EP1223404B1 - Warhead - Google Patents
Warhead Download PDFInfo
- 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
Links
Images
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 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
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
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
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
- 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)
- 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).
- 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.
- Warhead according to Claim 2, characterized in that the first charge element is composed of 90% of octogen and 10% of binding agent.
- 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.
- 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.
- Warhead according to one of Claims 1 to 5, characterized in that the inert plastic binding agent is hydroxyl-terminated polybutadien (HTPB).
- Warhead according to one of Claims 1 to 6, characterized in that a metal powder is mixed with the second charge element (8-10).
- Warhead according to Claim 7, characterized in that an aluminium powder is mixed with the second charge element (8-10) as the metal powder.
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)
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)
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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 |
-
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
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 |
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