JPS60218596A - Guided missile - Google Patents

Guided missile

Info

Publication number
JPS60218596A
JPS60218596A JP7295584A JP7295584A JPS60218596A JP S60218596 A JPS60218596 A JP S60218596A JP 7295584 A JP7295584 A JP 7295584A JP 7295584 A JP7295584 A JP 7295584A JP S60218596 A JPS60218596 A JP S60218596A
Authority
JP
Japan
Prior art keywords
warhead
guided missile
head device
homing head
shaped explosive
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
JP7295584A
Other languages
Japanese (ja)
Other versions
JPH0128878B2 (en
Inventor
山川 守良
横山 章
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.)
Technical Research and Development Institute of Japan Defence Agency
Original Assignee
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 Technical Research and Development Institute of Japan Defence Agency filed Critical Technical Research and Development Institute of Japan Defence Agency
Priority to JP7295584A priority Critical patent/JPS60218596A/en
Publication of JPS60218596A publication Critical patent/JPS60218596A/en
Publication of JPH0128878B2 publication Critical patent/JPH0128878B2/ja
Granted legal-status Critical Current

Links

Landscapes

  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【発明の詳細な説明】 本発明はノイマン効果又は破片自己鍛造弾頭(以下「ノ
イマン効果等」という。)を利用する弾頭部を備えてな
る誘導弾に関し、特に、そのホーミングヘッド装置の構
成部材に関するものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a guided missile equipped with a warhead that utilizes the Neumann effect or a fragment self-forging warhead (hereinafter referred to as "Neumann effect, etc."), and particularly relates to a component of a homing head device thereof. It is something.

従来この種誘導弾の弾頭部は、成形炸薬とソヤイロ、ジ
ンバル及びこれらを支持する部材或いはアンテナ等から
なるホーミングヘッド装置を備えてなるものであるが、
目標の探知、捕捉等を役目とするホーミングヘッド装置
は、前方視界を良好にするため、誘導弾の最前端部に位
置せしめる必要がちシ、従って成形炸薬等はその後方に
位置するのが一般的であった。
Conventionally, the warhead of this type of guided missile is equipped with a homing head device consisting of a shaped explosive charge, a soil, a gimbal, and a member or antenna that supports them.
The homing head device, whose role is to detect and acquire targets, tends to be located at the very front end of the guided missile in order to provide good forward visibility, and therefore shaped explosives, etc. are generally located behind it. Met.

本発明が適用されるノイマン効果等を利用する誘導弾は
、第1図に示す如くレドーム6におおわれた弾道部内に
は成形炸薬1が設けられ、また、その端部に成形炸薬内
ライナー2が貼設されている。炸薬1の前方には、ジャ
イロ、ジンバル又はこれらを支持する構造物等(以下単
に構造物等という。)3とアンテナ4から構成されるホ
ーミングヘッド装置5が内蔵されている。
As shown in FIG. 1, a guided missile that utilizes the Neumann effect or the like to which the present invention is applied is provided with a shaped explosive charge 1 in the trajectory section covered by a radome 6, and a shaped explosive liner 2 at the end thereof. It is pasted. In front of the explosive charge 1, a homing head device 5 comprising a gyro, a gimbal, or a structure supporting these (hereinafter simply referred to as a structure) 3 and an antenna 4 is built-in.

しかして、成形炸薬によるノイマン効果とは、成形炸薬
内ライナーの溶融金属を高温かつ高速のジェットとして
射出し、目標となる装甲鋼板等を射抜くことをいい、ま
た、破片自己鍛造弾頭とは、爆発により細かく破砕され
る重金属類が高速でビーム状に射出し前記目標の装甲鋼
板等を射抜くものである。
However, the Neumann effect of a shaped explosive means that the molten metal in the liner inside the shaped explosive is injected as a high-temperature, high-velocity jet to pierce the target, such as armored steel plates, and the fragmentation self-forging warhead is an explosion. Heavy metals that are crushed into smaller pieces are ejected at high speed in the form of a beam to pierce the target armor steel plate, etc.

しかしながら、いずれの場合にあっても成形炸薬1の前
部即ちホーミングヘッド装置5が金属塊等から構成され
ている場合には、弾頭部が目標に衝突したとき変形をき
たし、このため生成するジェット等が変形し、或いは、
該金属塊等に該ソエット等のエネルギの多くを吸収され
るため弾頭におけるノイマン効果等を十分に発揮するこ
とができなかった。なお、第1図で符号7は弾着センサ
、同8は信管、同9はブースタを示している。
However, in any case, if the front part of the shaped explosive charge 1, that is, the homing head device 5, is composed of a metal block or the like, the warhead will be deformed when it collides with the target, resulting in the formation of jets. etc. are deformed, or
Since most of the energy of the soet was absorbed by the metal lump, etc., the Neumann effect etc. in the warhead could not be fully demonstrated. In FIG. 1, reference numeral 7 indicates an impact sensor, 8 indicates a fuse, and 9 indicates a booster.

本発明は、誘導弾内部における弾頭威力の低下を可及的
減少させるため構造物等3とアンテナ4の一部又は全部
を着弾によシ破砕する引張シ強度4〜20 kg//+
i” のエンジニアリングセラミックス又ハエンソニア
リングプラスチックス或いはこれらの複合物によ多構成
せしめるもので、かくして、弾頭部が目標に衝突すると
、該構造物等3、アンテナ4等が速かに破砕して弾頭部
前方の障害が除かれ、成形炸薬の爆発に伴う所望のソエ
ット等が確実に目標を射抜き、ノイマン効果等の有効性
が−属高められるが如き誘導弾を提供することをその目
的とするものである。
The present invention provides a tensile strength of 4 to 20 kg//+ for crushing part or all of the structure 3 and antenna 4 upon impact, in order to reduce the drop in warhead power inside the guided missile as much as possible.
The warhead is made of engineering ceramics, hardening plastics, or composites of these materials, so that when the warhead collides with the target, the structures 3, antennas 4, etc. are quickly shattered. The purpose is to provide a guided missile in which obstacles in front of the warhead are removed, the desired soot, etc., accompanying the explosion of the shaped charge reliably hits the target, and the effectiveness of the Neumann effect etc. is increased. It is something.

本発明に係るエンジニアリングセラミックスの1例とし
てα−アルミナが、また、エンジニアリンググラスチッ
クスの1例としてエポキシ樹脂成形品等があるが、これ
らの材料はいずれも引張強度4〜20ユ//IIl+2
のもので、第3図に示す如き支台Cの上に載置された直
径106n、厚さ57mの円形試料Aに対し、高さh 
= 10 mの位置から直径40の鋼球Bf、自由落下
して該試料に直撃させる衝撃試験において、試料Aが5
關角以下の細片に破砕されるものである。
An example of engineering ceramics according to the present invention is α-alumina, and an example of engineering glasstics is an epoxy resin molded product, but both of these materials have a tensile strength of 4 to 20 U//IIl+2.
For a circular sample A with a diameter of 106n and a thickness of 57m placed on a support C as shown in Fig. 3, the height h
In an impact test in which a steel ball Bf with a diameter of 40 was freely dropped from a position of 10 m and directly hit the sample, sample A was
It is crushed into pieces smaller than the angle of angle.

さらに図面を参照しノイマン効果を利用する弾頭部に係
る実施例に基づいて本発明を説明する。
Furthermore, with reference to the drawings, the present invention will be described based on an embodiment of a warhead that utilizes the Neumann effect.

第2図(4)においては、成形炸薬1の爆発によシ概ね
三角錐状に形成される成形炸薬内ライナー2のソエット
12は、弾頭前方に障害物が存在しないので、例えば目
標物である金属板13を貫通して孔14を穿つこととな
るが、弾頭前方に金属塊からなる構造物等やアンテナを
含むホーミングヘッド装置5が存在する場合には、第2
図(B)に示す如く、弾頭部が目標に衝突しても破壊さ
れにくい構成部材は変形状態で残シ、ジェット12はこ
れらの構造物等に当ってこれらを破壊又は貫通したのち
でなければ目標物13に到達しないため、ジェット12
のエネルギーは減少し、ノイマン効果が大幅に弱まるこ
ととなる。
In FIG. 2 (4), the sotte 12 of the shaped explosive liner 2, which is formed into a roughly triangular pyramid shape by the explosion of the shaped explosive charge 1, is a target object because there is no obstacle in front of the warhead. A hole 14 is drilled through the metal plate 13, but if there is a structure made of a metal lump or a homing head device 5 including an antenna in front of the warhead, the second
As shown in Figure (B), even if the warhead collides with the target, the structural members that are difficult to destroy remain in a deformed state, and the jet 12 must hit these structures and destroy or penetrate them. The jet 12 does not reach the target 13.
energy will decrease, and the Neumann effect will be significantly weakened.

本発明に係るエンジニアリングセラミックス、エンジニ
アリンググラスチックス又はこれらの複合体を使用して
ホーミングヘッド装置、就中、構造物等3及びアンテナ
4の一部又は全部を構成した場合、弾頭部の衝突によシ
生成されるジェットの先端が速かに目標物に到達するこ
ととなシノイマン効果の有効性を高めうろこととなる。
When a part or all of the homing head device, especially the structure 3 and the antenna 4 are constructed using the engineering ceramics, engineering glasstics, or composites thereof according to the present invention, there is no damage caused by the collision of the warhead. The tip of the generated jet will quickly reach the target, increasing the effectiveness of the Chinoimann effect.

いま、第2図(4)の如く、成形炸薬1の前方に構造物
等及びアンテナを有しない弾頭部を速度150m/秒で
走行して目標物13に衝突せしめ、成形炸薬lを爆発さ
せた場合厚さ206nの装甲鋼板からなる該目標物には
直径約1crnの孔14が貫通した。
Now, as shown in Figure 2 (4), the warhead, which does not have structures or antennas in front of the shaped explosive charge 1, travels at a speed of 150 m/s and collides with the target object 13, causing the shaped explosive charge 1 to explode. The target, which in this case consisted of an armored steel plate with a thickness of 206 nm, was pierced by a hole 14 with a diameter of about 1 crn.

ついで、第2図(B)の如く、成形炸薬1の前方に金属
性の構造物等3及びアンテナ4からなるホーミングヘッ
ド部を有する弾頭部を同様に約150m/秒で走行させ
、上記と同様の装甲鋼板からなる □目標物13に衝突
せしめた場合、直径約ltMの孔は該鋼板を貫通せず、
深さ約15crnのところに止った。さらに、本発明に
係るエンジニアリングセラミックス及びエンジニアリン
ググラスチックスからなるホーミングヘッド装置を有す
る誘導弾の弾頭部にあっては、第2図(C)に示す如く
、上記と同様の条件で成形炸薬を爆発させたときホーミ
ングヘッド装置は完全に破砕物15とな9、同時に直径
1mの孔が完全に貫通し、発明所期の目的が十分に達成
された。
Next, as shown in FIG. 2(B), a warhead having a homing head portion consisting of a metal structure 3 and an antenna 4 was similarly run at about 150 m/sec in front of the shaped explosive charge 1, and the same as above. consists of an armored steel plate of
It stopped at a depth of about 15 crn. Furthermore, in the warhead of a guided missile having a homing head device made of engineering ceramics and engineering glasstics according to the present invention, a shaped explosive charge is detonated under the same conditions as above, as shown in FIG. 2(C). At this time, the homing head device was completely crushed 9, and at the same time, the hole with a diameter of 1 m was completely penetrated, and the intended purpose of the invention was fully achieved.

なお、上記実施例では、アンテナを有するホーミングヘ
ッド装置について述べたが、アンテナのかわシにレンズ
等を有するティクル方式のホーミングヘッド装置の場合
にも概ね同様の効果を葵しうるものである。また、本発
明はノイマン効果等を利用した誘導弾に係るものであっ
たが、誘導弾以外の類似の構造を有する砲弾前にあって
も、同第2図(B) 第2図(C) 第3図
In the above embodiments, a homing head device having an antenna has been described, but similar effects can be obtained in the case of a tickle type homing head device having a lens or the like in place of the antenna. In addition, although the present invention relates to a guided projectile that utilizes the Neumann effect, etc., even if it is in front of a shell having a similar structure other than a guided projectile, it can be used as shown in Fig. 2 (B) and Fig. 2 (C). Figure 3

Claims (1)

【特許請求の範囲】[Claims] ノイマン効果又は破片自己鍛造弾頭を利用する弾頭部を
備えてなる誘導弾において、該弾頭部の成形炸薬の前方
に位置せしめられるホーミングヘッド装置の構成部材の
一部又は全部が引張勺強度4〜20ψt2で目標物に対
する衝突によシ破砕するエンジニアリングセラミックス
又はエンジニアリングプラスチックス或いはこれらの複
合物からなることを特徴とする誘導弾。
In a guided missile comprising a warhead that utilizes the Neumann effect or a fragment self-forging warhead, some or all of the constituent members of the homing head device positioned in front of the shaped explosive of the warhead have a tensile strength of 4 to 20 ψt2. A guided missile characterized by being made of engineering ceramics, engineering plastics, or a composite thereof that shatters upon impact with a target object.
JP7295584A 1984-04-13 1984-04-13 Guided missile Granted JPS60218596A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP7295584A JPS60218596A (en) 1984-04-13 1984-04-13 Guided missile

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP7295584A JPS60218596A (en) 1984-04-13 1984-04-13 Guided missile

Publications (2)

Publication Number Publication Date
JPS60218596A true JPS60218596A (en) 1985-11-01
JPH0128878B2 JPH0128878B2 (en) 1989-06-06

Family

ID=13504313

Family Applications (1)

Application Number Title Priority Date Filing Date
JP7295584A Granted JPS60218596A (en) 1984-04-13 1984-04-13 Guided missile

Country Status (1)

Country Link
JP (1) JPS60218596A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH02106700A (en) * 1988-10-14 1990-04-18 Mitsubishi Heavy Ind Ltd Guided flying body

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5058900A (en) * 1973-09-27 1975-05-21

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5058900A (en) * 1973-09-27 1975-05-21

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH02106700A (en) * 1988-10-14 1990-04-18 Mitsubishi Heavy Ind Ltd Guided flying body

Also Published As

Publication number Publication date
JPH0128878B2 (en) 1989-06-06

Similar Documents

Publication Publication Date Title
US3302570A (en) Armor piercing, fragmenting and incendiary projectile
US4545286A (en) Active armor
US6494139B1 (en) Hole boring charge assembly
US8661980B1 (en) Weapon and weapon system employing the same
WO2008073540B1 (en) Weapons and weapon components incorporating reactive materials and related methods
US10837740B2 (en) Reactive armor
USH1235H (en) Armor-piercing projectile
CA1103090A (en) Overhead attack missile
US20180299229A1 (en) Reactive armor
ES2544762T3 (en) System and procedure for the protection of an enclosure
JP2004501339A (en) Self-propelled projectile with penetrating core
US5003885A (en) Warhead for an airborne body
JP7078699B2 (en) Reactive armor
US6244156B1 (en) Method of protecting an object from the effect of a high-speed projectile
US6581504B2 (en) Passive armor for protection against shaped charges
US4690062A (en) Warhead, especially for the attacking of radar installations
US3948180A (en) Non-explosive shaped-charge follow-through projectile
US8074552B1 (en) Flyer plate armor systems and methods
JPH0128878B2 (en)
RU2062439C1 (en) Hollow-charge tandem warhead
US5515786A (en) Projectiles for attacking hard targets and method for controlling initiation of a projectile
USH344H (en) High velocity canting shaped charge warhead
JP2018506697A5 (en)
EP0760458A1 (en) Asymmetric penetration warhead
GB1581125A (en) Structure for protection against projectile

Legal Events

Date Code Title Description
EXPY Cancellation because of completion of term