JPH0321840B2 - - Google Patents
Info
- Publication number
- JPH0321840B2 JPH0321840B2 JP57068552A JP6855282A JPH0321840B2 JP H0321840 B2 JPH0321840 B2 JP H0321840B2 JP 57068552 A JP57068552 A JP 57068552A JP 6855282 A JP6855282 A JP 6855282A JP H0321840 B2 JPH0321840 B2 JP H0321840B2
- Authority
- JP
- Japan
- Prior art keywords
- projectile
- explosive
- jacket
- tantalum
- metal
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 239000002360 explosive Substances 0.000 claims abstract description 64
- 229910052751 metal Inorganic materials 0.000 claims abstract description 15
- 239000002184 metal Substances 0.000 claims abstract description 15
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 claims abstract description 6
- 229910001080 W alloy Inorganic materials 0.000 claims abstract description 5
- 230000005484 gravity Effects 0.000 claims abstract description 5
- 229910052715 tantalum Inorganic materials 0.000 claims abstract description 5
- XGZGDYQRJKMWNM-UHFFFAOYSA-N tantalum tungsten Chemical compound [Ta][W][Ta] XGZGDYQRJKMWNM-UHFFFAOYSA-N 0.000 claims description 5
- 229910045601 alloy Inorganic materials 0.000 claims description 4
- 239000000956 alloy Substances 0.000 claims description 4
- 239000000203 mixture Substances 0.000 claims description 4
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Chemical compound [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 claims description 4
- 150000001875 compounds Chemical class 0.000 claims description 3
- 229910052770 Uranium Inorganic materials 0.000 claims description 2
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 claims description 2
- 229910052737 gold Inorganic materials 0.000 claims description 2
- 239000010931 gold Substances 0.000 claims description 2
- 229910052735 hafnium Inorganic materials 0.000 claims description 2
- VBJZVLUMGGDVMO-UHFFFAOYSA-N hafnium atom Chemical group [Hf] VBJZVLUMGGDVMO-UHFFFAOYSA-N 0.000 claims description 2
- 229910052741 iridium Inorganic materials 0.000 claims description 2
- GKOZUEZYRPOHIO-UHFFFAOYSA-N iridium atom Chemical compound [Ir] GKOZUEZYRPOHIO-UHFFFAOYSA-N 0.000 claims description 2
- 229910052762 osmium Inorganic materials 0.000 claims description 2
- SYQBFIAQOQZEGI-UHFFFAOYSA-N osmium atom Chemical compound [Os] SYQBFIAQOQZEGI-UHFFFAOYSA-N 0.000 claims description 2
- 229910052697 platinum Inorganic materials 0.000 claims description 2
- 229910052702 rhenium Inorganic materials 0.000 claims description 2
- WUAPFZMCVAUBPE-UHFFFAOYSA-N rhenium atom Chemical compound [Re] WUAPFZMCVAUBPE-UHFFFAOYSA-N 0.000 claims description 2
- DNYWZCXLKNTFFI-UHFFFAOYSA-N uranium Chemical compound [U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U] DNYWZCXLKNTFFI-UHFFFAOYSA-N 0.000 claims description 2
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 claims 1
- 229910052721 tungsten Inorganic materials 0.000 claims 1
- 239000010937 tungsten Substances 0.000 claims 1
- 229910001362 Ta alloys Inorganic materials 0.000 abstract 1
- 239000011133 lead Substances 0.000 description 13
- 229910000831 Steel Inorganic materials 0.000 description 9
- 239000010959 steel Substances 0.000 description 9
- 239000000463 material Substances 0.000 description 6
- 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 5
- 239000000026 Pentaerythritol tetranitrate Substances 0.000 description 5
- 229960004321 pentaerithrityl tetranitrate Drugs 0.000 description 5
- 238000004880 explosion Methods 0.000 description 4
- 150000001540 azides Chemical class 0.000 description 3
- 230000000149 penetrating effect Effects 0.000 description 3
- 239000000843 powder Substances 0.000 description 3
- 230000000981 bystander Effects 0.000 description 2
- 238000010304 firing Methods 0.000 description 2
- 230000035515 penetration Effects 0.000 description 2
- 238000009527 percussion Methods 0.000 description 2
- 239000003380 propellant Substances 0.000 description 2
- 239000011347 resin Substances 0.000 description 2
- 229920005989 resin Polymers 0.000 description 2
- 230000000087 stabilizing effect Effects 0.000 description 2
- 229910000851 Alloy steel Inorganic materials 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- USXDFAGDIOXNML-UHFFFAOYSA-N Fulminate Chemical compound [O-][N+]#[C-] USXDFAGDIOXNML-UHFFFAOYSA-N 0.000 description 1
- SNIOPGDIGTZGOP-UHFFFAOYSA-N Nitroglycerin Chemical compound [O-][N+](=O)OCC(O[N+]([O-])=O)CO[N+]([O-])=O SNIOPGDIGTZGOP-UHFFFAOYSA-N 0.000 description 1
- 208000027418 Wounds and injury Diseases 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 238000005474 detonation Methods 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 229910001385 heavy metal Inorganic materials 0.000 description 1
- 208000014674 injury Diseases 0.000 description 1
- DGMJZELBSFOPHH-KVTDHHQDSA-N mannite hexanitrate Chemical compound [O-][N+](=O)OC[C@@H](O[N+]([O-])=O)[C@@H](O[N+]([O-])=O)[C@H](O[N+]([O-])=O)[C@H](O[N+]([O-])=O)CO[N+]([O-])=O DGMJZELBSFOPHH-KVTDHHQDSA-N 0.000 description 1
- 229960001765 mannitol hexanitrate Drugs 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000007747 plating Methods 0.000 description 1
- 230000037452 priming Effects 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
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
- F42B12/20—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
- F42B12/201—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type characterised by target class
- F42B12/204—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type characterised by target class for attacking structures, e.g. specific buildings or fortifications, ships or vehicles
-
- 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
- F42B12/72—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material
- F42B12/76—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material of the casing
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Drilling And Exploitation, And Mining Machines And Methods (AREA)
- Toys (AREA)
- Powder Metallurgy (AREA)
- Manipulator (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
Abstract
Description
本発明は、爆発性小形兵器投射体、即ち、爆発
性装填物で満たされた投射体に関している。
厳密に言えば、弾丸或はミサイルは、飛行中に
限つて投射体と称されが、本明細書においては、
本発明は「投射体」として説明されている。併
し、「投射体」なる術語は、通常静止中或は飛行
中の弾丸或はミサイルを表わすのに用いられる
故、本明細書においても同様に使用されている。
この種の投射体は、主として、闘争性犯罪、特
に際テロリズムに使用される。その場合、例え
ば、航空機上から1群の無関係な傍観者の中の1
人を標的にする場合がある。該標的を完全に貫通
すれば、傍観者を傷付ける虞れがあり、従つて爆
発性投射体の目的は、標的を完全に貫通するのを
避け、或は少なくとも最少限にする一方、該投射
体によつて該標的内に最大の衝撃を与えることに
ある。
小形兵器の投射体の中に、高爆発物(雷酸水銀
或はアジ化鉛のような、1次爆発物、および4硝
酸5エリスリツト(PETN)、或は6硝酸マニト
ールのような、2次爆発物を含むものとする)を
含ませる目的は、主として、該投射体が標的に及
ぼす衝撃効果を高め、且つ該投射体が、貫通して
周囲に傷害を与えることを阻止するためである。
既知の小兵器投射体は、通常鋼もしくは鍍金用
金属のような比較的軽いが強力な金属より成るジ
ヤケツトと、部分的に爆発物で満たされた比較的
重いコアとから構成される。
従来の爆発性小形兵器投射体のジヤケツトは、
通常鍍金材料で鍍金或は被覆された鋼のような、
耐磨耗性の物質より成り、この場合鋼は、投射体
に燃焼する推進物質の圧力および高温に耐える機
械的強度を与える。前記鍍金物質は、摩耗を低減
するめに設けられる。既知の爆発性小形兵器の投
射体においては、鋼のジヤケツトは通常薄く、従
つて構造的に役立つてはいない。即ち、その作用
は、衝撃時に投射物の形状を保持するというより
は、鉛のコアを封じ込める役目を果たす。重さが
軽い程、貫通しにくくなるという原理から投射体
が標的を貫通しにくくなる。
従来の小形兵器の爆発性投射体においては、爆
発物は通常、鉛の中に明けられた細い中心孔の中
に収容される。爆発物は、例えばアジ化鉛のよう
な、衝撃感知1次起爆剤より成る、一連の起爆
体、或は3つの段を含金、複式起爆剤より構成さ
れる。上記3段の中の第1段は、衝撃感知機構よ
り成り、第2段としては、例えば、雷酸水銀のよ
うな、1次起爆剤が用いられ、そして最後の第3
段としては、(PETN)のような2次的高爆薬が
用いられる。或る種の設計では、高度爆発剤とし
て、多塩基性、3硝酸グリセロール・パイロセル
ローズの起爆剤粉末を使用して居り、これは可燃
性の固体で爆発性があり、且つ燃焼して爆鳴を生
ずるが、爆発用としては左程有効ではない。
第1図はこの種の従来の投射体10を示し、同
投射体10は、その内外に鍍金金属14と16が
張られた、比較的薄い鋼のジヤケツト12より成
つている。上記投射体10には、爆薬の容器とし
て役立つ中心孔20が形成された鉛のコア18が
設けられている。
爆薬3は、種々の方法の何れかによつて装填さ
れればよろしいが、図面を明瞭にするため、1団
の爆発性の粉末22と、市販の小形兵器用打撃雷
管24と、樹脂の蓋26より成るように示されて
いる。
既に説明した通り、ジヤケツトの目的は、兵器
の銃身内の溝と、加速する投射体との間の摩擦に
耐えると共に、燃焼する推進薬剤より生ずる圧力
と高温にも耐えることにある。鉛のコア18は、
該投射体の質量を増大させ、これによつて該投射
体の運動量を増大させる役割をなす。上記雷管2
4は、衝撃を受けたとき、爆薬22を爆発させる
ためのものであるが、投射体が高速度で移動する
ために、爆発が起るときまでには、投射体10
は、或る深さまで標的を打抜いているものと了解
されたい。
図面には、投射体を明瞭にするため拡大して示
されている。0.38カリバー投射体においては、中
心孔20の直径は5mmである。3段爆発柱体を含
む0.38カリバー投射体においては、飛行の最中に
爆発が誘発されることが判明した。爆発が空気中
で起つた場合、その爆発柱体の10−14%が、未発
となる。その理由は従来の爆発性投射体は、その
質量をできるだけ大きくするために、含有爆発物
のためのスペースを犠牲にしているからである。
このため、比較的細い爆発柱が生ずることにな
り、この柱体内では、特に実際使用時において高
速回転する条件の下では爆発性衝撃波面の伝播効
率が低下することになる。
既に述べたことでもあるが、鋼の薄いジヤケツ
ト12は、単に収容の作用をなすもので、発射中
該投射体と銃身内の溝との間に発生する摩擦力に
耐えるに足るだけの機械的強度を持つに過ぎな
い。このジヤケツトは、投射体が標的を貫通する
ときに、投射体の形状を最良に保持するために必
要とされる機械的強度を持たされては居ない。
従つて、上述の投射体10の不利点は、第1
に、或る量の爆薬を収容するのに、鉛の質量の20
%という著しい比率の質量が犠牲となること、第
2に、爆薬柱が細いこと、第3に、ジヤケツトの
耐張力が制限を受け、且つその慣性的特性が不充
分であること、そして、第4にその質量分布が不
充分であるため、安定化の回転エネルギの値が比
較的低くなることである。即ち、上述のような、
従来の小形兵器の爆発性投射体においては、通
常、コアの中の鉛の量によつて表わされるコアの
質量と、爆薬柱の大きさとの間に妥協が存在し、
高い質量と多量の爆薬との両条件、すなわち、高
い質量と大きな爆薬柱を同時に実現することが不
可能であつた。
本発明の目的は、周辺までその質量を再分布さ
せ、従来の投射体よりも高い回転エネルギを与え
て、命中精度を増進させた爆発性小形兵器の投射
体を提供することである。投射体の回転軸から離
れて投射体質量を再分布させることにより、総重
量と形状が同一の既知の高爆発性投射体に比べ
て、該投射体の、飛行中の回転安定力およびその
エネルギが向上する。
本発明の今一つの目的は、爆発に関与しないも
のを減らして、爆発性が増大された、爆発性の小
形兵器投射体を提供することである。本発明の更
に今一つの目的は、該投射体のジヤケツトが、従
来の鉛或は銅或は鋼のジヤケツトよりも、耐張性
および慣性の面で優つている。爆発性の小形兵器
の投射体を提供することにある。
上記目的を達成するために、本発明において
は、爆発性小形兵器投射体の中に、13以上の比
重、即ち13g/cm3以上の密度を有するジヤケツト
が用いられている。この場合ジヤケツト材料は、
約16.6乃至16.9g/cm3の密度を有するタンタルム
或はタンタルム・タングステン合金より成るのが
望ましい。その目的は、総ての従来の爆発性或は
その他の投射体とジヤケツトの質量を等しくする
ためである。
上記外被の金属は、その代換物として、ハフニ
ウム、ウラニウム、レニウム、オスミウム、白
金、イリジウム、金、或は、1次元素の合金或は
混合物の密度が13以上の比重を有することを条件
とする上記諸元素の合金、混合物或は化合物より
選択してもよい。
尚、従来の技術の投射体の場合と同様に、本発
明の投射体には、被覆或は鍍金を施し、或は代換
措置として、外被の1面或は両面に、金属を張り
或は金属を被覆してもよろしい。
次に、図面を参照して、本発明を更に具体的に
説明しよう。
第2図に示すような、本発明の投射体100
は、タンタルム・タングステン合金(TaW)よ
り成るジヤケツト102より作られている。併
し、比重が比較的高いものならば、他の金属でも
差支ない。ジヤケツト102の比重が高い故、内
側の高密度のコアが不要となり、且つ内側の空所
全体に爆薬を填充することができる。図示の3段
式爆薬柱体は、市販の小兵器用打撃雷管104、
アジ化鉛の1次起爆層106、高い2次爆発性の
PETN層108、および樹脂製の封止帽110
より成つている。上記投射体100の最終質量
は、少なくとも、前述の従来の投射体10のそれ
と等価となるように配置される。しかしながら、
重金属ジヤケツト102を設けても、該投射体1
0に比べて質量は軽くなるかもしれない。この場
合、その減つただけの質量は、少なくともより効
果的に分配され、これによつて、投射体10より
一層高いレベルの回転安定エネルギが得られる。
爆発柱は、体積で約250%だけ増大させられる
ことにより、従来では投射体の10乃至14%が無駄
になつていたが、(容易には検出し得ないが)そ
れを1%より著しく下廻る点まで低減されること
ができる。
従来の技術のジヤケツトと比較すれば、上記タ
ンタルム・タングステン合金のジヤケツト102
の、張力および慣性特性は、鋼或は合金鋼の張力
特性に近似すると想定され、且つ鉛のジヤケツト
を約46%上廻る改善された慣性的特性(TaWに
対する16.6g/cm2と、Pbに対する11.4g/cm2を基
準とする密度、従つて16.6/11.4=0.46)が得ら
れる。
更に、上記投射体の質量は、該投射体の回転軸
を離れて、この兵器の孔と接触しているその周囲
付近に再分布され、飛行中、回転安定エネルギー
が質量および形態が同一の従来の小形兵器の爆発
性投射体と等しくなり、更にこれより大きくな
る。この再分布と増大された回転安定化力は、よ
り長い射程において精度を高めるのに役立つ。
上記結果は、2つの長期に亘つて実用された米
国陸軍兵器、即ちUSモデル1911.45ACP(14.9g
の投射体を発射するコルト自動拳銃および、9.7
gの投射体を発射する(30−06)USカリバ30
(MLA2弾)ライフル)が参照される。従来の爆
発性投射体と、本発明の投射体との、計算に基づ
く概略的比較によつて確認することができる。即
ち、次の表を参照されたい。
The present invention relates to explosive small arms projectiles, i.e. projectiles filled with an explosive charge. Strictly speaking, a bullet or missile is called a projectile only when it is in flight, but in this specification,
The invention is described as a "projectile." However, since the term "projectile" is commonly used to describe a stationary or in-flight projectile or missile, it is also used herein. Projectiles of this type are primarily used in combat crimes, especially in terrorism. In that case, for example, one of a group of uninvolved bystanders may
They may target people. Completely penetrating the target could injure bystanders, and therefore the purpose of an explosive projectile is to avoid, or at least minimize, completely penetrating the target while The aim is to deliver the maximum impact into the target. Small arms projectiles contain high explosives (primary explosives, such as mercuric fulminate or lead azide, and secondary explosives, such as pentaerythritol tetranitrate (PETN) or mannitol hexanitrate). The purpose of including the projectile (including explosives) is primarily to increase the impact effect of the projectile on the target and to prevent the projectile from penetrating and causing injury to the surrounding area. Known small arms projectiles usually consist of a jacket made of a relatively light but strong metal, such as steel or galvanized metal, and a relatively heavy core partially filled with explosive material. Conventional explosive small arms projectile jackets are
such as steel that is usually plated or coated with a galvanized material.
It is comprised of a wear-resistant material, in this case steel, which provides the projectile with mechanical strength to withstand the pressures and high temperatures of the burning propellant. The plating material is provided to reduce wear. In known explosive small arms projectiles, the steel jacket is usually thin and therefore of no structural utility. That is, its action serves to contain the lead core rather than retain the shape of the projectile upon impact. Based on the principle that the lighter the weight, the harder it is to penetrate the target, it becomes harder for the projectile to penetrate the target. In conventional small arms explosive projectiles, the explosive charge is typically contained within a narrow central hole drilled into the lead. The explosive may consist of a series of detonators consisting of an impact-sensing primary detonator, such as lead azide, or a three-stage metal-containing, dual detonator. The first of the three stages consists of an impact sensing mechanism, the second stage uses a primary detonator, e.g. mercuric fulmate, and the third stage
A secondary high explosive such as (PETN) is used as a stage. Some designs use a polybasic, glycerol trinitrate pyrocellulose priming powder as a highly explosive agent, which is a flammable solid that is explosive and can burn to create an explosion. However, it is not as effective as the one on the left for explosive purposes. FIG. 1 shows a conventional projectile 10 of this type, which comprises a relatively thin steel jacket 12 with plated metal 14 and 16 clad inside and outside. The projectile 10 is provided with a lead core 18 in which a central hole 20 is formed which serves as a container for the explosive charge. The explosive charge 3 may be loaded in any of a variety of ways, but for clarity of the drawing, a group of explosive powder 22, a commercially available small arms percussion cap 24, and a plastic cap are used. 26. As previously explained, the purpose of the jacket is to withstand the friction between the groove in the barrel of the weapon and the accelerating projectile, as well as the pressure and high temperatures created by the burning propellant. The lead core 18 is
It serves to increase the mass of the projectile, thereby increasing the momentum of the projectile. Detonator 2 above
4 is for detonating the explosive 22 when it receives an impact, but since the projectile moves at high speed, by the time the explosion occurs, the projectile 10
should be understood as punching the target to a certain depth. In the drawings, the projectile is shown enlarged for clarity. In a 0.38 caliber projectile, the diameter of the center hole 20 is 5 mm. It has been found that a .38 caliber projectile containing a three-stage explosive column can be detonated during flight. If the explosion occurs in air, 10-14% of the explosion column will go unexploded. This is because conventional explosive projectiles sacrifice space for the explosive content in order to maximize their mass.
This results in a relatively thin explosive column, which reduces the propagation efficiency of the explosive shock wavefront within this column, especially under the conditions of high speed rotation during actual use. As already mentioned, the thin steel jacket 12 serves merely as a containment and has sufficient mechanical strength to withstand the frictional forces generated between the projectile and the groove in the barrel during firing. It just has strength. This jacket does not have the mechanical strength needed to best retain the shape of the projectile as it passes through the target. Therefore, the disadvantage of the projectile 10 described above is the first
20 of the mass of lead to contain a certain amount of explosives.
secondly, the explosive column is thin; thirdly, the tensile strength of the jacket is limited and its inertial properties are insufficient; 4. Due to the insufficient mass distribution, the value of the stabilizing rotational energy is relatively low. That is, as mentioned above,
In conventional small arms explosive projectiles, there is usually a compromise between the mass of the core, expressed by the amount of lead in the core, and the size of the explosive column;
It was impossible to simultaneously achieve both high mass and large amount of explosives, that is, high mass and large explosive column. It is an object of the present invention to provide a small explosive weapon projectile that redistributes its mass to the periphery and imparts higher rotational energy than conventional projectiles, thereby increasing accuracy. By redistributing the projectile mass away from the projectile's axis of rotation, the rotational stability of the projectile in flight and its energy is reduced compared to known high-explosive projectiles of the same total weight and geometry. will improve. It is another object of the present invention to provide an explosive small arms projectile with increased explosiveness with reduced non-explosive material. A further object of the invention is that the projectile jacket has superior tensile strength and inertia over conventional lead, copper or steel jackets. The purpose is to provide explosive small arms projectiles. To achieve the above object, the present invention uses a jacket having a specific gravity of 13 or more, that is, a density of 13 g/cm 3 or more in an explosive small weapon projectile. In this case, the jacket material is
Preferably, it is comprised of tantalum or a tantalum-tungsten alloy having a density of about 16.6 to 16.9 g/cm 3 . The purpose is to equalize the mass of the jacket with all conventional explosive or other projectiles. The metal of the above-mentioned outer jacket may be substituted with hafnium, uranium, rhenium, osmium, platinum, iridium, gold, or an alloy or mixture of primary elements with a density of 13 or more. It may be selected from alloys, mixtures or compounds of the above elements. It should be noted that, as in the case of prior art projectiles, the projectile of the present invention may be coated or plated, or alternatively, one or both surfaces of the outer cover may be coated with metal. may be coated with metal. Next, the present invention will be explained in more detail with reference to the drawings. A projectile 100 of the present invention as shown in FIG.
The jacket 102 is made of tantalum-tungsten alloy (TaW). However, other metals may be used as long as they have a relatively high specific gravity. The high specific gravity of the jacket 102 eliminates the need for a dense inner core and allows the entire inner cavity to be filled with explosives. The illustrated three-stage explosive column includes a commercially available small arms percussion detonator 104;
Primary detonation layer 106 of lead azide, high secondary explosive
PETN layer 108 and resin sealing cap 110
It consists of The final mass of the projectile 100 is arranged to be at least equivalent to that of the conventional projectile 10 described above. however,
Even if the heavy metal jacket 102 is provided, the projectile 1
The mass may be lighter than 0. In this case, the reduced mass is at least distributed more effectively, resulting in a higher level of rotationally stable energy than the projectile 10. The explosive column is increased in volume by about 250%, reducing the previously wasted 10-14% of the projectile to significantly less than 1% (though not easily detectable). can be reduced to the point where it turns. Compared to prior art jackets, the tantalum-tungsten alloy jacket 102
The tensile and inertial properties of the jacket are assumed to be close to those of steel or alloy steel, and have improved inertial properties of about 46% over lead jackets (16.6 g/cm 2 for TaW and 16.6 g/cm 2 for Pb). A density based on 11.4 g/cm 2 is obtained, thus 16.6/11.4=0.46). Furthermore, the mass of the projectile is redistributed away from the axis of rotation of the projectile and around its periphery in contact with the aperture of the weapon, and during flight the rotational stabilizing energy is transferred to a conventional is equal to and even larger than the explosive projectile of a small arms weapon. This redistribution and increased rotational stabilization forces help increase accuracy at longer ranges. The above results are valid for two long-serving U.S. Army weapons, namely the US Model 1911.45ACP (14.9g
A Colt automatic pistol that fires a projectile of 9.7
Firing a projectile of g (30-06) US Caliba 30
(MLA2 bullet) Rifle) is referenced. This can be seen by a schematic, calculated comparison of a conventional explosive projectile and the projectile of the present invention. That is, please refer to the following table.
【表】【table】
【表】
上表からは、拳銃から発射された従来の非爆発
性の弾丸と、ライフルから発射された従来の非爆
発性の弾丸とが比較され、銃口エネルギで表わし
た、従来の小形兵器の爆発性の投射体が一括的に
示されているが、本発明の爆発性の拳銃弾丸は、
ライフルから発射された場合の、従来の非爆発性
投射体と、大形狩りよう用ライフルから発射され
た従来の非爆発性投射体とが比較され、本発明に
よる爆発性の拳銃弾丸が一括的に示されている。
併し、本発明は、高度の操縦性ある、.45カリバ
手動銃においては、USカリバ、30MLのような
重目的ライフルによつて供与されるものより50%
多い銃口エネルギを供与し、そしてこれは、両者
が、同一の.45カリバ自動拳銃から発射された場
合を比較するとき、これが非爆発性の.45カリバ
ACP投射体のそれの約10倍となることが了解さ
れる。
この場合、銃口エネルギなる用語は、該投射体
が標的に引渡し得る、理論的最大エネルギを表わ
すのに使用されている。非爆発性の投射体が標的
内に抑留され、従つてその全エネルギが標的に移
された場合、標的内で消費されるエネルギ(摩擦
および重力エネルギ損を差引いた)は、該兵器の
銃口における、該投射体のエネルギと略々等しく
なる。該投射体が、該標的を貫通するならば、該
爆発性投射体による貫通の特性に従い、前記投射
体のエネルギより著しく少ない量のエネルギが、
標的に移されることになるが、併し、殆ど何れの
場合にも、前記投射体は、そのエネルギの全部を
標的へ引渡すことになる。
従来の技術における、爆発性投射体10におい
ては、ジヤケツト厚を増大されると、コアの質量
が減少し、投射体の全質量が低下していた。本発
明の投射体100においては、ジヤケツト102
は、所定限界内で、所望の厚さまで厚くすること
ができる。例えば、投射体の貫通能力を増大させ
るという要望がある場合、この要望に応じてジヤ
ケツトの能力的および質量的特性を増大させるこ
とができる。[Table] The table above compares a conventional non-explosive bullet fired from a handgun with a conventional non-explosive bullet fired from a rifle, and shows the difference in muzzle energy of conventional small arms. Although explosive projectiles are collectively shown, the explosive handgun bullets of the present invention are
Comparisons were made of conventional non-explosive projectiles when fired from rifles and conventional non-explosive projectiles fired from large hunting rifles, and the explosive handgun bullets of the present invention were compared. is shown.
However, the present invention has a high degree of maneuverability. 45 Caliva handgun, 50% more than that offered by US Caliva, heavy purpose rifles like the 30ML
They deliver more muzzle energy, and this is because they both deliver the same amount of muzzle energy. 45 Caliba automatic pistol when compared to a non-explosive pistol. 45 kariba
It is understood that it will be about 10 times that of an ACP projectile. In this case, the term muzzle energy is used to describe the theoretical maximum energy that the projectile can deliver to the target. If a non-explosive projectile is contained within a target, so that all of its energy is transferred to the target, the energy dissipated within the target (minus frictional and gravitational energy losses) is equal to the energy at the muzzle of the weapon. , approximately equal to the energy of the projectile. If the projectile penetrates the target, according to the characteristics of penetration by the explosive projectile, an amount of energy significantly less than the energy of the projectile is
However, in almost every case, the projectile will deliver all of its energy to the target. In the prior art explosive projectile 10, as the jacket thickness was increased, the core mass was reduced, and the total mass of the projectile was reduced. In the projectile 100 of the present invention, the jacket 102
can be increased to a desired thickness within predetermined limits. For example, if there is a desire to increase the penetration capability of a projectile, the power and mass characteristics of the jacket can be increased to meet this desire.
第1図は、従来の爆発性投射体の断面図、第2
図は、本発明による爆発性投射体の断面図であ
る。
図において、10:投射体、12:鋼の外被、
14,16:鍍金金属部、18:鉛の心、20:
中心孔、22:粉末爆薬、24:打撃起爆剤、1
00:本発明の投射体、102:外被、104:
打撃起爆剤、106:1次爆薬層、108:2次
PETN層、110:樹脂キヤツプ。
Figure 1 is a sectional view of a conventional explosive projectile; Figure 2 is a cross-sectional view of a conventional explosive projectile;
The figure is a cross-sectional view of an explosive projectile according to the invention. In the figure, 10: projectile, 12: steel jacket,
14, 16: Plated metal part, 18: Lead core, 20:
Center hole, 22: Powder explosive, 24: Impact detonator, 1
00: Projectile of the present invention, 102: Outer cover, 104:
Impact detonator, 106: Primary explosive layer, 108: Secondary
PETN layer, 110: resin cap.
Claims (1)
の中に配置された爆発性装填物とより成る爆発性
小形兵器の投射体。 2 前記ジヤケツトの金属が、主成分としてのタ
ンタルム或はタンタルム・タングステンより成る
特許請求の範囲第1項に記載の投射体。 3 前記金属ジヤケツトの金属が、ハフニウム、
ウラニウム、レニウム、オスミウム、白金、イリ
ジウム或は金、上記の中の任意の一つ或はより多
くのものの合金、混合物或は化合物の中より選択
され、上記合金混合物或は化合物にはタンタルム
或はタングステン或はその両者を含ませ得る、特
許請求の範囲第1項に記載の投射体。 4 前記ジヤケツトの金属がタンタルム或はタン
タルム・タングステン合金であり、而して前記投
射体の質量が、該目的で比較的厚くつくられたジ
ヤケツト中に著しく集中的に配置されている特許
請求の範囲第1項に記載の投射体。[Claims] 1. A small explosive weapon projectile comprising a metal jacket having a specific gravity of 13 or more and an explosive charge disposed therein. 2. The projectile according to claim 1, wherein the metal of the jacket consists of tantalum or tantalum-tungsten as a main component. 3. The metal of the metal jacket is hafnium,
selected from among uranium, rhenium, osmium, platinum, iridium or gold, alloys, mixtures or compounds of any one or more of the above, said alloy mixtures or compounds including tantalum or A projectile as claimed in claim 1, which may contain tungsten or both. 4. The metal of the jacket is tantalum or a tantalum-tungsten alloy, and the mass of the projectile is highly concentrated in a jacket made relatively thick for this purpose. The projectile according to item 1.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| ZA812677 | 1981-04-23 | ||
| ZA81/2677 | 1981-04-23 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5828997A JPS5828997A (en) | 1983-02-21 |
| JPH0321840B2 true JPH0321840B2 (en) | 1991-03-25 |
Family
ID=25575353
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP57068552A Granted JPS5828997A (en) | 1981-04-23 | 1982-04-23 | Projecting body of explosive small-sized arm |
Country Status (5)
| Country | Link |
|---|---|
| EP (1) | EP0063927B1 (en) |
| JP (1) | JPS5828997A (en) |
| AT (1) | ATE16850T1 (en) |
| CA (1) | CA1207186A (en) |
| DE (1) | DE3267756D1 (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4940404A (en) * | 1989-04-13 | 1990-07-10 | Westinghouse Electric Corp. | Method of making a high velocity armor penetrator |
| FR2840402B1 (en) * | 2002-05-31 | 2004-07-16 | Giat Ind Sa | ENCLOSURE GENERATING CHIPS, EXPLOSIVE CHARGE AND AMMUNITION IMPLEMENTING SUCH AN ENVELOPE |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE104738C (en) * | ||||
| CH8049A (en) * | 1894-02-23 | 1894-08-15 | Franz Tscherin | New floor |
| DE554538C (en) * | 1926-06-13 | 1932-07-09 | Elek Sche App M B H Ges | Bullet made from a tungsten-nickel alloy |
| DE737734C (en) * | 1934-11-14 | 1943-07-22 | Rheinmetall Borsig Ag | Hardened tank bullet |
| FR1212390A (en) * | 1959-05-26 | 1960-03-23 | Use of new materials for ammunition components and methods for obtaining these components | |
| LU54097A1 (en) * | 1967-07-13 | 1969-04-29 | ||
| GB2021739B (en) * | 1978-05-24 | 1982-04-28 | Oerlikon Buehrle Ag | Spin-stabilised sabot projectile |
-
1982
- 1982-04-22 CA CA000401456A patent/CA1207186A/en not_active Expired
- 1982-04-22 DE DE8282302069T patent/DE3267756D1/en not_active Expired
- 1982-04-22 EP EP82302069A patent/EP0063927B1/en not_active Expired
- 1982-04-22 AT AT82302069T patent/ATE16850T1/en not_active IP Right Cessation
- 1982-04-23 JP JP57068552A patent/JPS5828997A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5828997A (en) | 1983-02-21 |
| EP0063927A2 (en) | 1982-11-03 |
| ATE16850T1 (en) | 1985-12-15 |
| EP0063927A3 (en) | 1983-02-02 |
| CA1207186A (en) | 1986-07-08 |
| EP0063927B1 (en) | 1985-12-04 |
| DE3267756D1 (en) | 1986-01-16 |
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