, the AUTODYN planar Euler solver was selected, and the liner, case and explosive were filled on the Euler solver plane. The calculation results provided significant information about determining the optimal stand-off distance and allow the design of effective cutting plans for use with LSCs. Keywords: linear shaped charges, target penetration, stand-off distance, Euler solver. 1 Introduction Liner shaped charges (LSCs) have the ability of instantaneous cutting of structures and have been used in the separation of the first and second stages, and the command destruction of solid rocket boosters (SRB) in the H-2A rocket. In the military field, LSCs are used for the separation of the capsule in the anti- WIT Transactions on State of the Art in Science and Engineering, Vol 75, © 2014 WIT Press www.witpress.com, ISSN 1755-8336 (on-line) doi:10.2495/978-1-84564-879-4/009 88 Projectile Impacts: modelling techniques and target performance assessment submarine rockets. -
Damage Mechanism of PTFE/Al Reactive Charge Liner Structural Parameters on a Steel Target
materials Article Damage Mechanism of PTFE/Al Reactive Charge Liner Structural Parameters on a Steel Target Xuepeng Zhang 1,*, Zhijun Wang 1, Jianping Yin 1, Jianya Yi 1 and Haifu Wang 2,* 1 School of Mechatronic Engineering, North University of China, Taiyuan 030051, China; [email protected] (Z.W.); [email protected] (J.Y.); [email protected] (J.Y.) 2 State Key Laboratory of Explosion Science and Technology, Beijing Institute of Technology, Beijing 100081, China * Correspondence: [email protected] (X.Z.); [email protected] (H.W.); Tel.: +86-010-68918584 (H.W.) Abstract: The incorporation of reactive material damage element technology in ammunition war- heads is a research hotspot in the development of conventional ammunition. The research results are of great significance and military application value to promote the development of high-efficiency damage ammunition technology. In this paper, we aimed to understand the behavior of the reactive jet and its damage effect on a steel target by undertaking theoretical analysis, numerical simulation, and experimental research. We studied the influence of structural and material parameters on the shape of the reactive jet based on autodyn-2d finite element simulation software, and the formation behavior of the reactive jet was verified using a pulsed X-ray experiment. By studying the combined damage caused by the steel target penetrating and exploding the reactive jet, the influence of the structural and performance parameters, and the explosion height of the reactive jet liner on the damage effect to the steel target was studied. A static explosion experiment was carried out, and the optimal structural and performance parameters for the reactive material and explosion height of the Citation: Zhang, X.; Wang, Z.; Yin, J.; reactive jet liner were obtained. -
Penetration of a Shaped Charge
Penetration of a Shaped Charge Chris Poole Corpus Christi College University of Oxford A thesis submitted for the degree of Doctor of Philosophy Trinity 2005 Acknowledgements This research was funded by the EPSRC and QinetiQ, both of whom I would like to thank for funding the project. I would also like to thank my supervisor, Jon Chapman, for his inspiration and guidance throughout this work. I am also indebted to John Curtis (QinetiQ) for his invaluable support on the project. I must also thank John Ockendon, who has been a fountain of enthusiasm and stimulation throughout the project. Sasha Korobkin must be thanked for his input and insight into the chapter on filling-flows. The metallurgical analysis would not have been possible without the help of Paula Topping and others in the Materials Department, whom I would like to acknowledge. Finally, on a Mathematical note, I would like to thank all those in OCIAM who have helped me throughout the project. On a more personal level, I would like to thank all of those who have supported me and given me encouragement (and distractions!) since I have been in Oxford. In particular, I must mention the support of my family, the joviality of my friends in OCIAM (especially the DH9/DH10 folk, past and present), the conviviality of the OUSCR (and other ringers), and any other friends I haven’t yet mentioned. It is the mixture of all these people that has kept me (relatively) sane and made my time in Oxford so enjoyable. Abstract A shaped charge is an explosive device used to penetrate thick targets using a high velocity jet. -
Shock Initiation Experiments and Modeling of Composition B and C-4
UCRL-CONF-222137 SHOCK INITIATION EXPERIMENTS AND MODELING OF COMPOSITION B AND C-4 Paul A. Urtiew, Kevin S. Vandersall, Craig M. Tarver, Frank Garcia, Jerry W. Forbes June 16, 2006 13th International Detonation Symposium Norfolk, VA, United States July 23, 2006 through July 28, 2006 Disclaimer This document was prepared as an account of work sponsored by an agency of the United States Government. Neither the United States Government nor the University of California nor any of their employees, makes any warranty, express or implied, or assumes any legal liability or responsibility for the accuracy, completeness, or usefulness of any information, apparatus, product, or process disclosed, or represents that its use would not infringe privately owned rights. Reference herein to any specific commercial product, process, or service by trade name, trademark, manufacturer, or otherwise, does not necessarily constitute or imply its endorsement, recommendation, or favoring by the United States Government or the University of California. The views and opinions of authors expressed herein do not necessarily state or reflect those of the United States Government or the University of California, and shall not be used for advertising or product endorsement purposes. SHOCK INITIATION EXPERIMENTS AND MODELING OF COMPOSITION B AND C-4 Paul A. Urtiew1, Kevin S. Vandersall1, Craig M. Tarver1, Frank Garcia1, and Jerry W. Forbes2 1Energetic Materials Center, Lawrence Livermore National Laboratory, Livermore, CA 94550 2Center for Energetic Concepts Development, University of Maryland, College Park, MD 20742 Abstract. Shock initiation experiments on the explosives Composition B and C- 4 were performed to obtain in-situ pressure gauge data for the purpose of determining the Ignition and Growth reactive flow model with proper modeling parameters. -
Penetration in Granite by Shaped Charge Liners of Various Metals
Scholars' Mine Doctoral Dissertations Student Theses and Dissertations 1970 Penetration in granite by shaped charge liners of various metals Hemendra Nath Kalia Follow this and additional works at: https://scholarsmine.mst.edu/doctoral_dissertations Part of the Mining Engineering Commons Department: Mining Engineering Recommended Citation Kalia, Hemendra Nath, "Penetration in granite by shaped charge liners of various metals" (1970). Doctoral Dissertations. 2038. https://scholarsmine.mst.edu/doctoral_dissertations/2038 This thesis is brought to you by Scholars' Mine, a service of the Missouri S&T Library and Learning Resources. This work is protected by U. S. Copyright Law. Unauthorized use including reproduction for redistribution requires the permission of the copyright holder. For more information, please contact [email protected]. PENETRATION IN GRANITE BY SHAPED CHARGE LINERS OF VARIOUS METALS by HEMENDRA NATH KALlA, 1939 A DISSERTATION Presented to the Faculty of the Graduate School of the UNIVERSITY OF MISSOURI-ROLLA In Partial Fulfillment of the Require~ts for the Degree DOCTOR OF PHILOSOPHY in MINING ENGINEERING T2388 1970 c. I 92 pages 193955 i i ABSTRACT The penetration in Missouri red granite by cylindrical charges with metal liners of aluminum 2011 (T-3), aluminum 7075 (T-6), yellow brass, monel, maraging steel (vascomax 250), and copper was measured. Metals having high ductility and moderate compressive strength penetrated deeper than high strength maraging steel. Aluminum required a greater standoff for optimum penetration than the other metal liners tested. Preliminary metallographic studies of the liner metals and slugs showed that the grains had elongated along the slug axis. The metals containing zinc formed very small or no slugs. -
Material Combination to Mitigation of Behind Armour Debris After Shaped
MATEC Web of Conferences 182, 02009 (2018) https://doi.org/10.1051/matecconf/201818202009 17th International Conference Diagnostics of Machines and Vehicles Material combination to mitigation of behind armour debris after shaped charge jet attack Marek Szudrowicz1,*1 1Wojskowy Instytut Techniki Pancernej i Samochodowej, 05-070 Sulejówek, Okuniewska 1, Poland Abstract. When a shaped charge jet perforates the steel armour plate, the residual jet is accompanied by a much wider cloud of behind armour debris (BAD) generated by stress wave interactions. BAD plays an important role in the evaluation of survivability of vehicle crew and components in a vehicle. The Behind Armor Debris (BAD) cloud caused by shaped charge jet impact was investigated. In order to simulate different configuration of material to mitigation of debris cloud the thickness of ceramics target tiles, glass and aramid laminate liners in contact with the armour plates was varied. 1 Introduction Armour Piercing Discarding Sabot (APDS) projectiles and High Explosive Anti-Tank (HEAT) warheads are the main weapons used to damage or destroy armoured vehicles. If a such a warhead hits a vehicle, the highest danger for the crew is posed, apart primary jet, by fragments of the primary jet and armour spalls, which may reach a speed o 1000 m/s in case of heavier fragments and about 3000 m/s in case of the lighter ones. Additionally, effects related to changes of temperature and pressure should be considered (Fig. 1) [1]. Fig. 1. Effects of the penetration of armour. Behind armour debris. The following means are employed in design solutions in order to increase the chances of a vehicle crew to survive when vehicle is in danger of being hit by a HEAT warhead: - detonation of the warhead or otherwise destroying it at some distance from the vehicle, - disturbing, breaking or fragmenting the shaped charge jet produced after detonation of the warhead, - reduction of the depth of penetration, - minimizing of the above-mentioned detrimental effects caused by shaped charge jet penetrating the armour [2,3,4,5,6,7].