JPH06102000A - Warhead for tandem warhead - Google Patents

Warhead for tandem warhead

Info

Publication number
JPH06102000A
JPH06102000A JP27661192A JP27661192A JPH06102000A JP H06102000 A JPH06102000 A JP H06102000A JP 27661192 A JP27661192 A JP 27661192A JP 27661192 A JP27661192 A JP 27661192A JP H06102000 A JPH06102000 A JP H06102000A
Authority
JP
Japan
Prior art keywords
warhead
tandem
bullet
jet
era
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.)
Granted
Application number
JP27661192A
Other languages
Japanese (ja)
Other versions
JP2603176B2 (en
Inventor
Norio Sogo
憲夫 十河
Hideyo Ando
英世 安藤
Hirotaka Sato
浩孝 佐藤
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Japan Steel Works Ltd
Kawasaki Heavy Industries Ltd
Technical Research and Development Institute of Japan Defence Agency
Original Assignee
Japan Steel Works Ltd
Kawasaki Heavy Industries Ltd
Technical Research and Development Institute of Japan Defence Agency
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Japan Steel Works Ltd, Kawasaki Heavy Industries Ltd, Technical Research and Development Institute of Japan Defence Agency filed Critical Japan Steel Works Ltd
Priority to JP4276611A priority Critical patent/JP2603176B2/en
Publication of JPH06102000A publication Critical patent/JPH06102000A/en
Application granted granted Critical
Publication of JP2603176B2 publication Critical patent/JP2603176B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/04Projectiles, 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
    • F42B12/10Projectiles, 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
    • F42B12/16Projectiles, 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 in combination with an additional projectile or charge, acting successively on the target

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

(57)【要約】 【目的】 弾体内でのレイアウトの効率を高める。 【構成】 ATM2に搭載されるタンデム弾頭用子弾頭
1であって、ATM2の弾体3の内周又は外周に沿った
円弧状又はリング状に形成されることにより、弾体内に
配置された子弾頭によって生ずるデッドスペースを減少
させる。
(57) [Abstract] [Purpose] To improve the efficiency of the layout in the ammunition. [Structure] A tandem warhead warhead 1 to be mounted on an ATM 2, which is arranged in an ammunition body by being formed in an arc shape or a ring shape along an inner circumference or an outer circumference of an ammunition body 3 of the ATM 2. Reduces dead space caused by warheads.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は、ホーミング装置を有す
る誘導弾等、弾頭の前方に機器を設けた弾体に搭載され
るタンデム弾頭用子弾頭に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a tandem warhead warhead to be mounted on a bullet body equipped with equipment in front of a warhead such as a guided bullet having a homing device.

【0002】[0002]

【従来の技術】近年、戦車の対戦車兵器に対する防護策
の一つとして、反応装甲(Explosive Rea
ctive Armor:ERA)が注目されている。
ERAは、主にモンロー効果(弾殻の内部にさく薬を漏
斗状に充填し、弾着時漏斗孔の中心線上に爆発のエネル
ギーを集中させること。)を有する対戦車榴弾(Hig
h Explosive Anti−Tank:HEA
T)に対し抑止力を発揮するものであり、一例ではHE
ATの貫徹力の80%を減殺させ得るという結果も報告
されている。
2. Description of the Related Art In recent years, as one of the protective measures against anti-tank weapons of tanks, reactive armor (Explosive Rea) is used.
The active armor (ERA) has attracted attention.
ERA is an anti-tank grenade (Hig) that mainly has the Monroe effect (funnel-like filling of the shell with a piercing agent and concentrating the energy of the explosion on the centerline of the funnel hole when landing).
h Explosive Anti-Tank: HEA
It exerts a deterrent against T), and in one example, HE
It has also been reported that 80% of AT's penetration can be reduced.

【0003】ERAの基本的な構造は、2枚の鋼板の間
に爆薬を挟み込んだものであり、戦車の主装甲の表面に
所要の距離をおいて装着できるように設けられている。
ERAのHEATに対する貫徹力阻害は、弾頭の爆発に
よって生成されたジェットをERAの爆薬の爆発と鋼板
の飛散とによって散乱させることにより行われる。戦車
のERA装着による防護力向上に対し、HEAT側とし
ては、ERAに対処することが最重要課題となってお
り、その一対抗策として、タンデム弾頭(子弾頭と主弾
頭の2つの弾頭で構成される。)の開発が進められてい
る。
The basic structure of the ERA is that explosives are sandwiched between two steel plates, and they are provided so that they can be mounted on the surface of the main armor of a tank at a required distance.
The inhibition of the penetration force of ERA against HEAT is performed by scattering the jet generated by the explosion of the warhead by the explosion of the explosive of ERA and the scattering of the steel plate. For the HEAT side, it is the most important issue to deal with ERA against the improvement of protection by mounting ERA on tanks. As a countermeasure against it, tandem warhead (composed of two warheads, subwarhead and main warhead) Is being developed.

【0004】タンデム弾頭は、2段攻撃には対処できな
いというERAの欠点を利用したもので、ERA起爆方
式の場合、子弾頭のジェットによってERAを起爆させ
てその鋼板が軸線を離脱(ERAが無力化)した後、主
弾頭のジェットが阻害を受けずに進行して主装甲を貫徹
する一方、ERA無反応方式の場合、子弾頭のジェット
によってERAの爆薬を飛散させ、爆薬の無くなった部
分を主弾頭のジェットが通過するため、ERAは起爆せ
ず(ERAが無力化し)主弾頭のジェットは阻害を受け
ずに主装甲を貫徹するものである。従来、この種のタン
デム弾頭用子弾頭としては、図4に示すように、円筒状
の弾殻21内にさく薬22を漏斗状に充填すると共に、
その表面をライナ23で覆い、かつ弾殻21の後端部に
伝爆薬24を取り付けた円筒状子弾頭25が知られてい
る。
The tandem warhead utilizes the disadvantage of ERA that it cannot deal with a two-stage attack. In the case of the ERA detonation method, the steel plate leaves the axis line by detonating the ERA by the jet of the sub-warhead. After that, while the jet of the main warhead advances without being obstructed and penetrates the main armor, in the case of the ERA non-reactive method, the explosive of ERA is scattered by the jet of the warhead and the part where the explosive is lost Since the jet of the main warhead passes, the ERA does not detonate (the ERA becomes ineffective), and the jet of the main warhead penetrates the main armor without being obstructed. Conventionally, as a sub-warhead for this type of tandem warhead, as shown in FIG. 4, while a cylindrical shell 21 is filled with a punch 22 in a funnel shape,
There is known a cylindrical warhead 25 whose surface is covered with a liner 23 and which has an explosive charge 24 attached to the rear end of the shell 21.

【0005】この円筒状子弾頭25は、図5に示すよう
に、ATM26の弾体27内の前方に搭載された誘導装
置等の搭載物28の適宜後方に搭載されている。そし
て、円筒状子弾頭25は、ATM26が戦車の反応装甲
31に接近又は接触すると伝爆薬24の起爆によりさく
薬22が爆発され、この爆発のエネルギーのモンロー効
果によるジェットによってERA31を無力化し、しか
る後に信管32によって主弾頭29のさく薬30が爆発
され、そのジェットにより主装甲33が貫徹されるもの
である。
As shown in FIG. 5, the cylindrical warhead 25 is appropriately mounted behind a mount 28 such as a guiding device mounted in the front of the bullet 27 of the ATM 26. Then, when the ATM 26 approaches or contacts the reaction armor 31 of the tank, the cylindrical warhead 25 explodes the explosive 22 due to the detonation of the explosive charge 24, and the ERA 31 is inactivated by the jet due to the Monroe effect of the energy of this explosion. The fuse 32 explodes the shell 30 of the main warhead 29, and the jet penetrates the main armor 33.

【0006】[0006]

【発明が解決しようとする課題】この従来のタンデム弾
頭用子弾頭では、ATMにタンデム弾頭を搭載する場
合、子弾頭の前方に誘導装置等の搭載物が存在すること
があるので、子弾頭のジェットを、誘導装置等の阻害を
受けながらもERAを無力化し得る威力を有するものと
する必要があり、子弾頭には、必然的に口径の大きなも
のが要求される。このように、口径の大きな子弾頭をA
TMに搭載する場合、子弾頭の大型化の他、図6に示す
ように、ATM26の弾体27内におけるレイアウトの
効率が悪くなり、デッドスペース34の増加につなが
る。これは、ATMのみならず全ての飛しょう体に恒常
的に要求される小型軽量化に対して悪影響を与える結果
となる。そこで、本発明は、弾体内でのレイアウトの効
率を高め、かつ小型化を可能とするタンデム弾頭用子弾
頭の提供を目的とする。
In this conventional tandem warhead warhead, when a tandem warhead is mounted on an ATM, there may be a loading device such as a guiding device in front of the warhead. It is necessary to make the jet powerful enough to neutralize the ERA while being hindered by the guidance device and the like, and the warhead must necessarily have a large caliber. In this way, A
When it is mounted on the TM, the size of the warhead is increased and, as shown in FIG. 6, the layout efficiency in the bullet 27 of the ATM 26 is deteriorated and the dead space 34 is increased. This has an adverse effect on the miniaturization and weight reduction which is constantly required for all flying objects as well as ATM. Therefore, it is an object of the present invention to provide a sub-warhead for a tandem warhead that enhances the efficiency of layout in the bullet body and enables miniaturization.

【0007】[0007]

【課題を解決するための手段】本発明の第1のタンデム
弾頭用子弾頭は、弾頭の前方に機器を設けた弾体に搭載
されるタンデム弾頭用子弾頭であって、弾体の内周又は
外周に沿った円弧状又はリング状に形成されているもの
である。又、第2のタンデム弾頭用子弾頭は、弾頭の前
方に機器を設けた弾体に搭載されるダンデム弾頭用子弾
頭であって、弾体の内周又は外周に沿った円弧状又はリ
ング状に形成され、かつ上記弾体内に搭載された誘導装
置等の搭載物の外周に配置されているものである。ここ
で、リング状とは、弾体の内周又は外周の全周に沿うリ
ングと、複数の円弧状のものを内周又は外周に沿って適
宜に離隔して配置したものとの双方をいう。
A first tandem warhead warhead of the present invention is a tandem warhead warhead mounted on a bullet equipped with a device in front of the warhead, and has an inner circumference. Alternatively, it is formed in an arc shape or a ring shape along the outer circumference. The second tandem warhead warhead is a tandem warhead warhead that is mounted on a bullet that has a device in front of the warhead, and has an arc shape or ring shape along the inner or outer circumference of the bullet. And is arranged on the outer periphery of a mounting object such as a guiding device mounted in the bullet body. Here, the term "ring-shaped" refers to both a ring that extends along the entire inner or outer circumference of the bullet and a plurality of arc-shaped objects that are appropriately spaced along the inner or outer circumference. .

【0008】[0008]

【作用】上記第1の手段においては、弾体内に配置され
た子弾頭によって生ずるデットスペースが減少する。
又、第2の手段においては、第1の手段と同様の作用の
他に、子弾頭のジェットが搭載物の阻害を受けることが
ない。
In the first means described above, the dead space generated by the sub-warhead placed inside the ammunition body is reduced.
Further, in the second means, in addition to the same operation as in the first means, the jet of the warhead is not obstructed by the loaded object.

【0009】[0009]

【実施例】次に、本発明の実施例について図面を参照し
て説明する。図1,図2は本発明の一実施例のタンデム
弾頭用子弾頭の斜視図、その子弾頭を備えたATMの要
部の概略図である。この子弾頭1は、対戦車誘導弾(A
TM)2の弾体3の内周に沿った円弧状にして、かつA
TM2の前方(図1,図2においては先方)へ開口した
チャンネル状に形成され、ATM2の弾体3内に搭載さ
れた誘導装置等の搭載物4の周囲に配置された弾殻5を
有している。弾殻5内には、その幅方向の中間部を最深
部とするV字状のさく薬6が、弾着時に幅方向の中間部
を通る曲面C.Sに曲面ジェットを生成させ、かつAT
M2の適宜前方におけるその中心線L上のジェット焦点
Oに収斂するように充填され、このさく薬6の表面は、
ライナ7によって覆われている。そして、弾殻5の底部
外側における幅方向の中間部には、伝爆薬8が取付けら
れている。
Embodiments of the present invention will now be described with reference to the drawings. 1 and 2 are a perspective view of a sub-warhead for a tandem warhead according to one embodiment of the present invention, and a schematic view of a main part of an ATM having the sub-warhead. This warhead 1 is an anti-tank guided bullet (A
TM) 2 is made into an arc shape along the inner circumference of the bullet 3 and A
It has a shell 5 formed in a channel shape that opens to the front of TM2 (the front side in FIGS. 1 and 2), and is arranged around a mounting object 4 such as a guiding device mounted in the shell 3 of the ATM2. is doing. Inside the shell 5, there is formed a V-shaped punch 6 having a middle portion in the width direction as the deepest portion, and a curved surface C.I. Generates a curved jet on S, and AT
The surface of the explosive 6 is filled so as to converge on the jet focal point O on the center line L thereof in front of M2 as appropriate.
Covered by liner 7. An explosive charge 8 is attached to the middle portion of the shell 5 outside the bottom in the width direction.

【0010】上記構成の子弾頭1を備えたATM2にお
いては、伝爆薬8の起爆によりさく薬6が爆発され、そ
の爆轟波を曲面C.S上に集中させると共にジェット焦
点Oに収斂させるモンロー効果によって、ジェット焦点
O上に位置する図示しない戦車のERAに衝突させてE
RAを無力化させ、その後、ATM2の図示しない主弾
頭が起爆し、主弾頭のジェットがERAの阻害を受けず
に主装甲を貫徹するものである。従って、このタンデム
弾頭用子弾頭1によれば、図3に示すようにATM2の
弾体3内におけるデッドスペース9が極めて小さくな
り、ATM2内でのレイアウトの効率が非常に高くな
る。ジェットをジェット焦点Oに収斂させるに際し、ジ
ェットが搭載物4によって阻害されることがなく、子弾
頭1を小型化することができる。
In the ATM 2 equipped with the warhead 1 having the above structure, the explosive charge 6 is exploded by the detonation of the explosive charge 8, and the detonation wave is generated by the curved surface C.I. Due to the Monroe effect of concentrating on S and converging on the jet focus O, it collides with the ERA of a tank (not shown) located on the jet focus O and E
The RA is incapacitated, and then the main warhead (not shown) of the ATM2 is detonated, and the jet of the main warhead penetrates the main armor without being obstructed by the ERA. Therefore, according to this tandem warhead warhead 1, the dead space 9 in the bullet 3 of the ATM 2 becomes extremely small, as shown in FIG. 3, and the layout efficiency in the ATM 2 becomes very high. When the jet converges on the jet focal point O, the jet is not obstructed by the mounting object 4, and the subwarhead 1 can be downsized.

【0011】なお、上述した実施例においては、子弾頭
1をATM2の弾体3の内周に沿う円弧状とする場合に
ついて説明したが、これに限定されるものではなく、弾
体3の内周又は外周の全周に沿うリングとしたり、ある
いは複数の円弧状のものを円周方へ適宜に離隔して配置
してリング状としてもよく、単一の円弧状のものとほぼ
同様の作用効果が得られる。
In the above-described embodiment, the case where the sub-warhead 1 is formed in an arc shape along the inner circumference of the bullet 3 of the ATM 2 has been described, but the present invention is not limited to this and the inside of the bullet 3 is not limited to this. A ring may be formed along the entire circumference or the outer circumference, or a plurality of arc-shaped ones may be arranged in the circumferential direction at appropriate intervals to form a ring shape, which is substantially the same as a single arc-shaped one. The effect is obtained.

【0012】[0012]

【発明の効果】以上説明したように、本発明の第1のタ
ンデム弾頭用子弾頭によれば、弾体内に配置された弾頭
によって生ずるデットスペースが従来に比して大幅に減
少するので、ATM内でのレイアウトの効率を格段に高
めることができる。又、第2のタンデム弾頭用子弾頭に
よれば、第1のものと同様の作用効果の他、子弾頭のジ
ェットが搭載物の阻害を受けることがないので、比較的
小型のものでERAを無力化させることができる。
As described above, according to the first tandem warhead warhead of the present invention, the dead space generated by the warhead placed inside the ammunition body is greatly reduced as compared with the conventional art. The efficiency of internal layout can be significantly improved. In addition, according to the second tandem warhead warhead, in addition to the same effect as the first one, the jet of the warhead is not obstructed by the loaded object, so that the ERA is relatively small. Can be disabled.

【図面の簡単な説明】[Brief description of drawings]

【図1】本発明の一実施例のタンデム弾頭用子弾頭の斜
視図である。
FIG. 1 is a perspective view of a tandem warhead warhead of an embodiment of the present invention.

【図2】図1の子弾頭を備えた対戦車誘導弾の要部の概
略図である。
FIG. 2 is a schematic view of a main part of an anti-tank guided bullet equipped with the warhead of FIG.

【図3】図2におけるIII −III 線に沿った断面図であ
る。
3 is a sectional view taken along line III-III in FIG.

【図4】従来のタンデム弾頭用子弾頭の断面図である。FIG. 4 is a cross-sectional view of a conventional tandem warhead warhead.

【図5】図4の子弾頭を備えた対戦車誘導弾の一部を省
略した断面図である。
5 is a cross-sectional view in which a part of an anti-tank guided bullet equipped with the warhead of FIG. 4 is omitted.

【図6】図5におけるVI−VI線に沿った拡大断面図であ
る。
6 is an enlarged cross-sectional view taken along line VI-VI in FIG.

【符号の説明】[Explanation of symbols]

1 子弾頭 2 対戦車誘導弾(ATM) 3 弾体 4 搭載物 5 弾殻 6 さく薬 7 ライナ 8 伝爆薬 L 中心線 O ジェット焦点 C.S 曲面 1 sub-warhead 2 anti-tank guided missile (ATM) 3 bullet 4 payload 5 shell 6 punch 7 liner 8 explosive L centerline O jet focus C. S curved surface

───────────────────────────────────────────────────── フロントページの続き (72)発明者 佐藤 浩孝 岐阜県各務原市川崎町1番地 川崎重工業 株式会社岐阜工場内 ─────────────────────────────────────────────────── ─── Continuation of front page (72) Inventor Hirotaka Sato 1 Kawasaki-cho, Kakamigahara-shi, Gifu Kawasaki Heavy Industries Ltd. Gifu factory

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】 弾頭の前方に機器を設けた弾体に搭載さ
れるタンデム弾頭用子弾頭であって、弾体の内周又は外
周に沿った円弧状又はリング状に形成されていることを
特徴とするタンデム弾頭用子弾頭。
1. A sub-warhead for a tandem warhead mounted on a bullet equipped with a device in front of the warhead, which is formed in an arc shape or a ring shape along an inner circumference or an outer circumference of the bullet. Characteristic tandem warhead warhead.
【請求項2】 弾頭の前方に機器を設けた弾体に搭載さ
れるタンデム弾頭用子弾頭であって、弾体の内周又は外
周に沿った円弧状又はリング状に形成され、かつ上記弾
体内に搭載された誘導装置等の搭載物の外周に配置され
ていることを特徴とするタンデム弾頭用子弾頭。
2. A warhead for a tandem warhead, which is mounted on an ammunition body provided with a device in front of the warhead, and is formed in an arc shape or a ring shape along an inner circumference or an outer circumference of the ammunition body. A sub-warhead for a tandem warhead, which is arranged on the outer periphery of a loaded object such as a guidance device mounted inside the body.
JP4276611A 1992-09-21 1992-09-21 Child warhead for tandem warhead Expired - Lifetime JP2603176B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP4276611A JP2603176B2 (en) 1992-09-21 1992-09-21 Child warhead for tandem warhead

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP4276611A JP2603176B2 (en) 1992-09-21 1992-09-21 Child warhead for tandem warhead

Publications (2)

Publication Number Publication Date
JPH06102000A true JPH06102000A (en) 1994-04-12
JP2603176B2 JP2603176B2 (en) 1997-04-23

Family

ID=17571859

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4276611A Expired - Lifetime JP2603176B2 (en) 1992-09-21 1992-09-21 Child warhead for tandem warhead

Country Status (1)

Country Link
JP (1) JP2603176B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008121953A (en) * 2006-11-10 2008-05-29 Daikin Ind Ltd Molded glaze warhead and liner

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63259400A (en) * 1986-06-05 1988-10-26 カナダ国 Nose with sub-projectile
JPH0355500A (en) * 1989-07-19 1991-03-11 Hughes Aircraft Co Module missile reinforcing apparatus
JPH043900A (en) * 1990-04-19 1992-01-08 Mitsubishi Electric Corp Guidance control method for parent-child guided flying object

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63259400A (en) * 1986-06-05 1988-10-26 カナダ国 Nose with sub-projectile
JPH0355500A (en) * 1989-07-19 1991-03-11 Hughes Aircraft Co Module missile reinforcing apparatus
JPH043900A (en) * 1990-04-19 1992-01-08 Mitsubishi Electric Corp Guidance control method for parent-child guided flying object

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008121953A (en) * 2006-11-10 2008-05-29 Daikin Ind Ltd Molded glaze warhead and liner

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