KR20220012725A - Penetrator with explosive warhead having high explosive ability - Google Patents
Penetrator with explosive warhead having high explosive ability Download PDFInfo
- Publication number
- KR20220012725A KR20220012725A KR1020200091881A KR20200091881A KR20220012725A KR 20220012725 A KR20220012725 A KR 20220012725A KR 1020200091881 A KR1020200091881 A KR 1020200091881A KR 20200091881 A KR20200091881 A KR 20200091881A KR 20220012725 A KR20220012725 A KR 20220012725A
- Authority
- KR
- South Korea
- Prior art keywords
- penetrator
- explosive
- metal plate
- tungsten
- warhead
- Prior art date
Links
- 239000002360 explosive Substances 0.000 title claims abstract description 45
- 229910052751 metal Inorganic materials 0.000 claims abstract description 76
- 239000002184 metal Substances 0.000 claims abstract description 76
- 239000000463 material Substances 0.000 claims abstract description 26
- 238000002844 melting Methods 0.000 claims abstract description 9
- 230000008018 melting Effects 0.000 claims abstract description 9
- 238000000034 method Methods 0.000 claims description 19
- 238000004880 explosion Methods 0.000 claims description 17
- 239000003795 chemical substances by application Substances 0.000 claims description 14
- 239000010949 copper Substances 0.000 claims description 14
- UQSXHKLRYXJYBZ-UHFFFAOYSA-N Iron oxide Chemical compound [Fe]=O UQSXHKLRYXJYBZ-UHFFFAOYSA-N 0.000 claims description 13
- 239000002131 composite material Substances 0.000 claims description 13
- 238000006243 chemical reaction Methods 0.000 claims description 12
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 11
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 10
- 229910052802 copper Inorganic materials 0.000 claims description 8
- 239000011701 zinc Substances 0.000 claims description 7
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 claims description 6
- 229910052782 aluminium Inorganic materials 0.000 claims description 6
- IWOUKMZUPDVPGQ-UHFFFAOYSA-N barium nitrate Chemical compound [Ba+2].[O-][N+]([O-])=O.[O-][N+]([O-])=O IWOUKMZUPDVPGQ-UHFFFAOYSA-N 0.000 claims description 6
- 229920000642 polymer Polymers 0.000 claims description 6
- 229910052717 sulfur Inorganic materials 0.000 claims description 6
- 239000011593 sulfur Substances 0.000 claims description 6
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims description 5
- 238000002347 injection Methods 0.000 claims description 5
- 239000007924 injection Substances 0.000 claims description 5
- NDLPOXTZKUMGOV-UHFFFAOYSA-N oxo(oxoferriooxy)iron hydrate Chemical compound O.O=[Fe]O[Fe]=O NDLPOXTZKUMGOV-UHFFFAOYSA-N 0.000 claims description 5
- 239000000843 powder Substances 0.000 claims description 5
- 239000003832 thermite Substances 0.000 claims description 5
- 229910052725 zinc Inorganic materials 0.000 claims description 5
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims description 4
- 239000000020 Nitrocellulose Substances 0.000 claims description 4
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 4
- JKWMSGQKBLHBQQ-UHFFFAOYSA-N diboron trioxide Chemical compound O=BOB=O JKWMSGQKBLHBQQ-UHFFFAOYSA-N 0.000 claims description 4
- 229910052742 iron Inorganic materials 0.000 claims description 4
- NUJOXMJBOLGQSY-UHFFFAOYSA-N manganese dioxide Chemical compound O=[Mn]=O NUJOXMJBOLGQSY-UHFFFAOYSA-N 0.000 claims description 4
- 229910044991 metal oxide Inorganic materials 0.000 claims description 4
- 150000004706 metal oxides Chemical class 0.000 claims description 4
- 229920001220 nitrocellulos Polymers 0.000 claims description 4
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims description 3
- AWXLLPFZAKTUCQ-UHFFFAOYSA-N [Sn].[W] Chemical compound [Sn].[W] AWXLLPFZAKTUCQ-UHFFFAOYSA-N 0.000 claims description 3
- -1 acetcellulose Chemical compound 0.000 claims description 3
- 229910045601 alloy Inorganic materials 0.000 claims description 3
- 239000000956 alloy Substances 0.000 claims description 3
- 229910018084 Al-Fe Inorganic materials 0.000 claims description 2
- 229910018192 Al—Fe Inorganic materials 0.000 claims description 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims description 2
- QPLDLSVMHZLSFG-UHFFFAOYSA-N Copper oxide Chemical compound [Cu]=O QPLDLSVMHZLSFG-UHFFFAOYSA-N 0.000 claims description 2
- 239000005751 Copper oxide Substances 0.000 claims description 2
- 229910017518 Cu Zn Inorganic materials 0.000 claims description 2
- 229910017752 Cu-Zn Inorganic materials 0.000 claims description 2
- 229910017827 Cu—Fe Inorganic materials 0.000 claims description 2
- 229910017943 Cu—Zn Inorganic materials 0.000 claims description 2
- 229910001030 Iron–nickel alloy Inorganic materials 0.000 claims description 2
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 2
- ZLMJMSJWJFRBEC-UHFFFAOYSA-N Potassium Chemical compound [K] ZLMJMSJWJFRBEC-UHFFFAOYSA-N 0.000 claims description 2
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 2
- WGLPBDUCMAPZCE-UHFFFAOYSA-N Trioxochromium Chemical compound O=[Cr](=O)=O WGLPBDUCMAPZCE-UHFFFAOYSA-N 0.000 claims description 2
- OWUGOENUEKACGV-UHFFFAOYSA-N [Fe].[Ni].[W] Chemical compound [Fe].[Ni].[W] OWUGOENUEKACGV-UHFFFAOYSA-N 0.000 claims description 2
- AHIVCQLQCIBVOS-UHFFFAOYSA-N [Fe].[W] Chemical compound [Fe].[W] AHIVCQLQCIBVOS-UHFFFAOYSA-N 0.000 claims description 2
- FEAYSNXRKILIGP-UHFFFAOYSA-N [Zn].[Cu].[W] Chemical compound [Zn].[Cu].[W] FEAYSNXRKILIGP-UHFFFAOYSA-N 0.000 claims description 2
- CYUOWZRAOZFACA-UHFFFAOYSA-N aluminum iron Chemical compound [Al].[Fe] CYUOWZRAOZFACA-UHFFFAOYSA-N 0.000 claims description 2
- 229910000416 bismuth oxide Inorganic materials 0.000 claims description 2
- 229910052796 boron Inorganic materials 0.000 claims description 2
- 229910000423 chromium oxide Inorganic materials 0.000 claims description 2
- IYRDVAUFQZOLSB-UHFFFAOYSA-N copper iron Chemical compound [Fe].[Cu] IYRDVAUFQZOLSB-UHFFFAOYSA-N 0.000 claims description 2
- 229910000431 copper oxide Inorganic materials 0.000 claims description 2
- SBYXRAKIOMOBFF-UHFFFAOYSA-N copper tungsten Chemical compound [Cu].[W] SBYXRAKIOMOBFF-UHFFFAOYSA-N 0.000 claims description 2
- TYIXMATWDRGMPF-UHFFFAOYSA-N dibismuth;oxygen(2-) Chemical compound [O-2].[O-2].[O-2].[Bi+3].[Bi+3] TYIXMATWDRGMPF-UHFFFAOYSA-N 0.000 claims description 2
- 229910052741 iridium Inorganic materials 0.000 claims description 2
- 229910000464 lead oxide Inorganic materials 0.000 claims description 2
- 229910052744 lithium Inorganic materials 0.000 claims description 2
- 229910000103 lithium hydride Inorganic materials 0.000 claims description 2
- 229910052749 magnesium Inorganic materials 0.000 claims description 2
- 239000011777 magnesium Substances 0.000 claims description 2
- 239000000203 mixture Substances 0.000 claims description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 2
- MOWMLACGTDMJRV-UHFFFAOYSA-N nickel tungsten Chemical compound [Ni].[W] MOWMLACGTDMJRV-UHFFFAOYSA-N 0.000 claims description 2
- YEXPOXQUZXUXJW-UHFFFAOYSA-N oxolead Chemical compound [Pb]=O YEXPOXQUZXUXJW-UHFFFAOYSA-N 0.000 claims description 2
- 229910052700 potassium Inorganic materials 0.000 claims description 2
- 239000011591 potassium Substances 0.000 claims description 2
- 239000010703 silicon Substances 0.000 claims description 2
- 229910052710 silicon Inorganic materials 0.000 claims description 2
- 235000012239 silicon dioxide Nutrition 0.000 claims description 2
- 239000000377 silicon dioxide Substances 0.000 claims description 2
- 239000010936 titanium Substances 0.000 claims description 2
- 229910052719 titanium Inorganic materials 0.000 claims description 2
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 claims description 2
- 229910052721 tungsten Inorganic materials 0.000 claims description 2
- 239000010937 tungsten Substances 0.000 claims description 2
- XZLXGTUBUCMRCH-UHFFFAOYSA-N tungsten zinc Chemical compound [Zn].[W] XZLXGTUBUCMRCH-UHFFFAOYSA-N 0.000 claims description 2
- 229910001928 zirconium oxide Inorganic materials 0.000 claims description 2
- FJWGYAHXMCUOOM-QHOUIDNNSA-N [(2s,3r,4s,5r,6r)-2-[(2r,3r,4s,5r,6s)-4,5-dinitrooxy-2-(nitrooxymethyl)-6-[(2r,3r,4s,5r,6s)-4,5,6-trinitrooxy-2-(nitrooxymethyl)oxan-3-yl]oxyoxan-3-yl]oxy-3,5-dinitrooxy-6-(nitrooxymethyl)oxan-4-yl] nitrate Chemical compound O([C@@H]1O[C@@H]([C@H]([C@H](O[N+]([O-])=O)[C@H]1O[N+]([O-])=O)O[C@H]1[C@@H]([C@@H](O[N+]([O-])=O)[C@H](O[N+]([O-])=O)[C@@H](CO[N+]([O-])=O)O1)O[N+]([O-])=O)CO[N+](=O)[O-])[C@@H]1[C@@H](CO[N+]([O-])=O)O[C@@H](O[N+]([O-])=O)[C@H](O[N+]([O-])=O)[C@H]1O[N+]([O-])=O FJWGYAHXMCUOOM-QHOUIDNNSA-N 0.000 claims 1
- 150000002483 hydrogen compounds Chemical class 0.000 claims 1
- 238000004519 manufacturing process Methods 0.000 abstract description 15
- 230000006378 damage Effects 0.000 abstract description 14
- 239000003721 gunpowder Substances 0.000 description 17
- 239000000376 reactant Substances 0.000 description 10
- 230000000149 penetrating effect Effects 0.000 description 6
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 5
- 239000008188 pellet Substances 0.000 description 5
- 239000004014 plasticizer Substances 0.000 description 4
- 241000736199 Paeonia Species 0.000 description 3
- 235000006484 Paeonia officinalis Nutrition 0.000 description 3
- 239000000654 additive Substances 0.000 description 3
- 150000001875 compounds Chemical class 0.000 description 3
- 239000007789 gas Substances 0.000 description 3
- 230000035515 penetration Effects 0.000 description 3
- 230000035945 sensitivity Effects 0.000 description 3
- FMAXRAJQUCPQHD-UHFFFAOYSA-N 2-amino-1-nitroguanidine;nitric acid Chemical compound O[N+]([O-])=O.NN=C(N)N[N+]([O-])=O FMAXRAJQUCPQHD-UHFFFAOYSA-N 0.000 description 2
- 241000273930 Brevoortia tyrannus Species 0.000 description 2
- NDYLCHGXSQOGMS-UHFFFAOYSA-N CL-20 Chemical compound [O-][N+](=O)N1C2N([N+]([O-])=O)C3N([N+](=O)[O-])C2N([N+]([O-])=O)C2N([N+]([O-])=O)C3N([N+]([O-])=O)C21 NDYLCHGXSQOGMS-UHFFFAOYSA-N 0.000 description 2
- 229910002651 NO3 Inorganic materials 0.000 description 2
- NHNBFGGVMKEFGY-UHFFFAOYSA-N Nitrate Chemical compound [O-][N+]([O-])=O NHNBFGGVMKEFGY-UHFFFAOYSA-N 0.000 description 2
- TZRXHJWUDPFEEY-UHFFFAOYSA-N Pentaerythritol Tetranitrate Chemical compound [O-][N+](=O)OCC(CO[N+]([O-])=O)(CO[N+]([O-])=O)CO[N+]([O-])=O TZRXHJWUDPFEEY-UHFFFAOYSA-N 0.000 description 2
- IGUHATROZYFXKR-UHFFFAOYSA-N [W].[Ir] Chemical compound [W].[Ir] IGUHATROZYFXKR-UHFFFAOYSA-N 0.000 description 2
- 230000000996 additive effect Effects 0.000 description 2
- 239000000853 adhesive Substances 0.000 description 2
- 230000001070 adhesive effect Effects 0.000 description 2
- 239000003054 catalyst Substances 0.000 description 2
- 230000001066 destructive effect Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 2
- 229910052737 gold Inorganic materials 0.000 description 2
- 239000010931 gold Substances 0.000 description 2
- 229910052739 hydrogen Inorganic materials 0.000 description 2
- 239000001257 hydrogen Substances 0.000 description 2
- 238000000465 moulding Methods 0.000 description 2
- UZGLIIJVICEWHF-UHFFFAOYSA-N octogen Chemical compound [O-][N+](=O)N1CN([N+]([O-])=O)CN([N+]([O-])=O)CN([N+]([O-])=O)C1 UZGLIIJVICEWHF-UHFFFAOYSA-N 0.000 description 2
- 239000007800 oxidant agent Substances 0.000 description 2
- 239000002689 soil Substances 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910000975 Carbon steel Inorganic materials 0.000 description 1
- 239000000026 Pentaerythritol tetranitrate Substances 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 229910001297 Zn alloy Inorganic materials 0.000 description 1
- 238000009835 boiling Methods 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000010962 carbon steel Substances 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 238000000748 compression moulding Methods 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- TVZPLCNGKSPOJA-UHFFFAOYSA-N copper zinc Chemical compound [Cu].[Zn] TVZPLCNGKSPOJA-UHFFFAOYSA-N 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000005474 detonation Methods 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- 238000013467 fragmentation Methods 0.000 description 1
- 238000006062 fragmentation reaction Methods 0.000 description 1
- 230000003116 impacting effect Effects 0.000 description 1
- 239000000411 inducer Substances 0.000 description 1
- 230000001939 inductive effect Effects 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- GKOZUEZYRPOHIO-UHFFFAOYSA-N iridium atom Chemical compound [Ir] GKOZUEZYRPOHIO-UHFFFAOYSA-N 0.000 description 1
- WABPQHHGFIMREM-UHFFFAOYSA-N lead(0) Chemical compound [Pb] WABPQHHGFIMREM-UHFFFAOYSA-N 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 229960004321 pentaerithrityl tetranitrate Drugs 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 238000012805 post-processing Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000009257 reactivity Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 230000001960 triggered effect Effects 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/04—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type
- F42B12/10—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with shaped or hollow charge
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B33/00—Compositions containing particulate metal, alloy, boron, silicon, selenium or tellurium with at least one oxygen supplying material which is either a metal oxide or a salt, organic or inorganic, capable of yielding a metal oxide
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B1/00—Explosive charges characterised by form or shape but not dependent on shape of container
- F42B1/02—Shaped or hollow charges
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/44—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information of incendiary type
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- General Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
Description
본 발명은 소이성 물질을 안정적으로 함유하는 고폭소이능을 갖는 폭발형성탄두를 포함하는 관통자에 관한 것으로, 보다 구체적으로 탄두 자체 내에 소이성 물질을 머금고 있어 목표물에 1차 충돌시 내부 관성에 의해 압력을 받아 작열하며 2차 파괴를 유발하는 소이 및 반응성 관통자에 관한 것이다.The present invention relates to a penetrator comprising an explosive-forming warhead having a high explosive incendiary ability containing stably incendiary material, and more particularly, by retaining an incendiary material in the warhead itself, due to internal inertia during the first collision with a target. It relates to incendiary and reactive penetrators that glow under pressure and cause secondary destruction.
장갑 등의 표적을 파괴시키기 위해 화약의 폭발에너지를 집중하는 메커니즘을 갖는 지향성에너지 탄두의 종류에는 성형작약탄두(Shaped Charge Warhead)와 폭발성형관통자(Explosively Formed Penetrator, EFP)를 이용하는 것이 대표적이다. The typical types of directional energy warheads that have a mechanism to focus the explosive energy of gunpowder to destroy targets such as armor are the Shaped Charge Warhead and the Explosively Formed Penetrator (EFP).
성형작약은 화약에너지에 의해 생성된 초고속의 제트가 장갑과 충돌하는 과정에서 발생되는 압력이 장갑재료의 항복강도를 크게 초과하므로 장갑을 관통할 수 있는 충분한 에너지를 갖게 된다.The molding charge has enough energy to penetrate the armor because the pressure generated during the collision of the high-speed jet generated by the energy of the gunpowder with the armor greatly exceeds the yield strength of the armor material.
폭발성형관통자는 일반적으로 작약의 기폭시 폭발에너지에 고속으로 사출된 금속 라이너가 재질, 두께, 직경, 만곡도, 폭굉파의 형상 등에 따라 구형, 탄자형, 봉형 등으로 변형되고 목표물에 충돌시켜 파괴하는 관통자로 전차 및 장갑차의 발전하는 방호력에 대응하기 위해 개발되었으며, 장갑 차량의 취약부인 상부 장갑 관통을 목적으로 하고 있다. 전방이 개방된 탄체의 내부에 주작약이 채워지고, 탄체의 개방된 전방에 라이너는 밀폐시키는 구조를 가진다. 주작약이 폭팔하면서 라이너가 자가단조에 의해 관통자로 변형되고, 관통자가 목표물에 충돌됨으로써 목표물을 파괴하게 된다. 기존의 라이너는 원판형상으로 형성되고 전방을 향해 볼록한 형상을 가지며 폭발시 관통자로 성형되어 1000 m/s 이상의 초고속으로 목표물을 향해 비행하게 된다.In general, when detonating a peony, the metal liner injected at high speed with the explosive energy is transformed into a spherical shape, a ballistic shape, or a rod shape depending on the material, thickness, diameter, curvature, and the shape of the detonation wave, and collides with the target to destroy it. It was developed to counter the evolving protection power of tanks and armored vehicles as a penetrator, and aims to penetrate the upper armor, which is the weak point of armored vehicles. The main peony is filled in the inside of the bullet with the front open, and the liner in the open front of the bullet has a sealing structure. As the main peony explodes, the liner is transformed into a penetrator by self-forging, and the penetrator collides with the target, thereby destroying the target. The existing liner is formed in the shape of a disk, has a convex shape toward the front, and is formed into a penetrator in case of an explosion, so that it flies toward the target at a high speed of 1000 m/s or more.
기존의 폭발성형관통자의 탄두는 화약이 없이 조립된 탄두에 화약을 용융하여 충전하거나, 압축형 복합화약을 합축성형하여 화약 펠릿을 성형한 후 펠릿을 탄두 내 공간에 삽일될 수 있도록 후가공한 후 후가공된 화약 펠릿을 탄두 내에 조립하는 방법으로 제작하고 있다. 그러나 화약이 없이 조립된 탄두에 화약을 용융하여 충전하여 폭발성형관통자 탄두를 제조하는 경우 용융된 화약이 응고될 때 수축하여 화약 내부 기공 등의 발생으로 화약의 충전상태가 균일하지 못해 품질문제가 발생하고, 추후 관통자로 성형되는 라이너를 조립할 때 화약과 라이너의 접착면의 완전한 밀착이 어려워 화약과 라이너 사이에 간극이 발생하는 문제점이 있다. 또한, 성형된 화약 펠릿을 후가공한 후 탄두에 조립하는 경우 성형된 화약 펠릿과 라이너의 접착면의 완전한 밀착이 어려워 화약과 라이너 사이에 간극이 발생하고, 화약 펠릿과 라이너 사이의 간극 제거를 위해 추가적인 압착공정이 필요하여 제조공정이 복잡하고, 생산성이 낮으며, 제조원가가 증대되는 문제점이 있다. 또한, 파편 및 폭발성형관통자의 복합기능을 갖는 탄두를 구성하여 실제 유도탄 내에 배치하여 운용할 시에는 탄두 전방에 배치된 구성 스틸, 알루미늄 및 플라스틱 재질 등의 간섭효과에 의해 폭발성형관통자의 관통 성능 저하 및 관통에너지가 완전히 소모될 수도 있다.The warhead of the existing explosive-molded penetrator is either charged by melting gunpowder into a warhead assembled without gunpowder, or by compression-molding a compression-type compound gunpowder to form gunpowder pellets and post-processing so that the pellets can be inserted into the space within the warhead. It is manufactured by assembling the used gunpowder pellets in the warhead. However, in the case of manufacturing an explosive penetrator warhead by melting and charging gunpowder into a warhead assembled without gunpowder, it shrinks when the molten gunpowder solidifies and causes internal pores in the gunpowder to cause quality problems due to the inconsistent filling state of the gunpowder. However, when assembling a liner that is later formed into a penetrator, there is a problem in that a gap occurs between the gunpowder and the liner because it is difficult to completely adhere to the adhesive surface of the gunpowder and the liner. In addition, when the molded gunpowder pellets are post-processed and then assembled into the warhead, it is difficult to completely adhere to the adhesive surface of the molded gunpowder pellets and the liner, resulting in a gap between the gunpowder and the liner. There are problems in that the manufacturing process is complicated because a pressing process is required, the productivity is low, and the manufacturing cost is increased. In addition, when a warhead with a complex function of fragmentation and explosive-molding penetrator is configured and deployed and operated in an actual guided missile, the penetration performance of the explosive-molded penetrator is reduced due to the interference effect of the constituent steel, aluminum, and plastic materials placed in front of the warhead. and the penetrating energy may be completely consumed.
결론적으로, 종래의 폭발성형관통자는 단순히 폭발 후에 발생된 금속 성형 탄두를 이용하여 기존의 성형작약탄과 같은 단순관통자를 형성하는데에 고안을 멈추었고, 이러한 폭발성형관통자를 포함하는 탄두가 유도탄 내에 배치되었을 때 관통에너지가 소모되어 실제 표적을 무력화 시킬 수 있는 관통력을 갖지 못하게 되는 것이 일반적 현상이었다. 또한, 기존의 성형작약탄 또는 폭발성형관통자의 경우 폭발이 반대 방향으로 적용되거나 그 자리에 멈추도록 만드는 반응장갑이나 주장갑과 외장의 사이에 공간을 만들어 관통력을 줄이는 중공장갑(공간장갑) 및 2개의 장갑판 사이에 세라믹스 등의 복합소재를 채워넣은 복합장갑 등의 기술로 인해 무력화되는 경우가 많다. 외국 특허의 경우에도 목표물을 관통자로 1차 접촉 파괴한 후 반응성 물질을 그 공간 안으로 투입하여 2차 파괴를 유발하는 방식의 폭발 성형 관통자에 대한 언급만 있을 뿐이다.In conclusion, the conventional explosive-shaped penetrator simply stopped devising to form a simple penetrator like the conventional compacted charge bomb by using the metal-shaped warhead generated after the explosion, and the warhead including this explosive-shaped penetrator could have been placed in the guided missile. It was a common phenomenon that the penetrating energy was consumed and the penetrating force was not able to neutralize the actual target. In addition, in the case of conventional molded charge bombs or explosive molded penetrators, reactive armor that causes the explosion to be applied in the opposite direction or stop there, or heavy armor that reduces penetration by creating a space between the main armor and the exterior (space armor) and 2 In many cases, it is incapacitated by technology such as composite gloves filled with composite materials such as ceramics between the dog's armor plates. Even in the case of foreign patents, there is only mention of an explosion-molded penetrator in a method in which a target is first contact-destroyed with a penetrator and then a reactive material is injected into the space to cause secondary destruction.
이에, 본 발명자들은 운동에너지로 물리적인 파괴를 기대하는 종래의 폭발성형관통자와 달리 목표물의 1차 접촉 파괴 지점 자체에서 또다른 폭발을 일으켜 2차 파괴를 일으키는 고폭소이능을 갖는 폭발형성탄두를 포함하는 소이 및 반응성 관통자를 제조하여 본 발명을 완성하였다.Accordingly, the present inventors have included an explosive-forming warhead with high explosive incendiary ability to cause secondary destruction by causing another explosion at the first contact destruction point of the target itself, unlike the conventional explosive-type penetrator, which expects physical destruction with kinetic energy. The present invention was completed by preparing incendiary and reactive penetrators.
기존 폭발성형관통자의 경우 성형작약탄과 같은 단순관통자를 형성하는데에서 고안을 멈추었고, 반응장갑이나 공간장갑 등의 기술로 인해 무력화되는 경우가 많아, 효과적으로 목표물을 파괴하는 폭발성형관통자가 요구되고 있다.In the case of the existing explosive-shaped penetrator, the design stopped at forming a simple penetrator such as a shaped charge bomb, and it is often disabled due to technologies such as reactive armor or space armor, so an explosive-shaped penetrator that effectively destroys the target is required.
따라서, 본 발명은 1차 접촉 파괴 지점에 폭발을 일으켜 2차 파괴를 유발하는 고폭소이능을 갖는 폭발형성탄두를 포함하는 관통자를 제공하기 위한 것이다. Accordingly, an object of the present invention is to provide a penetrator including an explosive-forming warhead having a high explosive incendiary ability that causes an explosion at a primary contact destruction point to cause secondary destruction.
상기 목적을 달성하기 위해, 본 발명의 발명자는 자체 내에 소이성 물질을 머금고 목표물과 1차 충돌시 관성에 의해 내부에서 압력을 받아 작열하여 큰 2차 파괴를 유발하는 고폭소이능을 갖는 폭발형성탄두를 포함하는 관통자를 제공한다.In order to achieve the above object, the inventor of the present invention holds an incendiary material within itself and burns under pressure from the inside due to inertia during the first collision with a target to form an explosion having a high explosive ability to cause a large secondary destruction A penetrator containing a warhead is provided.
본 발명의 고폭소이능을 갖는 폭발형성탄두를 포함하는 관통자는 충돌한 목표물을 파괴하고 목표물 내부에서 촉발된 소이제의 반응으로 인한 폭발적 열팽창 유발로 내부 구조물을 효율적으로 파괴할 수 있어, 산업적 목적으로 일반 건축물 폭파해체의 응용을 포함하여 기존의 폭약으로는 해체가 까다롭거나 폭파가 곤란한 돌과 흙 등이 포함된 산이나 땅에서 사용할 수 있고, 군사적 목적으로 벙커 관통용이나 대전차 미사일 등의 탄두에도 응용되어 사용할 수 있다.The penetrator including the explosive-forming warhead having the high explosive incendiary ability of the present invention can destroy the colliding target and efficiently destroy the internal structure by inducing the explosive thermal expansion due to the reaction of the incendiary agent triggered inside the target. Existing explosives, including the application of demolition of general buildings, can be used in mountains or land containing stones and soil that are difficult to dismantle or detonate with conventional explosives. can be applied and used.
도 1은 발사체에 부착된 폭발형성탄두를 나타낸 도이다.
100 : 뒷부분 금속판
101 : 앞부분 금속판
102 : 복합소이제
103 : 발사체 케이스
104 : 발사체의 기폭장치
105 : 발사체의 반응물
도 2는 발사체에 의해 폭발사출된 폭발형성탄두가 관통자로 변형되는 과정을 간단히 나타낸 도이다.
도3은 폭발형성탄두를 포함하는 관통자가 목표물을 파괴하는 과정을 간단히 나타낸 도이다.
106 : 1차 목표물
107 : 2차 목표물1 is a view showing an explosive-forming warhead attached to a projectile.
100: back metal plate
101: front metal plate
102: complex incinerator
103: projectile case
104: projectile detonator
105: the reactant of the projectile
2 is a diagram briefly illustrating a process in which an explosion-forming warhead exploded and ejected by a projectile is transformed into a penetrator.
3 is a diagram schematically illustrating a process in which a penetrator including an explosive-forming warhead destroys a target.
106: primary target
107: secondary target
이하, 본원의 발명이 속하는 기술분야에서 통상의 지식을 가진 자가 용이하게 실시할 수 있도록 본 발명의 실시형태를 들어 상세히 설명한다. 본 발명의 실시형태는 당업계에서 평균적인 지식을 가진 자에게 본 발명을 더욱 완전하게 설명하기 위해서 제공되는 것이다. 따라서, 본 발명의 실시형태는 여러 가지 다른 형태로 변형될 수 있으며, 본 발명의 범위가 이하 설명하는 실시형태로 한정되는 것은 아니다.Hereinafter, embodiments of the present invention will be described in detail so that those of ordinary skill in the art to which the present invention pertains can easily carry out the present invention. The embodiments of the present invention are provided in order to more completely explain the present invention to those of ordinary skill in the art. Accordingly, the embodiment of the present invention may be modified in various other forms, and the scope of the present invention is not limited to the embodiments described below.
본 발명의 명세서 전체에서, 어떤 부분이 어떤 구성 요소를 "포함"한다고 할 때, 이는 특별히 반대되는 기재가 없는 한 다른 구성 요소를 제외하는 것이 아니라 다른 구성 요소를 더 포함할 수 있는 것을 의미한다.Throughout the specification of the present invention, when a part "includes" a certain component, it means that other components may be further included, rather than excluding other components, unless otherwise stated.
본 발명의 명세서 전체에서 사용되는 용어 "~ (하는) 단계" 또는 "~의 단계"는 "~를 위한 단계"를 의미하지 않는다.As used throughout the specification of the present invention, the term “step for (to)” or “step for” does not mean “step for”.
본 발명은 발사체의 반응물에 의해 사출되어 목표물까지 안정적으로 날아가다가 목표물을 타격하고, 목표물에 1차 충돌시 2개의 금속판 안에 있는 소이성 물질에 의한 2차 폭발이 발생하여 목표물을 파괴하는 고폭소이능을 갖는 폭발형성탄두를 포함하는 관통자를 제공한다. 또한 상기 고폭소이능을 갖는 폭발형성탄두를 포함하는 관통자는 소이성 물질을 안정적으로 포함할 수 있다.The present invention is a high-explosive incendiary ability that is ejected by the reactant of a projectile, stably flies to the target, hits the target, and when the target first collides, a secondary explosion by incendiary materials in two metal plates occurs to destroy the target It provides a penetrator comprising an explosive-forming warhead having a. In addition, the penetrator including the explosive-forming warhead having the high explosive ability may stably contain an incendiary material.
본 발명에 있어서, 상기 2차 폭발은 발사체의 반응물에 의해 발사된 폭발형성탄두와 목표물의 1차 충돌시 내부 관성에 의한 관통자 후방의 전진 압력이 금속판 안에 포함된 소이성 물질을 밀어내어 발생할 수 있다.In the present invention, the secondary explosion can be generated by pushing the incendiary material contained in the metal plate by the forward pressure behind the penetrator due to internal inertia during the first collision of the target with the explosive-forming warhead fired by the reactant of the projectile. .
본 발명에 있어서, 상기 소이성 물질은 일반적으로 사용되는 군사용이나 산업용 테르밋 제재를 사용할 경우 파괴적 특성이 발생하지 않을 수 있으므로, 테르밋 반응을 일으키는 밀도가 높은 금속 자체 또는 이의 수소화합물 및 소결된 금속 자체 또는 이의 수소화합물을 이용한 복합소이제일 수 있다. 또한, 상기 복합소이제는 밀도가 높을수록 위력이 증가할 수 있다.In the present invention, since the destructive properties may not occur when the generally used military or industrial thermite material is used, the inflammable material has a high density of the metal itself or its hydrogen compound and the sintered metal itself or It may be a complex incinerator using its hydrogen compound. In addition, the power of the complex incinerator may increase as the density increases.
상기 테르밋 반응은 금속산화물(산화제)이 금속분말(연료)에 의해 탈산되면서 강력한 반응열을 발생하는 반응으로, 반응식은 하기 (1)와 같다.The thermite reaction is a reaction in which a metal oxide (oxidizer) is deoxidized by a metal powder (fuel) to generate strong heat of reaction, and the reaction formula is shown in (1) below.
테르밋 반응(Thermite Reaction)= 2M + Y2O3 → 2Y + M2O3 (1)Thermite Reaction = 2M + Y 2 O 3 → 2Y + M 2 O 3 (1)
상기 반응식에서 M은 알루미늄, 리튬, 칼륨, 마그네슘, 타이타늄, 아연, 규소, 붕소 등을 포함하는 금속분말일 수 있고, 상기 금속분말을 단독 또는 혼합하여 사용할 수 있으나, 끓는 점이 높고 가격이 싼 알루미늄이 가장 흔하게 사용될 수 있다. 상기 반응식에서 Y는 산화비스무트, 삼산화붕소, 이산화규소, 산화크롬, 이산화망간, 산화철, 산화구리, 산화납을 포함하는 금속산화물 일 수 있다.In the above reaction formula, M may be a metal powder containing aluminum, lithium, potassium, magnesium, titanium, zinc, silicon, boron, etc., and the metal powder may be used alone or in combination, but aluminum has a high boiling point and is cheap It can be used most commonly. In the above reaction formula, Y may be a metal oxide including bismuth oxide, boron trioxide, silicon dioxide, chromium oxide, manganese dioxide, iron oxide, copper oxide, and lead oxide.
상기 복합소이제는 금속 분말(연료)로 알루미늄 분말을 사용할 수 있고, 상기 알루미늄 분말은 20 내지 60 중량% 일 수 있고 구체적으로 30 내지 60 중량 % 일 수 있으며 바람직하게는 30 내지 50 중량%일 수 있다. 또한, 상기 복합소이제는 금속산화물(산화제)로 산화제이철을 사용할 수 있고, 상기 산화제이철은 40 내지 80 중량% 일 수 있고 구체적으로 50 내지 70 중량 %일 수 있으며 바람직하게는 50 내지 70 중량%일 수 있다.The composite plasticizer may use aluminum powder as a metal powder (fuel), and the aluminum powder may be 20 to 60% by weight, specifically 30 to 60% by weight, and preferably 30 to 50% by weight. . In addition, the complex agent may use ferric oxide as the metal oxide (oxidizing agent), and the ferric oxide may be 40 to 80% by weight, specifically 50 to 70% by weight, preferably 50 to 70% by weight. can
본 발명에 있어서, 상기 복합소이제는 촉매 또는 가스 발생제인 황; 불꽃 유발제인 질산바륨; 첨가제(형태 고정제)인 니트로셀룰로오스, 아세트셀룰로오스, 황 및 아연; 및 충전물질인 수소화리튬, 지르코늄 및 산화철;을 추가할 수 있으나 이로 한정되는 것은 아니다.In the present invention, the complex incinerator is a catalyst or a gas generating agent sulfur; barium nitrate, which is a pyrotechnic agent; nitrocellulose, acetcellulose, sulfur and zinc as additives (shape fixing agents); and lithium hydride, zirconium and iron oxide, which are filling materials; but may be added, but is not limited thereto.
또한, 상기 첨가제는 목표물에 충돌 직후 점화되어야 할 온도에 따라 달라질 수 있고, 낮은 온도에서 점화되어야 하는 경우 가장 낮은 자연점화온도를 갖는 니트로셀룰로오스를 이용할 수 있으며, 중간 온도에서 점화되어야 하는 경우 비활성의 형태고정제인 아세트셀룰로오스에 황 및 아연을 혼합하여 이용할 수 있고, 높은 온도에서 또는 쉽게 점화되지 않아야 하는 경우 아세트셀룰로오스를 이용할 수 있다. 첨가제가 비활성(비에너지물질)일 경우, 테르밋 반응이 일어나는 자체 온도 1200℃의 온도가 필요할 수 있으므로 사용 용도, 주변 상황, 거리 및 환경 등을 고려하여 탄의 점화온도 조절을 위해 상황에 맞는 첨가제의 종류 및 조성을 조절하여 복합소이제를 제조할 수 있다.In addition, the additive may vary depending on the temperature to be ignited immediately after impacting the target, and when it is to be ignited at a low temperature, nitrocellulose having the lowest natural ignition temperature can be used, and when it is to be ignited at an intermediate temperature, it is in an inactive form Sulfur and zinc can be mixed with acetcellulose as a fixing agent, and acetcellulose can be used at high temperatures or when not easily ignited. If the additive is inactive (non-energy material), it may need a temperature of 1200°C for thermite reaction itself. By controlling the type and composition, it is possible to manufacture a complex incinerator.
본 발명에 있어서, 상기 2개의 금속판은 내측으로 기울기가 상이한 금속판을 이용할 수 있고, 상기 금속판은 각각 앞부분 금속판 및 뒷부분 금속판으로 구분할 수 있다. 상기 앞부분 금속판은 내측 5 내지 20도의 기울기를 가진 오목한 금속판 일 수 있고, 구체적으로는 내측으로 10 내지 15도의 기울기를 가진 오목한 금속판일 수 있다. 또한, 상기 뒷부분 금속판은 20 내지 40도의 기울기를 가진 오목한 금속판 일 수 있고, 구체적으로는 20 내지 30도의 기울기를 가진 오목한 금속판 일 수 있다. 또한, 상기 앞부분 금속판 및 뒷부분 금속판은 두께가 5 내지 10 mm의 금속판 일 수 있고, 지름이 150 내지 200 mm의 금속판 일 수 있으나 이로 한정되는 것은 아니다.In the present invention, the two metal plates may use a metal plate having a different inclination inward, and the metal plate may be divided into a front metal plate and a rear metal plate, respectively. The front metal plate may be a concave metal plate having an inclination of 5 to 20 degrees inside, and specifically, a concave metal plate having an inclination of 10 to 15 degrees inward. In addition, the rear metal plate may be a concave metal plate having an inclination of 20 to 40 degrees, specifically, a concave metal plate having an inclination of 20 to 30 degrees. In addition, the front metal plate and the rear metal plate may be a metal plate having a thickness of 5 to 10 mm, and may be a metal plate having a diameter of 150 to 200 mm, but is not limited thereto.
상기 기울기가 상이한 금속판을 겹쳐서 생긴 사이 공간에 상기 복합소이제를 충전하여 2개의 금속판 안에 복합소이제가 포함된 폭발형성탄두로 이용할 수 있다.By filling the space between the metal plates having different inclinations and overlapping the metal plates, the composite incinerator can be used as an explosive-forming warhead containing the composite incinerator in the two metal plates.
본 발명에 있어서, 상기 2개의 금속판은 강도 및 녹는점이 상이한 금속판을 이용할 수 있고, 앞부분 금속판은 뒷부분 금속판보다 경도가 낮은 금속을 이용할 수 있으며, 뒷부분 금속판은 발사체의 반응물의 폭발에너지를 견딜 수 있는, 앞부분 금속판보다 경도 및 녹는점이 높은 금속을 이용할 수 있다. 상기 앞부분 금속판은 납, 구리 및 알루미늄으로 구성된 군에서 하나를 선택할 수 있고, 상기 뒷부분 금속판은 구리 및 철로 구성된 군에서 하나를 선택할 수 있다. 또한, 상기 앞부분-뒷부분 금속판은 납-구리(Pb-Cu), 구리-철(Cu-Fe), 알루미늄-철(Al-Fe), 및 납-철(Pb-Fe)으로 구성된 군에서 하나의 조합을 선택할 수 있고, 바람직하게는 납-구리의 조합을 선택할 수 있다. 또한, 상기 구리는 구리-아연 합금일 수 있고, 상기 철은 일정 비율 이상의 탄소가 포함된 탄소강일 수 있다.In the present invention, the two metal plates may use a metal plate with different strength and melting point, the front metal plate may use a lower hardness than the rear metal plate, and the rear metal plate can withstand the explosive energy of the reactant of the projectile, A metal having a higher hardness and melting point than the front metal plate can be used. One of the front metal plates may be selected from the group consisting of lead, copper and aluminum, and one of the rear metal plates may be selected from the group consisting of copper and iron. In addition, the front-rear metal plate is one of lead-copper (Pb-Cu), copper-iron (Cu-Fe), aluminum-iron (Al-Fe), and lead-iron (Pb-Fe). A combination can be selected, preferably a combination of lead-copper can be selected. In addition, the copper may be a copper-zinc alloy, and the iron may be carbon steel containing carbon in a certain ratio or more.
본 발명에 있어서, 상기 앞부분 금속판은 폭발사출 충격으로 복합소이제가 점화하여 반응이 시작되고, 상기 반응에 의한 열과 충격에 의해 변형되어 관통자 전면부로 형성될 수 있다.In the present invention, the metal plate of the front part may be ignited by an explosive injection impact to initiate a reaction, and may be deformed by the heat and impact caused by the reaction to form a penetrator front part.
본 발명에 있어서, 상기 변형되어 관통자 전면부로 형성될 수 있는 앞부분 금속판의 관통효과를 증진시키기 위해 폭발에너지가 모이는 중심축 부분에 텅스텐, 이리듐 및 이의 중합금을 부착할 수 있고, 구체적으로 텅스텐-구리(W-Cu)계, 텅스텐-주석(W-Sn)계, 텅스텐-아연(W-Zn)계, 텅스텐-철(W-Fe)계, 텅스텐-이리듐(W-Ir)계, 텅스텐-니켈(W-Ni)계, 텅스텐-구리-아연(W-Cu-Zn)계, 텅스텐-철-니켈(W-Fe-Ni)계의 중합금을 부착할 수 있으며, 바람직하게는 텅스텐-이리듐(W-Ir)계의 중합금을 부착할 수 있다. 또한, 상기 앞부분 금속판에 부착되는 중합금은 원뿔형 및 원뿔의 면이 기준 수평면에서 구부러진 원뿔형 모양의 중합금일 수 있다.In the present invention, tungsten, iridium, and a polymer thereof may be attached to the central axis where explosive energy is collected in order to enhance the penetrating effect of the front metal plate that is deformed and formed into the front part of the penetrator, specifically tungsten-copper (W-Cu), tungsten-tin (W-Sn), tungsten-zinc (W-Zn), tungsten-iron (W-Fe), tungsten-iridium (W-Ir), tungsten-nickel (W-Ni)-based, tungsten-copper-zinc (W-Cu-Zn)-based, tungsten-iron-nickel (W-Fe-Ni)-based polymer alloy can be attached, preferably tungsten-iridium ( W-Ir)-based polymer alloy can be attached. In addition, the polymer gold attached to the front part of the metal plate may be a conical shape and a cone-shaped polymer gold in which a surface of the cone is bent from a reference horizontal plane.
본 발명에 있어서, 상기 2개의 금속판은 폭발사출 직후 폭발과 동시에 판의 가장자리가 폭압으로 자연 용접될 수 있고, 상기 자연 용접으로 견고한 소이성 관통자가 형성될 수 있다. 상기 관통자는 약 3000 m/s의 속도로 목표물까지 비행하여 목표물을 타격할 수 있고, 상기 목표물을 1차 파괴 및 2차 파괴할 수 있다.In the present invention, the edges of the two metal plates can be naturally welded by blast pressure immediately after the explosion and simultaneously with the explosion, and a strong incendiary penetrator can be formed by the natural welding. The penetrator may fly to the target at a speed of about 3000 m/s to strike the target, and may primary and secondary destruction of the target.
또한, 본 발명은 발사체의 반응물에 의해 사출되는 목표물에 1차 충돌시 2개의 금속판 안에 포함된 소이성 물질에 의한 2차 폭발이 발생하여 목표물을 파괴하는 고폭소이능을 갖는 폭발형성탄두를 포함하는 관통자의 제조방법을 제공한다.In addition, the present invention includes an explosive-forming warhead having high explosive incendiary ability to destroy the target by generating a secondary explosion by incendiary materials contained in two metal plates upon the first collision with the target injected by the reactant of the projectile. A method for manufacturing a penetrator is provided.
상기 폭발형성탄두를 포함하는 관통자의 제조방법은 하기의 단계들을 포함하는 방법에 의해 제조된다.The method for manufacturing a penetrator including the explosive-forming warhead is manufactured by a method including the following steps.
(a) 복합소이제를 제조하는 단계;(a) preparing a complex incinerator;
(b) 녹는점 및 강도가 서로 다른 2개의 금속판을 다른 각도로 오목하게 만들고 겹쳐서 만든 렌즈 사이에 상기 단계 (a)에서 제조한 복합소이제를 충전하여 폭발형성탄두를 제조하는 단계; 및(b) manufacturing an explosive warhead by filling the composite incinerator prepared in step (a) between the lenses made by concave and overlapping two metal plates having different melting points and strengths at different angles; and
(c) 상기 단계 (b)의 복합소이제가 충전된 폭발형성탄두를 발사체에 앞부분에 부착하는 단계;(c) attaching the explosive-forming warhead filled with the complex incendiary agent of step (b) to the front part of the projectile;
상기 (a) 단계의 복합소이제 및 (b) 단계의 2개의 금속판, 겹쳐진 2개의 금속판에 충전되는 복합소이제, 2개의 금속판에 복합소이제를 충전하여 만든 폭발형성탄두는 고폭소이능을 갖는 폭발형성탄두를 포함하는 관통자에서 설명과 동일한 바, 구체적인 설명은 상기 내용을 원용한다.The composite incendiary agent of step (a) and the two metal plates of step (b), the composite incendiary agent charged in the two overlapping metal plates, and the composite incendiary agent in the two metal plates are filled with the explosive-forming warhead made with high explosive capability. It is the same as the description for the penetrator including the explosive-forming warhead, and the detailed description refers to the above.
상기 단계 (c)의 발사체는 폭발성 반응물을 가지고 있고, 상기 폭발성 반응물에 의해 고폭소이능을 갖는 폭발형성탄두가 사출될 수 있다. 상기 폭발성 반응물은 고성능 폭약인 ANQ nitrate(1-Amino-3-nitroguanidine nitrate), HMX(1,3,5,7-tetranitro-1,3,5,7-tetrazocane), RDX(1,3,5-Trinitro-1,3,5-triazinane), HNIW(Hexanitrohexa-azaisowurtzitane) 및 PETN(Pentaerythritol tetranitrate)으로 구성된 군에서 선택되는 하나 이상의 폭약일 수 있다.The projectile of step (c) has an explosive reactant, and an explosive-forming warhead having a high explosive ability can be ejected by the explosive reactant. The explosive reactants are high explosives ANQ nitrate (1-Amino-3-nitroguanidine nitrate), HMX (1,3,5,7-tetranitro-1,3,5,7-tetrazocane), RDX (1,3,5) -Trinitro-1,3,5-triazinane), HNIW (Hexanitrohexa-azaisowurtzitane), and PETN (Pentaerythritol tetranitrate) may be one or more explosives selected from the group consisting of.
또한, 상기 사출시 폭압으로 앞부분-뒷부분 금속판 렌즈의 가장자리가 자연 용접 및 일체화가 진행될 수 있다.In addition, natural welding and integration of the edges of the front-rear metal plate lens may be performed due to blast pressure during the injection.
상기 발사체의 반응물과 상기 반응물의 폭발에너지를 견딜 수 있는 상기 폭발형성탄두의 밀도가 크고 녹는점 및 경도가 높은 뒷부분 금속판이 접촉될 수 있다. The reactant of the projectile and the rear metal plate having a high melting point and high hardness of the explosive-forming warhead capable of withstanding the explosive energy of the reactant may be in contact.
또한, 본 발명은 상기 고폭소이능을 갖는 폭발형성탄두를 포함하는 관통자의 제조방법으로 제조된 고폭소이능을 갖는 폭발형성탄두를 포함하는 관통자를 제공한다.In addition, the present invention provides a penetrator including an explosion-forming warhead having a high-explosive incendiary capability manufactured by the method for manufacturing a penetrator including an explosive-forming warhead having a high explosive incendiary capability.
본 발명의 고폭소이능을 갖는 폭발형성탄두는 소이성 물질을 안정적으로 포함하는 탄두이고, 발사체에 의해 폭발사출되면서 관통자로 변형되는 고폭소이능을 갖는 폭발형성 탄두를 포함하는 관통자로, 상기 관통자는 목표물에 충돌하여 앞부분은 저항에 속도가 감소하지만 뒷부분은 관성에 의해 같은 속도로 전진하여 내부의 복합소이제가 목표물로 침두할 수 있다. 저항으로 속도가 줄고 좁혀진 관통자 앞부분과 동일한 속도로 전진하는 관통자 뒷부분에 의해 내부에 침투했을 때 최고의 압력을 받아 목표물을 내부에서 파괴할 수 있다. 또한, 내부에 관통되어 침투한 상태에서 2차 폭발이 일어나는 경우, 가스생성 및 열팽창폭발을 일으킬 수 있다.The explosive-forming warhead having a high explosive incendiary capability of the present invention is a warhead stably containing an incendiary material, and is a penetrator including an explosive-forming warhead having a high explosive incendiary capability that is transformed into a penetrator while being exploded and ejected by a projectile, wherein the penetrator is When it collides with a target, the speed of the front part decreases due to resistance, but the rear part advances at the same speed due to inertia, so the internal compound incinerator can sink into the target. The target can be destroyed from the inside under maximum pressure when penetrating inside by the rear part of the penetrator, which is slowed by resistance and advanced at the same speed as the front part of the narrowed penetrator. In addition, when a secondary explosion occurs while penetrating through the interior, it may cause gas generation and thermal expansion explosion.
또한, 본 발명의 고폭소이능을 갖는 폭발형성탄두는 기존의 이중탄두(Tandem)과 달리 1차 파괴용 탄두로 또다른 성형작약탄이나 고폭탄과 같은 폭발탄을 사용하지 않아 탄두 진행방향의 반대방향으로 오는 저항이 발생하지 않는다.In addition, the explosive-forming warhead having a high explosive incendiary capability of the present invention does not use explosive ammunition such as another shaped charge or high explosive as a primary destructive warhead unlike the existing double warhead (Tandem), so the direction opposite to the direction of the warhead resistance does not occur.
또한, 본 발명의 고폭소이능을 갖는 폭발형성탄두는 1차 파괴 후 탄두 내부의 복합소이제가 2차 목표물과 직접 반응하여 에너지가 발생하거나, 공간으로 들어올 때 내부의 공기와 고속으로 마찰하여 고폭소이 효과가 발생하여 탱크나 벙커 등의 구조물을 2차 파괴할 수 있다. 또한, 1차 파괴 후에 남아있는 관통자의 후면 구조가 목표물이 파괴된 부분을 통과하여 2차 목표물을 타격할 수 있다.In addition, the explosive-forming warhead having the high-explosive incendiary ability of the present invention generates energy by directly reacting with the secondary target after the primary destruction by the complex incendiary agent inside the warhead, or when it enters the space, friction with the internal air at high speed to create a high-explosive incendiary. The effect can occur and secondary destruction of structures such as tanks and bunkers is possible. In addition, the rear structure of the penetrator remaining after the primary destruction may pass through the portion where the target is destroyed to hit the secondary target.
본 발명의 고폭소이능을 갖는 폭발형성탄두를 포함하는 관통자는 군사적 목적으로 벙커 관통용 및 대전차 미사일 등의 탄두에 사용될 수 있고, 산업적 목적으로 일반 건축물 폭파해체, 기존의 폭약으로는 해체가 까다롭고 곤란한 돌 및 흙 등이 포함된 산이나 땅에서 사용될 수 있으며, 단순히 건축물에만 제한되지 않고 직접파괴나 2차 파괴가 가능한 모든 물체에 사용할 수 있다.The penetrator including the explosive-forming warhead with high explosive incendiary ability of the present invention can be used for warheads such as bunker penetration and anti-tank missiles for military purposes, and for industrial purposes, it is difficult to dismantle general buildings and dismantle them with conventional explosives. It can be used in mountains or land containing difficult stones and soil, and it is not limited to simple buildings and can be used for all objects that can be destroyed directly or secondary destruction.
이하 본 발명의 실시예를 통해 보다 상세히 설명한다. 다만 하기 실시예는 본 발명의 이해를 돕기 위한 것이지 본 발명의 권리범위를 이로 한정하는 것을 의도하지 않는다.Hereinafter, an embodiment of the present invention will be described in more detail. However, the following examples are provided to help the understanding of the present invention and are not intended to limit the scope of the present invention.
<실시예 1> 고폭소이능을 갖는 폭발형성탄두를 포함하는 관통자 제조<Example 1> Manufacture of a penetrator comprising an explosive-forming warhead having a high explosive incendiary capability
<1-1> 복합소이제 제조<1-1> Manufacture of complex incinerator
알루미늄(Al) 및 산화제이철(Fe2O3)을 이용하여 복합소이제를 제조하였다.A composite plasticizer was prepared using aluminum (Al) and ferric oxide (Fe 2 O 3 ).
구체적으로 알루미늄 분말 400 g 및 산화제이철 600 g 을 혼합한 후, 촉매 및 가스 발생제인 황 15 g, 불꽃 유발제인 질산바륨 7 g, 형태고정제인 아세트셀룰로오스 3 g 및 충전물질인 지르코늄 3 g 을 첨가하여 복합소이제를 제조하였다.Specifically, after mixing 400 g of aluminum powder and 600 g of ferric oxide, 15 g of sulfur as a catalyst and gas generator, 7 g of barium nitrate as a flame inducer, 3 g of acetcellulose as a shape fixing agent, and 3 g of zirconium as a filling material were added. A complex incinerator was prepared.
본원의 발명은 민감성, 충격감도, 온도감도와 연관되어 있으므로 목적에 따라 구성성분을 조절한다.Since the present invention is related to sensitivity, impact sensitivity, and temperature sensitivity, the components are adjusted according to the purpose.
<1-2> 폭발형성탄두용 금속판 제조<1-2> Manufacture of metal plate for explosive warhead
앞부분은 납(Pb) 금속판을 이용하고 뒷부분은 구리(Cu) 금속판을 이용하여 폭발형성탄두를 제조하였다.A lead (Pb) metal plate was used for the front part and a copper (Cu) metal plate was used for the rear part to manufacture an explosive-forming warhead.
구체적으로 수평선을 기준으로 내측 30도의 기울기를 가진, 두께 5 mm 및 지름 200 mm인 원형의 납 앞부분 금속판 및 수평선을 기준으로 내측 10도의 기울기를 가진, 두께 5 mm 및 지름 200 mm인 원형의 구리 뒷부분 금속판을 제작하여 겹쳐 생긴 사이 공간에 상기 실시예 <1-1>에서 제조한 복합소이제를 충전하였다.Specifically, a circular lead metal plate 5 mm thick and 200 mm in diameter with an inclination of 30 degrees on the inside with respect to the horizontal line and a circular copper back part with a thickness of 5 mm and a diameter of 200 mm with an inclination of 10 degrees on the inside with respect to the horizontal line The composite plasticizer prepared in Example <1-1> was filled in the space between the metal plates and the overlapping space.
상기 겹쳐진 2개의 금속판 가장자리는 발사 후 자동으로 용접되므로 용접하지 않았다.The edges of the two overlapping metal plates were not welded because they were automatically welded after firing.
<1-3> 복합소이제가 충전된 관통자 제조<1-3> Manufacture of a penetrator filled with a compound incinerator
ANQ nitrate(1-Amino-3-nitroguanidine nitrate) 폭약이 들어있는, 니트로셀룰로오스가 케이스로 되어있는 발사체 앞부분에 상기 실시예 <1-2>에서 제조한 폭발형성탄두의 Cu 금속판(뒷부분)과 상기 반응성 물질이 접촉하도록 부착하여 복합소이제가 충전된 관통자를 제조하였다.ANQ nitrate (1-Amino-3-nitroguanidine nitrate) Cu metal plate (rear part) of the explosive-forming warhead prepared in Example <1-2> on the front part of the projectile containing the nitrocellulose case and the reactivity By attaching the materials to contact, a penetrator filled with a composite plasticizer was prepared.
Claims (12)
고폭소이능을 갖는 폭발형성탄두를 포함하는 관통자.
In the case of the first collision with the target during the explosive injection by the projectile, the second explosion occurs by the incendiary material contained in the two metal plates, destroying the target and stably containing the incendiary material,
A penetrator comprising an explosive-forming warhead with high explosive incendiary capability.
상기 2차 폭발은 1차 충돌시 내부 관성에 의해 압력을 받아 금속판 안에 포함된 소이성 물질의 열에너지로 발생하는, 관통자.
The method of claim 1,
The second explosion is a penetrator, which is generated by thermal energy of the incendiary material contained in the metal plate under pressure by internal inertia during the first collision.
상기 소이성 물질은 알루미늄, 리튬, 칼륨, 마그네슘, 타이타늄, 아연, 규소, 붕소 및 이의 수소화합물로 구성된 군에서 선택되는 하나 이상의 분말 및 산화비스무트, 삼산화붕소, 이산화규소, 산화크롬, 이산화망간, 산화철, 산화구리 및 산화납으로 구성된 군에서 선택되는 하나 이상의 금속산화물을 혼합한 것이고,
이들은 테르밋 반응을 일으키는 복합소이제인, 관통자.
The method of claim 1,
The incendiary material is at least one powder selected from the group consisting of aluminum, lithium, potassium, magnesium, titanium, zinc, silicon, boron and hydrogen compounds thereof, and bismuth oxide, boron trioxide, silicon dioxide, chromium oxide, manganese dioxide, iron oxide, It is a mixture of one or more metal oxides selected from the group consisting of copper oxide and lead oxide,
These are complex agents that cause thermite reaction, penetrators.
상기 소이성 물질은 알루미늄 분말은 20 내지 60 중량%이고 산화제이철은 40 내지 80 중량%를 포함하는 복합소이제인, 관통자.
The method of claim 1,
The penetrator, wherein the inflammable material is a composite incinerator comprising 20 to 60% by weight of aluminum powder and 40 to 80% by weight of ferric oxide.
상기 복합소이제는 황, 질산바륨, 니트로셀룰로오스, 아세트셀룰로오스, 황, 아연, 수소화리튬, 지르코늄 및 산화철로 구성된 군에서 선택되는 하나 이상이 추가될 수 있는, 관통자.
4. The method of claim 3,
The complex agent may be added at least one selected from the group consisting of sulfur, barium nitrate, nitrocellulose, acetcellulose, sulfur, zinc, lithium hydride, zirconium and iron oxide, penetrators.
상기 2개의 금속판은 두께가 5 내지 10 mm 및 지름이 150 내지 200 mm인,
강도, 녹는점 및 내측으로 기울기가 상이한 앞부분 금속판-뒷부분 금속판으로 구성되는, 관통자.
The method of claim 1,
The two metal plates have a thickness of 5 to 10 mm and a diameter of 150 to 200 mm,
A penetrator, consisting of a front metal plate-back metal plate with different strength, melting point and inward inclination.
상기 2개의 금속판에서 앞부분 금속판은 내측 5 내지 20도의 기울기를 가지고 뒷부분 금속판은 내측 20 내지 40도의 기울기를 가진 오목한 금속판인 관통자.
7. The method of claim 6,
In the two metal plates, the front metal plate has an inner inclination of 5 to 20 degrees, and the rear metal plate is a concave metal plate having an inner inclination of 20 to 40 degrees.
상기 2개의 금속판에서 뒷부분 금속판은 앞부분 금속판보다 강도가 강하고 녹는점이 높은 금속으로 되어있는, 관통자.
7. The method of claim 6,
In the two metal plates, the rear metal plate is made of a metal having a higher strength and a higher melting point than the front metal plate.
상기 2개의 금속판은 앞부분 금속판-뒷부분 금속판의 조합은 납-구리(Pb-Cu), 구리-철(Cu-Fe), 알루미늄-철(Al-Fe), 및 납-철(Pb-Fe)로 구성된 군에서 선택되는 하나의 조합인, 관통자
7. The method of claim 6,
The combination of the front metal plate and the rear metal plate is lead-copper (Pb-Cu), copper-iron (Cu-Fe), aluminum-iron (Al-Fe), and lead-iron (Pb-Fe). One combination selected from the group consisting of a penetrator
상기 앞부분 금속판은 폭발사출시 열과 충격에 의해 변형되어 관통자 전면부로 형성되는, 관통자.
7. The method of claim 6,
The front metal plate is deformed by heat and impact during explosion injection and is formed as a penetrator front part.
상기 변형되는 앞부분 금속판의 중심축에 텅스텐-구리(W-Cu)계, 텅스텐-주석(W-Sn)계, 텅스텐-아연(W-Zn)계, 텅스텐-철(W-Fe)계, 텅스텐-이리듐(W-Ir)계, 텅스텐-니켈(W-Ni)계, 텅스텐-구리-아연(W-Cu-Zn)계, 텅스텐-철-니켈(W-Fe-Ni)계 원뿔형 또는 구불어진 원뿔형 모양의 중합금을 부착하는, 관통자.
11. The method of claim 10,
Tungsten-copper (W-Cu)-based, tungsten-tin (W-Sn)-based, tungsten-zinc (W-Zn)-based, tungsten-iron (W-Fe)-based, tungsten on the central axis of the deformed front metal plate -Iridium (W-Ir), tungsten-nickel (W-Ni), tungsten-copper-zinc (W-Cu-Zn), tungsten-iron-nickel (W-Fe-Ni) conical or curved A penetrator that attaches a cone-shaped polymer alloy.
2개의 금속판은 폭발사출시 가장자리가 폭압으로 자연 용접되는, 관통자.
The method of claim 1,
The two metal plates are a penetrator, whose edges are naturally welded by blast pressure during explosion injection.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR1020200091881A KR102696509B1 (en) | 2020-07-23 | 2020-07-23 | Penetrator with explosive warhead having high explosive ability |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR1020200091881A KR102696509B1 (en) | 2020-07-23 | 2020-07-23 | Penetrator with explosive warhead having high explosive ability |
Publications (2)
Publication Number | Publication Date |
---|---|
KR20220012725A true KR20220012725A (en) | 2022-02-04 |
KR102696509B1 KR102696509B1 (en) | 2024-08-20 |
Family
ID=80267810
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
KR1020200091881A KR102696509B1 (en) | 2020-07-23 | 2020-07-23 | Penetrator with explosive warhead having high explosive ability |
Country Status (1)
Country | Link |
---|---|
KR (1) | KR102696509B1 (en) |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0156090A2 (en) * | 1983-09-28 | 1985-10-02 | State of Israel Ministry of Defence Raphael Armament Development Authority | Liners for shaped-charge warhead and method of making same |
JP2008121953A (en) * | 2006-11-10 | 2008-05-29 | Daikin Ind Ltd | Molded explosive charge warhead and liner |
JP2011085319A (en) * | 2009-10-15 | 2011-04-28 | Daikin Industries Ltd | Ammunition |
KR101346238B1 (en) * | 2012-10-19 | 2014-01-03 | 국방과학연구소 | Method for manufacturing graded porous multiple layered reactive shaped charge liner by using kinetic spray coating, and graded porous multiple layered reactive shaped charge liner manufactured by the same |
US20150233688A1 (en) * | 2012-07-17 | 2015-08-20 | Orbital Atk, Inc. | Methods of forming fragmentation bodies, warheads, and ordnance |
KR101823819B1 (en) | 2017-03-31 | 2018-01-30 | 국방과학연구소 | The liner for penetrator with dual performance for multi-functional warhead |
KR101924966B1 (en) | 2017-09-25 | 2018-12-04 | 주식회사 한화 | Pellet forming apparatus for explosively formed projectile and manufacturing method of explosively formed projectile and explosively formed projectile |
-
2020
- 2020-07-23 KR KR1020200091881A patent/KR102696509B1/en active IP Right Grant
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0156090A2 (en) * | 1983-09-28 | 1985-10-02 | State of Israel Ministry of Defence Raphael Armament Development Authority | Liners for shaped-charge warhead and method of making same |
JP2008121953A (en) * | 2006-11-10 | 2008-05-29 | Daikin Ind Ltd | Molded explosive charge warhead and liner |
JP2011085319A (en) * | 2009-10-15 | 2011-04-28 | Daikin Industries Ltd | Ammunition |
US20150233688A1 (en) * | 2012-07-17 | 2015-08-20 | Orbital Atk, Inc. | Methods of forming fragmentation bodies, warheads, and ordnance |
KR101346238B1 (en) * | 2012-10-19 | 2014-01-03 | 국방과학연구소 | Method for manufacturing graded porous multiple layered reactive shaped charge liner by using kinetic spray coating, and graded porous multiple layered reactive shaped charge liner manufactured by the same |
KR101823819B1 (en) | 2017-03-31 | 2018-01-30 | 국방과학연구소 | The liner for penetrator with dual performance for multi-functional warhead |
KR101924966B1 (en) | 2017-09-25 | 2018-12-04 | 주식회사 한화 | Pellet forming apparatus for explosively formed projectile and manufacturing method of explosively formed projectile and explosively formed projectile |
Also Published As
Publication number | Publication date |
---|---|
KR102696509B1 (en) | 2024-08-20 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US8230789B1 (en) | Method and apparatus for a projectile incorporating a metastable interstitial composite material | |
US9683821B2 (en) | Reactive material enhanced projectiles, devices for generating reactive material enhanced projectiles and related methods | |
US8375859B2 (en) | Shaped explosive charge | |
US8505427B2 (en) | Ordnance neutralization method and device using energetic compounds | |
EP2037208A2 (en) | Metal matrix reactive composite projectiles | |
US20120227609A1 (en) | Initiation systems for explosive devices, scalable output explosive devices including initiation systems, and related methods | |
US8616130B2 (en) | Liners for warheads and warheads having improved liners | |
US6308607B1 (en) | Neutralizing munition | |
US8776689B2 (en) | Energetics train reaction and method of making an intensive munitions detonator | |
JPS6144240B2 (en) | ||
US8434411B2 (en) | Cluster explosively-formed penetrator warheads | |
US6467416B1 (en) | Combined high-blast/anti-armor warheads | |
EA038243B1 (en) | Full metal jacket safety bullet, in particular for multi-purpose applications | |
US4714022A (en) | Warhead with tandem shaped charges | |
CN111919081B (en) | Projectile with pyrotechnical active charge | |
US4711177A (en) | Auxiliary booster | |
KR102696509B1 (en) | Penetrator with explosive warhead having high explosive ability | |
US9982979B2 (en) | Device and method for controlled fragmentation by means of temperature-activatable notch charges | |
US11293730B1 (en) | Bullet projectile with enhanced mechanical shock wave delivery for warfare | |
RU2655338C1 (en) | Cartridge with armor-piercing incendiary bullet | |
US5196646A (en) | Dual purpose fuze | |
RU2206862C1 (en) | Concrete-piercing ammunition | |
UA113654C2 (en) | METHOD OF HYPERSONAL PROTECTION OF TANK GALCHENKO AND MODULE OF ACTIVE PROTECTION COMPLEX | |
KR20140040959A (en) | Projectile generated fragments | |
KR102627761B1 (en) | Non-initiating tandem warhead with precursor forming powder jet against explosive reactive armor |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
A201 | Request for examination | ||
E902 | Notification of reason for refusal | ||
E701 | Decision to grant or registration of patent right | ||
GRNT | Written decision to grant |