EP1223404B1 - Warhead - Google Patents

Warhead Download PDF

Info

Publication number
EP1223404B1
EP1223404B1 EP01122815A EP01122815A EP1223404B1 EP 1223404 B1 EP1223404 B1 EP 1223404B1 EP 01122815 A EP01122815 A EP 01122815A EP 01122815 A EP01122815 A EP 01122815A EP 1223404 B1 EP1223404 B1 EP 1223404B1
Authority
EP
European Patent Office
Prior art keywords
charge
warhead
explosive
charge element
volume
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
Application number
EP01122815A
Other languages
German (de)
French (fr)
Other versions
EP1223404A3 (en
EP1223404A2 (en
Inventor
Jürgen Dr. Böcker
Paul Dr. Wanninger
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.)
Rheinmetall Waffe Munition GmbH
Original Assignee
Rheinmetall Waffe Munition GmbH
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 Rheinmetall Waffe Munition GmbH filed Critical Rheinmetall Waffe Munition GmbH
Publication of EP1223404A2 publication Critical patent/EP1223404A2/en
Publication of EP1223404A3 publication Critical patent/EP1223404A3/en
Application granted granted Critical
Publication of EP1223404B1 publication Critical patent/EP1223404B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

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
    • F42B12/20Projectiles, 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
    • F42B12/22Projectiles, 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 with fragmentation-hull construction

Definitions

  • the invention relates to a warhead with an explosive charge enclosing Warhead casing.
  • the charges consist of the known Warheads of a unitary material chosen such that the when the charge detonates, splinters generated in a particular direction (e.g. Flight direction) have a predetermined acceleration and angular distribution. Splinters flying in a different direction (e.g., perpendicular to the direction of flight) become Although then also correspondingly high speeds, although such a high acceleration this splitter is not necessary.
  • the invention is based on the object, a warhead of the aforementioned Kind to reveal, on the one hand in detonation of its explosive charge a high acceleration the flying in the direction of splitter causes and on the other hand a less acceleration of splinters flying sideways from the warhead caused and / or in the side of a relatively strong pressure wave is generated.
  • the invention is based essentially on the idea, not a uniform charge to arrange in the shell of the warhead, but at least two different To provide charges.
  • the points in the area of the top of the warhead arranged, e.g. from octogen (HMX) existing first partial charge a high Detonation on, around the arranged before this partial charge heavy metal splitter (preferably WSM-ball splitter) at detonation of the explosive charge very much fast forward (in the direction of flight) to accelerate.
  • this partial charge heavy metal splitter preferably WSM-ball splitter
  • This partial charge is only for one Acceleration of the lateral flying away e.g. Steel splitter required.
  • explosives can also be used as the second charge can be used, which only generates a strong lateral pressure wave.
  • the first partial charge of a mixture of 70-90 vol% octogen (HMX) and 10-30 vol% of an inert plastic binder e.g., hydroxyl terminated polybutadiene (HTPB)
  • an inert plastic binder e.g., hydroxyl terminated polybutadiene (HTPB)
  • RDX hexogen
  • both partial charges should use the same binders be used.
  • the second partial charge should be a metal powder (e.g., aluminum powder). blended to create a blast effect.
  • a metal powder e.g., aluminum powder
  • the warhead 1 is a ballistic warhead fireable from a gun referred to, which is to be used against bunkered positions and while sideways from the respective position vehicles should also destroy.
  • the warhead 1 comprises a warhead casing 2 made of steel, a front side of the warhead casing arranged proximity fuse 3, one adjoining the igniter Splinter plate 4 with heavy metal splinters (e.g., WSM balls) and an explosive charge 5.
  • the explosive charge 5 is made up of four, in the direction of the longitudinal axis 6 of the warhead Seen 1, arranged in succession partial charges 7-10 together.
  • the splitter plate 4 adjacent first partial charge 7 consists of a mixture of e.g. 90% HMX and 10% of a HTPB binder system and has a relatively high Guerney constant of 2830 m / s. This serves to make the WSM balls extra special to accelerate high in the direction of flight.
  • the partial charges 8-10 are used to generate and accelerate the destruction the warhead casing 2 resulting splinters flying away from the side of the warhead. For this much less expensive RDX charges are sufficient. Both Splinters may be natural or preformed structural shards act.
  • the RDX partial charges 8-10 can range from area to area have a different composition (e.g., charge 8: 85% RDX and 15% HTPB binder system; Charge 9: 90% RDX and 10% HTPB binder system and charge 10: 70% RDX, 10% HTPB binder system and 20% aluminum powder).
  • the warhead casing 2 becomes a certain one Share filled with the first partial charge 7.
  • the second mixture is poured on the first partial charge, etc.
  • the layered Infusion of various formulations based on the same polymer system then leads to a "tailored" effect (detonation speed) the charge.

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)
  • Supporting Of Heads In Record-Carrier Devices (AREA)
  • Paper (AREA)
  • Surgical Instruments (AREA)
  • Compositions Of Macromolecular Compounds (AREA)

Description

Die Erfindung betrifft einen Gefechtskopf mit einer eine Sprengladung umschließenden Gefechtskopfhülle.The invention relates to a warhead with an explosive charge enclosing Warhead casing.

Es ist seit langem bekannt, bei großkalibrigen Geschossen kunststoffgebundene Sprengladungen zu verwenden. Üblicherweise bestehen die Ladungen der bekannten Gefechtsköpfe aus einem einheitlichen Material, welches derart gewählt wird, daß die bei der Detonation der Ladung erzeugten Splitter in einer bestimmten Richtung (z.B. in Flugrichtung) eine vorgegebene Beschleunigung und Winkelverteilung aufweisen. Splitter, die in eine andere Richtung fliegen (z.B. senkrecht zur Flugrichtung), werden dann zwar ebenfalls entsprechend hoch beschleunigt, obwohl eine derartige hohe Beschleunigung dieser Splitter gar nicht erforderlich ist. In DE 196 48 355 wird eine Splittergranate mit einer (einzigen) Sprengladung beschrieben.It has long been known that plastic-bound in large-caliber projectiles To use explosive charges. Usually, the charges consist of the known Warheads of a unitary material chosen such that the when the charge detonates, splinters generated in a particular direction (e.g. Flight direction) have a predetermined acceleration and angular distribution. Splinters flying in a different direction (e.g., perpendicular to the direction of flight) become Although then also correspondingly high speeds, although such a high acceleration this splitter is not necessary. In DE 196 48 355 a fragmentation grenade with a (single) explosive charge described.

Aus der DE 38 34 491 A1 ist bereits eine projektilbildende Sprengladung mit einer Auskleidung bekannt, die eine Initialladung sowie mehrere unterschiedliche, in Richtung der Längsachse des Gefechtskopfes gesehen, hintereinander angeordnete Teilladungen aufweist, deren Detonationsgeschwindigkeiten von der Initialladung in Richtung der Auskleidung zunehmen. Durch eine derartige Anordnung unterschiedlicher Teilladungen wird erreicht, daß die Stachel- bzw. Projektilgeschwindigkeit eine größere Durchschlagsleistung besitzt als vergleichbare Gefechtsköpfe mit einer Ladung konstanter Detonationsgeschwindigkeit. Mit dem Aufbau von Gefechtsköpfen zur Beschleunigung von Splittern (Splittergeschosse) in unterschiedlichen Richtungen beschäftigt sich diese Patentanmeldung hingegen nicht. From DE 38 34 491 A1 is already a projectile-forming explosive charge with a Lining known, which is an initial charge and several different, in the direction Seen the longitudinal axis of the warhead, successively arranged partial charges whose detonation speeds from the initial charge in the direction to increase the lining. By such an arrangement different Partial charges is achieved that the spiked or Projektilgeschwindigkeit a larger Penetration performance is comparable to comparable warheads with a constant charge Detonation velocity. With the construction of warheads for acceleration of splinters (fragmentation projectiles) engaged in different directions However, this patent application is not.

Der Erfindung liegt die Aufgabe zugrunde, einen Gefechtskopf der eingangs erwähnten Art zu offenbaren, der einerseits bei Detonation seiner Sprengladung eine hohe Beschleunigung der in Flugrichtung fliegenden Splitter bewirkt und der andererseits eine geringere Beschleunigung der seitlich von dem Gefechtskopf wegfliegenden Splitter verursacht und/oder bei dem seitlich eine relativ starke Druckwelle erzeugt wird.The invention is based on the object, a warhead of the aforementioned Kind to reveal, on the one hand in detonation of its explosive charge a high acceleration the flying in the direction of splitter causes and on the other hand a less acceleration of splinters flying sideways from the warhead caused and / or in the side of a relatively strong pressure wave is generated.

Diese Aufgabe wird erfindungsgemäß durch die Merkmale des Anspruchs 1 gelöst. Weitere, besonders vorteilhafte Ausgestaltungen der Erfindung offenbaren die Unteransprüche.This object is achieved by the features of claim 1. Further, particularly advantageous embodiments of the invention disclose the dependent claims.

Die Erfindung beruht im wesentlichen auf dem Gedanken, nicht eine einheitliche Ladung in der Hülle des Gefechtskopfes anzuordnen, sondern mindestens zwei unterschiedliche Ladungen vorzusehen. Dabei weist die im Bereich der Spitze des Gefechtskopfes angeordnete, z.B. aus Octogen (HMX) bestehende erste Teilladung eine hohe Detonationsgeschwindigkeit auf, um die vor dieser Teilladung angeordneten Schwermetallsplitter (vorzugsweise WSM-Kugelsplitter) bei Detonation der Sprengladung sehr schnell nach vorne (in Flugrichtung) zu beschleunigen. Hingegen handelt es sich bei der zweiten, heckseitig sich an die erste Teilladung anschließenden Teilladung um eine weitaus billigere Ladung (z.B. RDX-Ladung). Diese Teilladung ist lediglich für eine Beschleunigung der seitlich wegfliegenden z.B. aus Stahl bestehenden Splitter erforderlich. Statt einer splitterbeschleunigenden Ladung kann als zweite Ladung auch Sprengstoff verwendet werden, der lediglich eine starke seitliche Druckwelle erzeugt.The invention is based essentially on the idea, not a uniform charge to arrange in the shell of the warhead, but at least two different To provide charges. In this case, the points in the area of the top of the warhead arranged, e.g. from octogen (HMX) existing first partial charge a high Detonation on, around the arranged before this partial charge heavy metal splitter (preferably WSM-ball splitter) at detonation of the explosive charge very much fast forward (in the direction of flight) to accelerate. On the other hand it concerns with the second, at the back of the first partial charge subsequent partial charge to a much cheaper charge (e.g., RDX charge). This partial charge is only for one Acceleration of the lateral flying away e.g. Steel splitter required. Instead of a fragment-accelerating charge, explosives can also be used as the second charge can be used, which only generates a strong lateral pressure wave.

Als vorteilhaft hat es sich erwiesen, wenn die erste Teilladung aus einer Mischung von 70-90 Vol% Octogen (HMX) und 10-30 Vol% eines inerten Kunststoff-Bindemittels (z.B. Hydroxylterminiertes Polybutadien (HTPB)) und die zweite Teilladung aus einer Mischung von 70-90 Vol % Hexogen (RDX) und ebenfalls 10-30 Vol% eines Kunststoff-Bindemittels besteht. Dabei sollten bei beiden Teilladungen die gleichen Bindemittel verwendet werden.It has proved to be advantageous if the first partial charge of a mixture of 70-90 vol% octogen (HMX) and 10-30 vol% of an inert plastic binder (e.g., hydroxyl terminated polybutadiene (HTPB)) and the second partial charge of one Mixture of 70-90% by volume hexogen (RDX) and also 10-30% by volume of a plastic binder consists. Both partial charges should use the same binders be used.

Vorzugsweise sollte der zweiten Teilladung ein Metallpulver (z.B. Aluminiumpulver) zugemischt sein, um einen Blasteffekt zu erzeugen. Preferably, the second partial charge should be a metal powder (e.g., aluminum powder). blended to create a blast effect.

Weitere Einzelheiten und Vorteile der Erfindung ergeben sich aus dem folgenden anhand einer Figur erläuterten Ausführungsbeispiel.Further details and advantages of the invention will become apparent from the following a figure illustrated embodiment.

In der Fig. ist mit 1 ein aus einem Geschütz abfeuerbarer ballistischer Gefechtskopf bezeichnet, der gegen verbunkerte Stellungen eingesetzt werden soll und dabei seitlich von der jeweiligen Stellung befindliche Fahrzeuge ebenfalls zerstören soll. Der Gefechtskopf 1 umfaßt eine Gefechtskopfhülle 2 aus Stahl, einen vorderseitig an der Gefechtskopfhülle angeordneten Annäherungszünder 3, eine sich an den Zünder anschließende Splitterplatte 4 mit Schwermetallsplittern (z.B. WSM-Kugeln) und eine Sprengladung 5. Die Sprengladung 5 setzt sich aus vier, in Richtung der Längsachse 6 des Gefechtskopfes 1 gesehen, hintereinander angeordneten Teilladungen 7-10 zusammen.In the figure, 1 is a ballistic warhead fireable from a gun referred to, which is to be used against bunkered positions and while sideways from the respective position vehicles should also destroy. The warhead 1 comprises a warhead casing 2 made of steel, a front side of the warhead casing arranged proximity fuse 3, one adjoining the igniter Splinter plate 4 with heavy metal splinters (e.g., WSM balls) and an explosive charge 5. The explosive charge 5 is made up of four, in the direction of the longitudinal axis 6 of the warhead Seen 1, arranged in succession partial charges 7-10 together.

Die der Splitterplatte 4 benachbarte erste Teilladung 7 besteht aus einer Mischung von z.B. 90 % HMX und 10 % eines HTPB Bindersystems und weist eine relativ hohe Guerney-Konstante von 2830 m/s auf. Diese dient dazu, die WSM-Kugeln besonders hoch in Flugrichtung zu beschleunigen.The splitter plate 4 adjacent first partial charge 7 consists of a mixture of e.g. 90% HMX and 10% of a HTPB binder system and has a relatively high Guerney constant of 2830 m / s. This serves to make the WSM balls extra special to accelerate high in the direction of flight.

Die Teilladungen 8-10 dienen zur Erzeugung und Beschleunigung der bei Zerstörung der Gefechtskopfhülle 2 entstehenden Splitter, die seitlich von dem Gefechtskopf wegfliegen. Hierzu reichen wesentlich kostengünstigere RDX-Ladungen aus. Bei den Splittern kann es sich um natürliche oder in der Hülle vorgeformte Konstuktionssplitter handeln.The partial charges 8-10 are used to generate and accelerate the destruction the warhead casing 2 resulting splinters flying away from the side of the warhead. For this much less expensive RDX charges are sufficient. Both Splinters may be natural or preformed structural shards act.

Um eine möglichst gute Anpassung an die gewünschte seitliche Splitterverteilung des Gefechtskopfes 1 zu erhalten, können die RDX-Teilladungen 8-10 von Bereich zu Bereich eine unterschiedliche Zusammensetzung aufweisen (z.B. Ladung 8: 85 % RDX und 15 % HTPB Bindersystem; Ladung 9: 90 % RDX und 10 % HTPB Bindersystem und Ladung 10: 70 % RDX, 10 % HTPB Bindersystem und 20 % Aluminiumpulver).To the best possible adaptation to the desired lateral splinter distribution of To get Warhead 1, the RDX partial charges 8-10 can range from area to area have a different composition (e.g., charge 8: 85% RDX and 15% HTPB binder system; Charge 9: 90% RDX and 10% HTPB binder system and charge 10: 70% RDX, 10% HTPB binder system and 20% aluminum powder).

Zur Laborierung des Gefechtskopfes 1 wird die Gefechtskopfhülle 2 zu einem bestimmten Anteil mit der ersten Teilladung 7 gefüllt. Während der Topfzeit dieser Mischung wird die zweite Mischung auf die erste Teilladung gegossen usw. Das schichtförmige Aufgießen von verschiedenen Formulierungen auf der Basis desselben Polymersystems führt dann zu einer "maßgeschneiderten" Wirkung (Detonationsgeschwindigkeit) der Ladung. For the purpose of the warhead 1, the warhead casing 2 becomes a certain one Share filled with the first partial charge 7. During the pot life of this mixture the second mixture is poured on the first partial charge, etc. The layered Infusion of various formulations based on the same polymer system then leads to a "tailored" effect (detonation speed) the charge.

BezugszeichenlisteLIST OF REFERENCE NUMBERS

11
Gefechtskopfwarhead
22
GefechtskopfhülleWarhead casing
33
Annäherungszünderproximity fuse
44
Splitterplatte, SchwermetallsplitterSplinter plate, heavy metal splinter
55
Sprengladungexplosive charge
66
Längsachselongitudinal axis
77
erste Teilladungfirst partial charge
8-108-10
Teilladungenpartial loads

Claims (8)

  1. Warhead having a warhead casing (2) which surrounds an explosive charge (5), having the following features:
    a) the explosive charge (5) comprises at least two plastic-bonded charge elements (7, 8-10) which are adjacent to one another, seen in the direction of the longitudinal axis (6) of the warhead (1);
    b) the first charge element (7), which faces the nose of the warhead (1) is composed of an explosive which has a higher detonation speed than the second charge element (8-10) and is chosen such that, when it detonates, heavy metal fragments (4), which are arranged on the front of the warhead (1), accelerate axially;
    c) the second charge element (8-10) is chosen such that it is used either as a fragment-accelerating charge in order to produce fragments flying away from the warhead (1) at the sides, or as a charge for producing a pressure wave which acts at the side of the warhead (1).
  2. Warhead according to Claim 1, characterized in that the first charge element (7) is composed of 70-90% by volume of octogen (HMX) and 10-30% by volume of an inert plastic binding agent.
  3. Warhead according to Claim 2, characterized in that the first charge element is composed of 90% of octogen and 10% of binding agent.
  4. Warhead according to one of Claims 1 to 3, characterized in that the second charge element is composed of 70-90% by volume of hexogen (RDX) and 10-30% by volume of an inert plastic binding agent.
  5. Warhead according to one of Claims 1 to 4, characterized in that the explosive charge (5) comprises four charge elements (7, 8-10), with the first charge element (7), which is adjacent to the nose of the warhead, being composed of octogen, and the adjacent charge elements (8-10) being composed of hexogen.
  6. Warhead according to one of Claims 1 to 5, characterized in that the inert plastic binding agent is hydroxyl-terminated polybutadien (HTPB).
  7. Warhead according to one of Claims 1 to 6, characterized in that a metal powder is mixed with the second charge element (8-10).
  8. Warhead according to Claim 7, characterized in that an aluminium powder is mixed with the second charge element (8-10) as the metal powder.
EP01122815A 2000-11-21 2001-09-22 Warhead Expired - Lifetime EP1223404B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE10057673A DE10057673A1 (en) 2000-11-21 2000-11-21 warhead
DE10057673 2000-11-21

Publications (3)

Publication Number Publication Date
EP1223404A2 EP1223404A2 (en) 2002-07-17
EP1223404A3 EP1223404A3 (en) 2003-04-09
EP1223404B1 true EP1223404B1 (en) 2005-11-16

Family

ID=7664066

Family Applications (1)

Application Number Title Priority Date Filing Date
EP01122815A Expired - Lifetime EP1223404B1 (en) 2000-11-21 2001-09-22 Warhead

Country Status (4)

Country Link
US (1) US6536351B2 (en)
EP (1) EP1223404B1 (en)
DE (2) DE10057673A1 (en)
NO (1) NO320402B1 (en)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7977420B2 (en) 2000-02-23 2011-07-12 Alliant Techsystems Inc. Reactive material compositions, shot shells including reactive materials, and a method of producing same
US7614348B2 (en) * 2006-08-29 2009-11-10 Alliant Techsystems Inc. Weapons and weapon components incorporating reactive materials
US20050199323A1 (en) 2004-03-15 2005-09-15 Nielson Daniel B. Reactive material enhanced munition compositions and projectiles containing same
USRE45899E1 (en) 2000-02-23 2016-02-23 Orbital Atk, Inc. Low temperature, extrudable, high density reactive materials
DE10248696A1 (en) * 2002-10-18 2004-04-29 Rheinmetall W & M Gmbh splitter floor
FR2867469A1 (en) 2004-03-15 2005-09-16 Alliant Techsystems Inc Reactive composition, useful in military and industrial explosives, comprises a metallic material defining a continuous phase and having an energetic material, which comprises oxidant and/or explosive of class 1.1
EP2116807A2 (en) 2005-10-04 2009-11-11 Alliant Techsystems Inc. Reactive Material Enhanced Projectiles And Related Methods
SE0502564L (en) 2005-11-23 2007-05-22 Bae Systems Bofors Ab Ways of producing grenades that give shrapnel at lower speed backwards than the grenade's own flight speed forward
FR2954309B1 (en) * 2009-12-21 2012-03-23 Eurenco France MALLEABLE SOLID EXPLOSIVE AND ITS OBTAINING
US9587921B2 (en) 2013-05-31 2017-03-07 Robert T. Faxon Warhead casings and methods of manufacture
US10260849B2 (en) * 2017-03-21 2019-04-16 The United States Of America As Represented By The Secretary Of The Army Off-on explosive warhead for high energy formulations with tailorable output performance
DE102019101762A1 (en) * 2019-01-24 2020-07-30 Rheinmetall Denel Munition (Pty) Ltd. Explosive charge arrangement of a rocket with two different explosives

Family Cites Families (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1236736A (en) * 1916-03-17 1917-08-14 Thomas S Miller Explosive device.
BE550308A (en) * 1955-08-17
NL263826A (en) * 1960-04-21
NO135445C (en) * 1973-05-18 1977-04-05 Raufoss Ammunisjonsfabrikker
NO134882C (en) * 1973-05-18 1976-12-29 Raufoss Ammunisjonsfabrikker
DE2452942C1 (en) * 1974-11-08 1993-12-02 Deutsche Aerospace Combined projectile with several parallely arranged behind and behind projectiles to combat armored targets
US4003313A (en) * 1975-06-10 1977-01-18 The United States Of America As Represented By The Secretary Of The Army Projectile
NO137297C (en) * 1976-07-01 1978-02-01 Raufoss Ammunisjonsfabrikker PROJECT.
SE7802634L (en) * 1978-03-08 1979-09-09 Foerenade Fabriksverken PROJECTILE OR BOMB WITH RELEASABLE SUB PROJECTILES
DE8218940U1 (en) * 1982-07-02 1986-10-16 Rheinmetall GmbH, 4000 Düsseldorf Explosive projectile with a single or multilayer outer shell
DE3336853A1 (en) * 1983-10-11 1985-04-25 Rheinmetall GmbH, 4000 Düsseldorf MULTIPURPOSE HEAD
US4625650A (en) * 1984-10-29 1986-12-02 Olin Corporation Multiple effect ammunition
US4648324A (en) * 1985-10-01 1987-03-10 Olin Corporation Projectile with enhanced target penetrating power
DE3736842A1 (en) * 1987-10-30 1989-05-11 Diehl Gmbh & Co BLASTING BULLET WITH A BULLET BODY
DE3800455A1 (en) * 1988-01-09 1989-07-20 Dynamit Nobel Ag IGNITION ELEMENT, PREFERABLY WITH A LONG DELAY TIME
DE3834491A1 (en) 1988-10-11 1990-04-12 Messerschmitt Boelkow Blohm Projectile-forming explosive charge
US5020439A (en) * 1989-05-05 1991-06-04 Olin Corporation Projectile having improved baseplug
US5164533A (en) * 1990-05-23 1992-11-17 Olin Corporation Method of assembling a pyrotechnically initiated projectile
FR2664970B1 (en) * 1990-07-17 1992-09-25 Manurhin Defense PROJECTILE HAVING A DESTRUCTIVE IMPACT EXPLOSING.
US5191169A (en) * 1991-12-23 1993-03-02 Olin Corporation Multiple EFP cluster module warhead
FR2718842B1 (en) * 1994-04-15 1996-06-28 Luchaire Defense Sa Projectile intended to attack hard targets.
US5542354A (en) * 1995-07-20 1996-08-06 Olin Corporation Segmenting warhead projectile
DE19648355A1 (en) * 1996-11-22 1999-07-15 Diehl Stiftung & Co Artillery shell for shrapnel production
DE19722698C1 (en) * 1997-05-30 1998-11-05 Rheinmetall Ind Ag Practice floor
US5996501A (en) * 1997-08-27 1999-12-07 The United States Of America As Represented By The Secretary Of The Air Force Blast and fragmentation enhancing explosive
US6135028A (en) * 1998-10-14 2000-10-24 The United States Of America As Represented By The Secretary Of The Navy Penetrating dual-mode warhead

Also Published As

Publication number Publication date
DE50108077D1 (en) 2005-12-22
NO320402B1 (en) 2005-11-28
NO20014667L (en) 2002-05-22
DE10057673A1 (en) 2002-05-23
US20020121215A1 (en) 2002-09-05
US6536351B2 (en) 2003-03-25
NO20014667D0 (en) 2001-09-26
EP1223404A3 (en) 2003-04-09
EP1223404A2 (en) 2002-07-17

Similar Documents

Publication Publication Date Title
DE2727970C2 (en)
EP1223404B1 (en) Warhead
DE2947165A1 (en) BULLET WITH KINETIC ENERGY
WO1998030863A1 (en) Projectile or warhead
DE69206711T2 (en) Low-sensitivity explosive ammunition element containing a two-component explosive charge and method of producing a splinter effect
DE19524726B4 (en) warhead
EP0113833B1 (en) Projectile with explosive and incendiary action
DE2919807C2 (en) Twist-stabilized sabot projectile to overcome a heterogeneous resistance
DE3235404A1 (en) Explosive charge
DE3625965A1 (en) WARM HEAD AND METHOD FOR PRODUCING THE WARM HEAD
DE8000028U1 (en) EXPLOSION CHARGE FROM TWO TANDEM ARRANGEMENTS
DE2557676A1 (en) Projectile contg. fragments of depleted uranium alloy - giving high penetrating power esp. armour piercing and incendiary action
EP0950870B1 (en) Combination type warhead
DE2414310C2 (en)
EP1286129B1 (en) Incendiary munition for a flight stabilised penetrating projectile
DE69213612T2 (en) BULLET STOCK WITH SPLIT EFFECT
DE10227002B4 (en) Decomposition charge for a warhead
DE3301150A1 (en) CHARGE
EP0881459B1 (en) Training projectile
DE3240310A1 (en) Armour-piercing conflagration projectile
EP3759417A1 (en) Projectile having a pyrotechnic explosive charge
DE19752102B4 (en) Armor piercing projectile with balancing effect
DE102004005042B4 (en) Universal KE bullet, especially for mid-caliber munitions
DE3401249A1 (en) Round for weapons with barrels, especially cannons, or a warhead
DE19633113B3 (en) Warhead for controlling airborne target e.g. tactical ballistic missiles, has fragments which are fixedly connected to covers of facing surfaces, where fragments and covers are made of layers having different shock wave impedances

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE TR

AX Request for extension of the european patent

Free format text: AL;LT;LV;MK;RO;SI

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE TR

AX Request for extension of the european patent

Extension state: AL LT LV MK RO SI

RIC1 Information provided on ipc code assigned before grant

Ipc: 7F 42B 12/32 A

Ipc: 7F 42B 12/22 B

17P Request for examination filed

Effective date: 20030228

AKX Designation fees paid

Designated state(s): DE FR GB SE

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: RHEINMETALL WAFFE MUNITION GMBH

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): DE FR GB SE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20051116

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REF Corresponds to:

Ref document number: 50108077

Country of ref document: DE

Date of ref document: 20051222

Kind code of ref document: P

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20060216

GBV Gb: ep patent (uk) treated as always having been void in accordance with gb section 77(7)/1977 [no translation filed]

Effective date: 20051116

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed

Effective date: 20060817

EN Fr: translation not filed
PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20070105

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20051116

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20140922

Year of fee payment: 14

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 50108077

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20160401