EP0249678A2 - Ammunition, especially for fighting targets provided with a reactive armour - Google Patents

Ammunition, especially for fighting targets provided with a reactive armour Download PDF

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Publication number
EP0249678A2
EP0249678A2 EP87102607A EP87102607A EP0249678A2 EP 0249678 A2 EP0249678 A2 EP 0249678A2 EP 87102607 A EP87102607 A EP 87102607A EP 87102607 A EP87102607 A EP 87102607A EP 0249678 A2 EP0249678 A2 EP 0249678A2
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EP
European Patent Office
Prior art keywords
charge
active body
target
active
body according
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
EP87102607A
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German (de)
French (fr)
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EP0249678B1 (en
EP0249678B2 (en
EP0249678A3 (en
Inventor
Jörg Dr. Peters
Benjamin Furch
Jürg Pfaehler
Jürgen Dr. Böcker
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Rheinmetall Industrie AG
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Rheinmetall GmbH
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Application filed by Rheinmetall GmbH filed Critical Rheinmetall GmbH
Priority to AT87102607T priority Critical patent/ATE55831T1/en
Publication of EP0249678A2 publication Critical patent/EP0249678A2/en
Publication of EP0249678A3 publication Critical patent/EP0249678A3/en
Publication of EP0249678B1 publication Critical patent/EP0249678B1/en
Application granted granted Critical
Publication of EP0249678B2 publication Critical patent/EP0249678B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • 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
    • F42B1/032—Shaped or hollow charges characterised by the material of the liner
    • 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
    • F42B12/16—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 in combination with an additional projectile or charge, acting successively on the target
    • F42B12/18—Hollow charges in tandem arrangement

Definitions

  • the invention relates to an active body according to the preamble of patent claim 1.
  • a generic object is known from DE-OS 34 16 787.
  • the two landings are essentially of the same diameter, and each of them is arranged in a respective housing with stabilizing wings and forms an independent projectile after the initiation of a separate separating charge.
  • an active body 10 has a casing 11 with a charge 12 that is rotationally symmetrical with respect to the longitudinal axis A.
  • a connection means 13 serves as a receptacle for devices 22 for the power supply for control electronics 24.
  • a tube 15 defines an A coaxial channel 16 for a shaped charge beam to be formed from an insert 14 after the charge 12 has been initiated.
  • the tube 15 serves as a receptacle with a front region of the channel 16 of a charge 18 with a casing 19 and a flat projectile-forming insert 20.
  • the active body 10 is particularly advantageously suitable for combating, in particular actively, armored targets.
  • a proximity fuse not shown and known per se, specifies a predeterminable distance a signal to the control electronics 24 from a target.
  • a first control signal for initiating the front load 18 is formed from the signal, and a projectile from the flat insert 20 leads the active body 10 ahead of the target.
  • a known interference device is brought into effect there by the impact of the projectile and is thus rendered harmless for a shaped charge jet which is formed from the insert 14 of the rear charge 12 initiated by a second control signal.
  • the target-side "interference suppression effect" is achieved with space-saving means, with the lowest possible dead load component and without a separation charge which increases and complicates the susceptibility of the active body and complicates it, which is known from the publication cited at the beginning.
  • the flat insert 20 of the front load 18 is preferably made of a material with an average density between about 16 and about 19 g / cm3.
  • a target-side interfering device is made harmless with a high probability, so that the shaped charge jet from the insert 14 can become fully effective.
  • a cheapest stand-off can be observed. Because of the comparatively small size of the insert 20, the price for the insert material does not need to play such an important role, so that, for example, the use of tantalum does not hinder the cost.
  • FIGS. 2, 3 and 4 of the drawing it can be seen in connection with the above description how versatile the active body 10 according to the invention is.
  • the active body 10 is inserted into a warhead 40, which can be ejected from a cargo floor as a steerable submunition unit.
  • a warhead 40 which can be ejected from a cargo floor as a steerable submunition unit.
  • the connection means 13 ⁇ extends to a known seeker 52 and serves electronics 44 and a control block 46 with gas generators 48 and control nozzles 50 as a receptacle, the aforementioned devices behind the seeker 52 around the pipe 15 with the channel 16 to save space group.
  • Stabilizing wings 42 can be pivoted in a known manner from a space-saving transport position into the operative position shown.
  • the direction of flight of the warhead 40 with the active body 10 is indicated by an arrow F.
  • the active body 10 slightly modified, (reference is made, inter alia, to the shape of the insert 64) of an anti-tank mine 60. It has a launch tube 62 on a tripod mount 74.
  • the central longitudinal axis (not shown) of a known target device 66 with the required control electronics runs parallel to the longitudinal axis A.
  • a rocket engine 70 can be initiated via an ignition device 68.
  • the launch tube 62 is set up by means of the mount 74 so that its longitudinal axis is directed towards an area in which armored targets to be combated are expected. If the target device 66 has identified such a target, the ignition device 68 is initiated via a signal and the rocket motor 70 is ignited by it.
  • the active body 10 leaves the tube 62 after blasting away its cover 76 in the direction of an arrow F, and stabilizing wing 72 fold out of their rest position shown in the drawing into their operative position. Because of the sequence of functions, reference is made to the description in conjunction with FIG. 1.
  • FIG. 4 shows an anti-tank projectile 80 of a known ammunition for a cannon.
  • the tube 15 is designed as a standoff tube 82 and carries on the front side a known approach nozzle 86, which is therefore not shown or described in detail.
  • a known stabilizing stabilizer 90 is arranged on a tail boom 88.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Optical Radar Systems And Details Thereof (AREA)
  • Agricultural Chemicals And Associated Chemicals (AREA)
  • Chemical And Physical Treatments For Wood And The Like (AREA)
  • Fire-Extinguishing Compositions (AREA)
  • Valve-Gear Or Valve Arrangements (AREA)
  • Valve Device For Special Equipments (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

1. Warhead (10, 40, 60, 80) for combating actively armoured targets, the warhead having two active charges (18, 12) arranged in succession to each other and capable of being fired by detonators provided for the purpose, the front active charge (18) having a considerably smaller diameter than the rear main charge (12) and being provided for the purpose of destroying an interference device situated at the target in front of the main armouring of the target, while the rear main charge (12) of large calibre for penetration of the main armouring is constructed as a hollow charge with a liner (14) forming a hollow charge jet, a detonator (24, 86) and a tube (15) with a channel (16) wherein - the front active charge (18) has a projectile-forming liner (20) of flat conical shape, - for the detonation of the front active charge (18) the detonator (24, 86) is designed as a proximity fuse which, through a first control signal, brings about the detonation of the front active charge (18) at a preselectable distance in front of the target, after which - the detonation of the main charge (12) is effected by means of a second control signal.

Description

Die Erfindung betrifft einen Wirkkörper nach dem Oberbe­griff des Patentanspruchs 1.The invention relates to an active body according to the preamble of patent claim 1.

Ein gattungsgleicher Gegenstand ist bekannt aus der DE-OS 34 16 787. Die beiden Landungen sind im wesentlichen einander durchmessergleich, und jede von ihnen ist in einem jeweiligen Gehäuse mit Stabilisierungsflügeln an­geordnet und bildet nach dem Initiieren einer gesonderten Trennladung jeweils ein selbständiges Projektil.A generic object is known from DE-OS 34 16 787. The two landings are essentially of the same diameter, and each of them is arranged in a respective housing with stabilizing wings and forms an independent projectile after the initiation of a separate separating charge.

Die bekannte Anordnung ist nicht nur kompliziert und sehr raum- sowie fertigungsaufwendig, sondern erzwingt auch das Vorhandensein großer zielunwirksamer Lastanteile (Totlast). Diese Nachteile fallen bei jeder Einsatzart derart ins Gewicht, daß sich als Aufgabe die dringende Forderung nach Abhilfe derart stellt, einen gattungs­gleichen Gegenstand zu schaffen, der sich raumsparend und mit geringem Totlastanteil vielseitig einsetzen läßt.The known arrangement is not only complicated and takes up a lot of space and production, but also forces the presence of large, ineffective load components (dead load). These disadvantages are so important for every type of use that the urgent need for remedy is to create a generic object that can be used in a space-saving manner and with a low dead load percentage.

Gelöst wird die Aufgabe nach der Lehre des Patentan­spruchs 1 mit den in dessen Kennzeichen angegebenen er­finderischen Merkmalen.The object is achieved according to the teaching of claim 1 with the inventive features specified in its characteristics.

Die Erfindung wird nachstehend anhand der Zeichnung näher erläutert.The invention is explained below with reference to the drawing.

Es zeigen

  • Fig. 1 eine vereinfachte Prinzipdarstellung des Wirkkörpers nach der Erfindung im längsaxialen Schnitt,
  • Fig. 2 einem aus einem Lastengeschoß als Sub­munition ausstoßbaren und lenkbaren Gefechtskopf mit dem Wirkkörper nach Fig. 1,
  • Fig. 3 eine Panzerabwehr-Richtmine mit dem Wirkkörper nach Fig. 1 und
  • Fig. 4 ein flügelstabilisiertes vollkalibriges Panzerabwehrgeschoß,
wobei in den Figuren 2, 3 und 4 aus Gründen besserer Übersichtlichkeit auf eine in Einzelheiten gehende Dar­stellung der Erfindung mit Rücksicht auf Fig. 1 verzichtet werden kann.Show it
  • Fig. 1 is a simplified schematic diagram of the active body according to the invention in a longitudinal axial section,
  • 2 a warhead, which can be ejected and steered from a cargo floor as a submunition, with the active body according to FIG. 1,
  • Fig. 3 is an anti-tank directional mine with the active body of FIG. 1 and
  • 4 a wing-stabilized full-caliber anti-tank projectile,
in FIGS. 2, 3 and 4, for reasons of better clarity, a detailed illustration of the invention with regard to FIG. 1 can be dispensed with.

Gemäß Fig. 1 weist ein Wirkkörper 10 nach der Erfindung eine zur Längsachse A rotationssymmetrische Hülle 11 mit einer Ladung 12 auf. Ein Anschlußmittel 13 dient als Aufnahme für Einrichtungen 22 zur Stromversorgung für eine Steuerelektronik 24. Ein Rohr 15 definiert einen A koaxialen Kanal 16 für einen nach dem initiieren der Ladung 12 aus einer Einlag 14 zu bildenden Hohl­ladungsstrahl. Das Rohr 15 dient mit einem vorderen Bereich des Kanals 16 einer Ladung 18 mit einer Hülle 19 und einer flachen projektilbildenden Einlage 20 als Aufnahme.1, an active body 10 according to the invention has a casing 11 with a charge 12 that is rotationally symmetrical with respect to the longitudinal axis A. A connection means 13 serves as a receptacle for devices 22 for the power supply for control electronics 24. A tube 15 defines an A coaxial channel 16 for a shaped charge beam to be formed from an insert 14 after the charge 12 has been initiated. The tube 15 serves as a receptacle with a front region of the channel 16 of a charge 18 with a casing 19 and a flat projectile-forming insert 20.

Der Wirkkörper 10 eignet sich auf besonders vorteilhafte Weise zum Bekämpfen, insbesondere aktiv, gepanzerter Ziele. Ein nicht dargestellter und an sich bekannter Annäherungszünder gibt in vorgebbarer Entfernung vor einem Ziel ein Signal an die Steuerelektronik 24. Aus dem Signal wird ein erstes Steuersignal zum Initiieren der vorderen Ladung 18 gebildet, und ein Projektil aus der flachen Einlage 20 eilt dem Wirkkörper 10 voraus gegen das Ziel. Dort wird durch das Auftreffen des Pro­jektils eine bekannte Störeinrichtung zur Wirkung ge­bracht und damit für einem Hohlladungsstrahl unschädlich gemacht, welcher aus der Einlage 14 der durch ein zweites Steuersignal initiierten, hinteren Ladung 12 gebildet wird. Der zielseitige "Entstöreffekt" wird dabei mit raumsparenden Mitteln, mit geringstmöglichem Totlastanteil und ohne eine die Störanfälligkeit des Wirkkörpers erhöhende und ihn komplizierende, aus der eingangs zitierten Druckschrift bekannte Trennladung erzielt.The active body 10 is particularly advantageously suitable for combating, in particular actively, armored targets. A proximity fuse, not shown and known per se, specifies a predeterminable distance a signal to the control electronics 24 from a target. A first control signal for initiating the front load 18 is formed from the signal, and a projectile from the flat insert 20 leads the active body 10 ahead of the target. A known interference device is brought into effect there by the impact of the projectile and is thus rendered harmless for a shaped charge jet which is formed from the insert 14 of the rear charge 12 initiated by a second control signal. The target-side "interference suppression effect" is achieved with space-saving means, with the lowest possible dead load component and without a separation charge which increases and complicates the susceptibility of the active body and complicates it, which is known from the publication cited at the beginning.

Die flache Einlage 20 der vorderen Ladung 18 besteht vorzugsweise aus einem Werkstoff mit der durchschnitt­lichen Dichte zwischen etwa 16 und etwa 19 g/cm³. Hier­durch wird infolge entsprechend hoher Wuchtwirkung des aus der Einlage 30 sprengumgeformten Projektils eine zielseitige Störeinrichtung mit hoher Wahrschein­lichkeit unschädlich gemacht, so daß der Hohlladungs­strahl aus der Einlage 14 voll zielwirksam werden kann. Dabei läßt sich ein günstigster Stand-off einhalten. Wegen der vergleichsweisen Kleinheit der Einlage 20 braucht vorteilhafterweise der Preis für den Einlagen­werkstoff keine so wesentliche Rolle zu spielen, so daß beispielsweise auch der Verwendung von Tantal kein Kostenhindernis im Wege steht.The flat insert 20 of the front load 18 is preferably made of a material with an average density between about 16 and about 19 g / cm³. As a result, due to the correspondingly high balancing effect of the projectile explosively formed from the insert 30, a target-side interfering device is made harmless with a high probability, so that the shaped charge jet from the insert 14 can become fully effective. A cheapest stand-off can be observed. Because of the comparatively small size of the insert 20, the price for the insert material does not need to play such an important role, so that, for example, the use of tantalum does not hinder the cost.

Beim Betrachten der Figuren 2, 3 und 4 der Zeichnung wird im Zusammenhang mit der vorstehenden Beschreibung erkennbar, wie vielseitig einsetzbar der Wirkkörper 10 nach der Erfindung ist.When viewing FIGS. 2, 3 and 4 of the drawing, it can be seen in connection with the above description how versatile the active body 10 according to the invention is.

Nach Figur 2 ist der Wirkkörper 10 einem Gefechtskopf 40 eingefügt, welcher als lenkbare Submunitionseinheit aus einem Lastengeschoß ausstoßbar ist. In diesem Zu­sammenhang wird auf ein Prospektblatt der Firmen Allied Bendix Aerospace und Rheinmetall GmbH (Anmelder) verwiesen, welcher seit Oktober 1985 veröffentlicht ist. Das Anschlußmittel 13ʹ erstreckt sich bis zu einem an sich bekannten Zielsuchkopf 52 und dient einer Elek­tronik 44 und einem Steuerblock 46 mit Gasgeneratoren 48 und Steuerdüsen 50 als Aufnahme, wobei sich die vor­genannten Einrichtungen hinter dem Zielsuchkopf 52 um das Rohr 15 mit dem Kanal 16 herum raumsparend gruppieren. Stabilisierungsflügel 42 sind auf bekannte Weise aus einer raumsparenden Transportstellung in ihre darge­stellte Wirkstellung schwenkbar. Die Flugrichtung des Gefechtskopfs 40 mit dem Wirkkörper 10 ist durch einen Pfeil F angedeutet.According to FIG. 2, the active body 10 is inserted into a warhead 40, which can be ejected from a cargo floor as a steerable submunition unit. In this context, reference is made to a brochure by Allied Bendix Aerospace and Rheinmetall GmbH (applicant), which has been published since October 1985. The connection means 13ʹ extends to a known seeker 52 and serves electronics 44 and a control block 46 with gas generators 48 and control nozzles 50 as a receptacle, the aforementioned devices behind the seeker 52 around the pipe 15 with the channel 16 to save space group. Stabilizing wings 42 can be pivoted in a known manner from a space-saving transport position into the operative position shown. The direction of flight of the warhead 40 with the active body 10 is indicated by an arrow F.

Nach Figur 3 ist der Wirkkörper 10, geringfügig modi­fiziert, (verwiesen wird u.a. auf die Gestalt der Einlage 64) einer Panzerabwehrrichtmine 60 integriert. Sie weist ein Abschußrohr 62 auf einer Dreibeinlafette 74 auf. Die nicht dargestellte zentrale Längsachse einer bekannten Zieleinrichtung 66 mit der erforderlichen Steuerelektronik verläuft der Längsachse A parallel. Ein Raketenmotor 70 ist über eine Anzündeinrichtung 68 initiierbar. Das Abschußrohr 62 wird mittels der Lafette 74 so aufgestellt, daß seine Längsachse auf einen Bereich gerichtet ist, in welchem zu bekämpfende gepanzerte Ziele erwartet werden. Hat die Zieleinrich­tung 66 ein solches Ziel identifiziert, wird über ein Signal die Anzündeinrichtung 68 initiiert und von ihr der Raketenmotor 70 gezündet. Der Wirkkörper 10 ver­läßt das Rohr 62 nach Wegsprengen dessen Deckels 76 in Richtung eines Pfeils F, und Stabilisierungsflügel 72 klappen aus ihrer in der Zeichnung dargestellten Ruhestellung in ihre Wirkstellung aus. Wegen der Funktionsabfolge wird auf die Beschreibung im Zusammen­hand mit Figur 1 verwiesen.According to FIG. 3, the active body 10, slightly modified, (reference is made, inter alia, to the shape of the insert 64) of an anti-tank mine 60. It has a launch tube 62 on a tripod mount 74. The central longitudinal axis (not shown) of a known target device 66 with the required control electronics runs parallel to the longitudinal axis A. A rocket engine 70 can be initiated via an ignition device 68. The launch tube 62 is set up by means of the mount 74 so that its longitudinal axis is directed towards an area in which armored targets to be combated are expected. If the target device 66 has identified such a target, the ignition device 68 is initiated via a signal and the rocket motor 70 is ignited by it. The active body 10 leaves the tube 62 after blasting away its cover 76 in the direction of an arrow F, and stabilizing wing 72 fold out of their rest position shown in the drawing into their operative position. Because of the sequence of functions, reference is made to the description in conjunction with FIG. 1.

In Figur 4 ist ein Panzerabwehrgeschoß 80 einer bekannten Munition für eine Kanone dargestellt. Mit Ausnahme einer Spitzkegeleinlage 84 der hinteren Ladung 12 ist auf eine Darstellung von Einzelheiten des integrierten Wirkkörpers 10 verzichtet. Das Rohr 15 ist als Stand­off-Rohr 82 ausgebildet und trägt vorderseitig einen bekannten und deshalb nicht näher dargestellten und zu beschreibenden Annäherungsünder 86. An einem Leitwerk­schaft 88 ist ein bekanntes feststehendes Stabilisierungs­leitwerk 90 angeordnet.FIG. 4 shows an anti-tank projectile 80 of a known ammunition for a cannon. With the exception of a pointed cone insert 84 of the rear cargo 12, details of the integrated active body 10 are not shown. The tube 15 is designed as a standoff tube 82 and carries on the front side a known approach nozzle 86, which is therefore not shown or described in detail. A known stabilizing stabilizer 90 is arranged on a tail boom 88.

Claims (6)

1. Wirkkörper zum Bekämpfen, insbesondere aktiv, gepanzer­ter Ziele mit zwei hintereinander angeordneten und durch hierfür vorgesehene Mittel initiierbaren La­dungen, wobei aus der vorderen Ladung im Ziel Wuchtwir­kung zum Verbrauchen einer zielseitigen Störeinrich­tung entfaltet wird, so daß anschließend ein Hohlla­dungsstrahl aus der hinteren Ladung ungestört zielwirk­sam werden kann, dadurch gekennzeich­net, daß der Wirkkörper ( 10 ) für den Hohlla­dungsstrahl einen vergleichsweise engen längsaxialen Kanal ( 16 ) aufweist, welcher mit einem Bereich der vorderen Ladung ( 18, 29 ) als Aufnahme dient.1. Active body for combating, in particular active, armored targets with two charges arranged one behind the other and initiatable by means provided for this purpose, wherein the front charge in the target develops a balancing effect to consume a target-side interfering device, so that subsequently a shaped charge jet from the rear charge is effective and undisturbed can be characterized in that the active body (10) for the shaped charge beam has a comparatively narrow longitudinal-axial channel (16) which serves as a receptacle with an area of the front charge (18, 29). 2. Wirkkörper nach Anspruch 1, gekennzeich­net durch seine Integrierung in einen mit ei­nem Zielsucher ( 52 ) ausgestatteten Gefechtskopf ( 40 ).2. Active body according to claim 1, characterized by its integration into a warhead (40) equipped with a seeker (52). 3. Wirkkörper nach Anspruch 1, gekennzeich­net, durch seine Integrierung in eine Panzer­abwehrrichtmine ( 60 ).3. The active body according to claim 1, characterized by its integration in an anti-tank directional mine (60). 4. Wirkkörper nach Anspruch 1, 2 oder 3, dadurch gekennzeichnet, daß die Mittel (24; 44) zum Initiieren der beiden Ladungen (12, 14; 64; 84 und 18, 20) und erforderliche Energiequellen (22) im Um­fangsbereich des Kanals (16) angeordnet sind.4. active body according to claim 1, 2 or 3, characterized in that the means (24; 44) for initiating the two charges (12, 14; 64; 84 and 18, 20) and required energy sources (22) in the peripheral region of the channel (16) are arranged. 5. Wirkkörper nach Anspruch 1, dadurch ge­kennzeichnet, daß der Kanal (16) im unter­kalibrigen Stand-off-Rohr (82) eines flügelstabilisier­ten Panzerabwehrgeschosses (80) angeordnet ist.5. active body according to claim 1, characterized in that the channel (16) in the sub-caliber stand-off tube (82) of a wing-stabilized anti-tank projectile (80) is arranged. 6. Wirkkörper nach einem der Ansprüche 1 bis 4, da­durch gekennzeichnet, daß die projektilbildende Einlage (20) der vorderen Ladung (18) eine durchschnittliche Dichte im Bereich zwischen etwa 16 und etwa 19 g/cm³ aufweist.6. Active body according to one of claims 1 to 4, characterized in that the projectile-forming insert (20) of the front load (18) has an average density in the range between about 16 and about 19 g / cm³.
EP87102607A 1986-06-18 1987-02-24 Ammunition, especially for fighting targets provided with a reactive armour Expired - Lifetime EP0249678B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AT87102607T ATE55831T1 (en) 1986-06-18 1987-02-24 MATTERS FOR COMBATTING, ESPECIALLY ACTIVELY ARMORED TARGETS.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19863619791 DE3619791A1 (en) 1986-06-18 1986-06-18 ACTIVITIES TO COMBAT, PARTICULARLY ACTIVE, ARMORED TARGETS
DE3619791 1986-06-18

Publications (4)

Publication Number Publication Date
EP0249678A2 true EP0249678A2 (en) 1987-12-23
EP0249678A3 EP0249678A3 (en) 1988-02-17
EP0249678B1 EP0249678B1 (en) 1990-08-22
EP0249678B2 EP0249678B2 (en) 1993-08-18

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ID=6302869

Family Applications (1)

Application Number Title Priority Date Filing Date
EP87102607A Expired - Lifetime EP0249678B2 (en) 1986-06-18 1987-02-24 Ammunition, especially for fighting targets provided with a reactive armour

Country Status (9)

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EP (1) EP0249678B2 (en)
JP (1) JPS62299700A (en)
AT (1) ATE55831T1 (en)
CA (1) CA1303905C (en)
DE (2) DE3619791A1 (en)
ES (1) ES2016939B3 (en)
IL (1) IL82794A0 (en)
NO (1) NO871542L (en)
ZA (1) ZA874366B (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0452541A2 (en) * 1990-04-14 1991-10-23 W.C. Heraeus GmbH Method of manufacturing hollow objects from tantalum
US5780766A (en) * 1996-04-30 1998-07-14 Diehl Gmbh & Co. Guided missile deployable as mortar projectile
DE4117871C1 (en) * 1991-05-31 1999-08-19 Diehl Stiftung & Co Hollow charge warhead used as a 'tandem' warhead for triggering reactive armor and then forming a hollow charge spike
RU193124U1 (en) * 2019-07-12 2019-10-15 Федеральное государственное бюджетное военное образовательное учреждение высшего образования "Черноморское высшее военно-морское ордена Красной Звезды училище имени П.С. Нахимова" Министерства обороны Российской Федерации Universal cumulative mine
EP3882563A1 (en) * 2020-03-17 2021-09-22 Diehl Defence GmbH & Co. KG Projectile, weapon assembly and method
DE102020113411A1 (en) 2020-05-18 2021-11-18 Rheinmetall Waffe Munition Gmbh Device of a defense technology effector

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3924087C1 (en) * 1989-07-20 1997-05-28 Rheinmetall Ind Ag Tandem battle head for combating active targets with two parts
DE3926711C2 (en) * 1989-08-12 1995-12-07 Rheinmetall Ind Gmbh Storey with interior
DE3934850C1 (en) * 1989-10-19 2000-09-28 Daimlerchrysler Aerospace Ag Tandem munitions head e.g. for long-range missile, has deformable structure for protecting main explosive charge upon detonation of initial explosive charge

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FR999974A (en) * 1946-02-11 1952-02-06 Soc Tech De Rech Ind Improvements to shaped charge machines
FR2310547A1 (en) * 1975-05-06 1976-12-03 Realisa Et Applic Tech Et Missile with secondary charge ahead of main charge - has small charge on nose cone positioned not to disturb main explosion
DE2829002A1 (en) * 1978-07-01 1984-03-29 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Multiple headed missile system - moves initial- and after-action bodies apart axially before detonation
EP0160118A2 (en) * 1983-10-07 1985-11-06 Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung Liner for a hollow or plane charge
EP0201433A1 (en) * 1985-05-10 1986-12-17 ETAT-FRANCAIS représenté par le DELEGUE GENERAL POUR L'ARMEMENT (DPAG) Armour-perforating projectile

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FR999974A (en) * 1946-02-11 1952-02-06 Soc Tech De Rech Ind Improvements to shaped charge machines
FR2310547A1 (en) * 1975-05-06 1976-12-03 Realisa Et Applic Tech Et Missile with secondary charge ahead of main charge - has small charge on nose cone positioned not to disturb main explosion
DE2829002A1 (en) * 1978-07-01 1984-03-29 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Multiple headed missile system - moves initial- and after-action bodies apart axially before detonation
EP0160118A2 (en) * 1983-10-07 1985-11-06 Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung Liner for a hollow or plane charge
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Cited By (9)

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EP0452541A2 (en) * 1990-04-14 1991-10-23 W.C. Heraeus GmbH Method of manufacturing hollow objects from tantalum
EP0452541A3 (en) * 1990-04-14 1992-01-02 W.C. Heraeus Gmbh Method of manufacturing hollow objects from tantalum
DE4117871C1 (en) * 1991-05-31 1999-08-19 Diehl Stiftung & Co Hollow charge warhead used as a 'tandem' warhead for triggering reactive armor and then forming a hollow charge spike
US5780766A (en) * 1996-04-30 1998-07-14 Diehl Gmbh & Co. Guided missile deployable as mortar projectile
DE19617221C2 (en) * 1996-04-30 1999-07-01 Diehl Stiftung & Co Steerable projectile that can be used as a mortar
RU193124U1 (en) * 2019-07-12 2019-10-15 Федеральное государственное бюджетное военное образовательное учреждение высшего образования "Черноморское высшее военно-морское ордена Красной Звезды училище имени П.С. Нахимова" Министерства обороны Российской Федерации Universal cumulative mine
EP3882563A1 (en) * 2020-03-17 2021-09-22 Diehl Defence GmbH & Co. KG Projectile, weapon assembly and method
DE102020113411A1 (en) 2020-05-18 2021-11-18 Rheinmetall Waffe Munition Gmbh Device of a defense technology effector
EP3913318A1 (en) 2020-05-18 2021-11-24 Rheinmetall Waffe Munition GmbH Device for a defence effector

Also Published As

Publication number Publication date
IL82794A0 (en) 1987-12-20
EP0249678B1 (en) 1990-08-22
ATE55831T1 (en) 1990-09-15
NO871542D0 (en) 1987-04-13
JPS62299700A (en) 1987-12-26
NO871542L (en) 1987-12-21
EP0249678B2 (en) 1993-08-18
ZA874366B (en) 1987-12-18
DE3764406D1 (en) 1990-09-27
DE3619791A1 (en) 1988-01-14
ES2016939B3 (en) 1990-12-16
CA1303905C (en) 1992-06-23
DE3619791C2 (en) 1988-04-14
EP0249678A3 (en) 1988-02-17

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