EP1223404A2 - Warhead - Google Patents
Warhead Download PDFInfo
- Publication number
- EP1223404A2 EP1223404A2 EP01122815A EP01122815A EP1223404A2 EP 1223404 A2 EP1223404 A2 EP 1223404A2 EP 01122815 A EP01122815 A EP 01122815A EP 01122815 A EP01122815 A EP 01122815A EP 1223404 A2 EP1223404 A2 EP 1223404A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- warhead
- charge
- partial
- load
- 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
Links
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/20—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
- F42B12/22—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type with fragmentation-hull construction
Definitions
- the invention relates to a warhead with an explosive charge surrounding Warhead casing.
- the charges usually exist in the known Warheads made of a uniform material, which is chosen such that the Splinters generated during the detonation of the charge in a certain direction (e.g. in Flight direction) have a predetermined acceleration and angular distribution. Splinters that fly in a different direction (e.g. perpendicular to the direction of flight) become then also accelerated accordingly high, although such a high acceleration this splinter is not necessary at all.
- the invention has for its object a warhead of the aforementioned Kind of revealing that on the one hand a high acceleration upon detonation of its explosive charge the splitter flying in the direction of flight and the other causes one less acceleration of the fragments flying away to the side of the warhead caused and / or in which a relatively strong pressure wave is generated laterally.
- the invention is essentially based on the idea, not a uniform charge to be placed in the shell of the warhead, but at least two different ones To provide charges. It points in the area of the top of the warhead arranged, e.g. first partial load consisting of octogen (HMX) high Detonation speed up to the heavy metal fragments arranged in front of this partial charge (preferably WSM bullet splinters) upon detonation of the explosive charge accelerate quickly forward (in the direction of flight). On the other hand, it is the second, rear load adjoining the first partial load by one much cheaper charge (e.g. RDX charge). This partial load is only for one Acceleration of the flying away e.g. steel splinters required. Instead of a fragment accelerating charge, explosives can also be used as a second charge can be used, which only generates a strong lateral pressure wave.
- HMX octogen
- the first partial load consists of a mixture of 70-90% by volume octogen (HMX) and 10-30% by volume of an inert plastic binder (e.g. hydroxyl-terminated polybutadiene (HTPB)) and the second partial charge from one Mixture of 70-90% by volume hexogen (RDX) and also 10-30% by volume of a plastic binder consists.
- HMX octogen
- HTPB hydroxyl-terminated polybutadiene
- the second part load should preferably be a metal powder (e.g. aluminum powder) be added to create a blast effect.
- a metal powder e.g. aluminum powder
- the warhead 1 is a ballistic warhead that can be fired from a gun designated, which is to be used against bunker positions and at the side vehicles from the respective position should also destroy.
- the warhead 1 comprises a warhead shell 2 made of steel, one on the front of the warhead shell arranged proximity detonator 3, an adjoining the detonator Splinter plate 4 with heavy metal splinters (e.g. WSM balls) and an explosive charge 5.
- the explosive charge 5 is composed of four, in the direction of the longitudinal axis 6 of the warhead 1 seen, consecutive partial loads 7-10 together.
- the first partial charge 7 adjacent to the splinter plate 4 consists of a mixture of e.g. 90% HMX and 10% of an HTPB binder system and has a relatively high Guerney constant of 2830 m / s. This serves to make the WSM balls special accelerate high in the direction of flight.
- the partial loads 8-10 are used to generate and accelerate the destruction the warhead shell 2 resulting splinters that fly away from the warhead laterally. Much cheaper RDX charges are sufficient for this. Both Splinters can be natural or preformed in the shell act.
- the RDX partial loads 8-10 can range from range to range 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 load 10: 70% RDX, 10% HTPB binder system and 20% aluminum powder).
- the warhead shell 2 is made into a specific one for laboratory use of the warhead 1 Part filled with the first partial load 7. During the pot life of this mixture the second mixture is poured onto the first part load, etc. The layered Pour on different formulations based on the same polymer system then leads to a "tailor-made” effect (detonation speed) the cargo.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Radar Systems Or Details Thereof (AREA)
- Compositions Of Macromolecular Compounds (AREA)
- Paper (AREA)
- Surgical Instruments (AREA)
- Supporting Of Heads In Record-Carrier Devices (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
Die Erfindung betrifft einen Gefechtskopf (1) mit einer eine Sprengladung (5) umschließenden Gefechtskopfhülle (2). Um zu erreichen, daß der Gefechtskopf (1) bei Detonation seiner Sprengladung (5) eine hohe Beschleunigung der in Flugrichtung fliegenden Splitter und eine geringere Beschleunigung der seitlich von dem Gefechtskopf wegfliegenden Splitter bewirkt und/oder eine relativ starke seitliche Druckwelle erzeugt, schlägt die Erfindung vor, entsprechend der bestimmungsgemäßen Verwendung des Gefechtskopfes (1) mindestens zwei unterschiedliche Ladungen (7,8-9) vorzusehen. Dabei weist die im Bereich der Spitze des Gefechtskopfes (1) angeordnete, z.B. aus Octogen (HMX) bestehende erste Teilladung (7) 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 (7) anschließenden Teilladung (8-10) 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. <IMAGE>The invention relates to a warhead (1) with a warhead shell (2) surrounding an explosive charge (5). In order to ensure that the warhead (1) detonates its explosive charge (5) causes a high acceleration of the fragments flying in the direction of flight and a lower acceleration of the fragments flying away from the warhead and / or generates a relatively strong lateral pressure wave, the invention proposes plan to provide at least two different charges (7,8-9) in accordance with the intended use of the warhead (1). The one located in the area of the tip of the warhead (1), e.g. the first partial charge (7) consisting of octogen (HMX) has a high detonation speed in order to accelerate the heavy metal fragments (preferably WSM ball fragments) arranged in front of this partial charge very quickly to the front (in the direction of flight) when the explosive charge is detonated. On the other hand, the second part load (8-10), which is connected to the rear of the first part load (7), is a much cheaper load (e.g. RDX load). This partial load is only for accelerating the e.g. steel splinters required. Instead of a charge accelerating the fragmentation, explosives can also be used as the second charge, which only generates a strong lateral pressure wave. <IMAGE>
Description
Die Erfindung betrifft einen Gefechtskopf mit einer eine Sprengladung umschließenden Gefechtskopfhülle.The invention relates to a warhead with an explosive charge surrounding 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.It has long been known that plastic-bound bullets are used for large-caliber bullets To use explosive charges. The charges usually exist in the known Warheads made of a uniform material, which is chosen such that the Splinters generated during the detonation of the charge in a certain direction (e.g. in Flight direction) have a predetermined acceleration and angular distribution. Splinters that fly in a different direction (e.g. perpendicular to the direction of flight) become then also accelerated accordingly high, although such a high acceleration this splinter is not necessary at all.
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. DE 38 34 491 A1 already describes a projectile-forming explosive charge with a Lining known to carry an initial charge as well as several different ones seen along the longitudinal axis of the warhead, partial loads arranged one behind the other has, whose detonation speeds from the initial charge in the direction of the lining. By such an arrangement different Partial loads are achieved that the spike or projectile speed is greater Penetration is more constant than comparable warheads with a charge Detonation velocity. With the construction of warheads for acceleration of fragments (fragments) in different directions this patent application, however, does 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 has for its object a warhead of the aforementioned Kind of revealing that on the one hand a high acceleration upon detonation of its explosive charge the splitter flying in the direction of flight and the other causes one less acceleration of the fragments flying away to the side of the warhead caused and / or in which a relatively strong pressure wave is generated laterally.
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 configurations of the invention are disclosed in the subclaims.
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 essentially based on the idea, not a uniform charge to be placed in the shell of the warhead, but at least two different ones To provide charges. It points in the area of the top of the warhead arranged, e.g. first partial load consisting of octogen (HMX) high Detonation speed up to the heavy metal fragments arranged in front of this partial charge (preferably WSM bullet splinters) upon detonation of the explosive charge accelerate quickly forward (in the direction of flight). On the other hand, it is the second, rear load adjoining the first partial load by one much cheaper charge (e.g. RDX charge). This partial load is only for one Acceleration of the flying away e.g. steel splinters required. Instead of a fragment accelerating charge, explosives can also be used as a 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 proven to be advantageous if the first partial load consists of a mixture of 70-90% by volume octogen (HMX) and 10-30% by volume of an inert plastic binder (e.g. hydroxyl-terminated polybutadiene (HTPB)) and the second partial charge from one Mixture of 70-90% by volume hexogen (RDX) and also 10-30% by volume of a plastic binder consists. The same binders should be used for both partial loads be used.
Vorzugsweise sollte der zweiten Teilladung ein Metallpulver (z.B. Aluminiumpulver) zugemischt sein, um einen Blasteffekt zu erzeugen. The second part load should preferably be a metal powder (e.g. aluminum powder) be added 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 that can be fired from a gun
designated, which is to be used against bunker positions and at the side
vehicles from the respective position should also destroy. The warhead
1 comprises a
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 first
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 loads 8-10 are used to generate and accelerate the destruction
the
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).In order to adapt to the desired lateral splinter distribution of the To obtain warhead 1, the RDX partial loads 8-10 can range from range to range 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 load 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. The
- 11
- Gefechtskopfwarhead
- 22
- GefechtskopfhülleWarhead casing
- 33
- Annäherungszünderproximity fuse
- 44
- Splitterplatte, SchwermetallsplitterSplinter plate, heavy metal splinters
- 55
- Sprengladungexplosive charge
- 66
- Längsachselongitudinal axis
- 77
- erste Teilladungfirst part load
- 8-108-10
- Teilladungenpartial loads
Claims (8)
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 true EP1223404A2 (en) | 2002-07-17 |
EP1223404A3 EP1223404A3 (en) | 2003-04-09 |
EP1223404B1 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)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
USRE45899E1 (en) | 2000-02-23 | 2016-02-23 | Orbital Atk, Inc. | Low temperature, extrudable, high density reactive materials |
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 |
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 |
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 |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3834491A1 (en) | 1988-10-11 | 1990-04-12 | Messerschmitt Boelkow Blohm | Projectile-forming explosive charge |
Family Cites Families (25)
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US1236736A (en) * | 1916-03-17 | 1917-08-14 | Thomas S Miller | Explosive device. |
LU34581A1 (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 |
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 |
-
2000
- 2000-11-21 DE DE10057673A patent/DE10057673A1/en not_active Withdrawn
-
2001
- 2001-09-22 DE DE50108077T patent/DE50108077D1/en not_active Expired - Lifetime
- 2001-09-22 EP EP01122815A patent/EP1223404B1/en not_active Expired - Lifetime
- 2001-09-26 NO NO20014667A patent/NO320402B1/en not_active IP Right Cessation
- 2001-11-21 US US09/989,755 patent/US6536351B2/en not_active Expired - Lifetime
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3834491A1 (en) | 1988-10-11 | 1990-04-12 | Messerschmitt Boelkow Blohm | Projectile-forming explosive charge |
Also Published As
Publication number | Publication date |
---|---|
DE10057673A1 (en) | 2002-05-23 |
EP1223404A3 (en) | 2003-04-09 |
US20020121215A1 (en) | 2002-09-05 |
NO20014667D0 (en) | 2001-09-26 |
NO20014667L (en) | 2002-05-22 |
EP1223404B1 (en) | 2005-11-16 |
NO320402B1 (en) | 2005-11-28 |
US6536351B2 (en) | 2003-03-25 |
DE50108077D1 (en) | 2005-12-22 |
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