EP1223404B1 - Tête de combat - Google Patents
Tête de combat 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)
- Compositions Of Macromolecular Compounds (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Paper (AREA)
- Surgical Instruments (AREA)
- Supporting Of Heads In Record-Carrier Devices (AREA)
Claims (8)
- Tête de munition dotée d'une coque (2) de tête de munition qui enferme une charge explosive (5), et qui présente les caractéristiques suivantes:a) la charge explosive (5) comprend au moins deux charges partielles (7, 8-10) liées par matière synthétique et adjacentes l'une à l'autre dans la direction de l'axe longitudinal (6) de la tête de munition (1),b) la première charge partielle (7) tournée vers la pointe de la tête de munition (1) est constituée d'un explosif dont la vitesse de détonation est plus élevée que celle de la deuxième charge partielle (8-10) et est sélectionnée de telle sorte que lors de sa détonation, on obtienne une accélération axiale d'éclats (4) en métal lourd disposés sur le côté avant de la tête de munition (1),c) la deuxième charge partielle (8-10) est sélectionnée de manière à servir soit de charge d'accélération des éclats pour créer des éclats qui se propagent latéralement par rapport à la tête de munition (1) soit de charge qui crée une onde de pression qui agit latéralement par rapport à la tête de munition (1).
- Tête de munition selon la revendication 1, caractérisée en ce que la première charge partielle (7) est constituée de 70 à 90 % en volume d'octogène (HMX) et de 10 à 30 % en volume d'un liant en matière synthétique inerte.
- Tête de munition selon la revendication 2, caractérisée en ce que la première charge partielle est constituée de 90 % d'octogène et de 10 % d'un liant.
- Tête de munition selon l'une des revendications 1 à 3, caractérisée en ce que la deuxième charge partielle est constituée de 70 à 90 % en volume d'hexogène (RDX) et de 10 à 30 % en volume d'un liant en matière synthétique inerte.
- Tête de munition selon l'une des revendications 1 à 4, caractérisée en ce que la charge explosive (5) est constituée de quatre charges partielles (7, 8-10), la première charge partielle (7) voisine de la pointe de la tête de munition étant constituée d'octogène et les charges partielles (8-10) qui s'y raccordent étant constituées d'hexogène.
- Tête de munition selon l'une des revendications 1 à 5, caractérisée en ce que le liant en matière synthétique inerte est un polybutadiène à terminaisons hydroxyle (HTPB).
- Tête de munition selon l'une des revendications 1 à 6, caractérisée en ce qu'une poudre métallique est mélangée à la deuxième charge partielle (8-10).
- Tête de munition selon la revendication 7, caractérisée en ce que comme poudre métallique, on mélange une poudre d'aluminium à la deuxième charge partielle (8-10).
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10057673 | 2000-11-21 | ||
DE10057673A DE10057673A1 (de) | 2000-11-21 | 2000-11-21 | Gefechtskopf |
Publications (3)
Publication Number | Publication Date |
---|---|
EP1223404A2 EP1223404A2 (fr) | 2002-07-17 |
EP1223404A3 EP1223404A3 (fr) | 2003-04-09 |
EP1223404B1 true EP1223404B1 (fr) | 2005-11-16 |
Family
ID=7664066
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP01122815A Expired - Lifetime EP1223404B1 (fr) | 2000-11-21 | 2001-09-22 | Tête de combat |
Country Status (4)
Country | Link |
---|---|
US (1) | US6536351B2 (fr) |
EP (1) | EP1223404B1 (fr) |
DE (2) | DE10057673A1 (fr) |
NO (1) | NO320402B1 (fr) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
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 |
DE10248696A1 (de) * | 2002-10-18 | 2004-04-29 | Rheinmetall W & M Gmbh | Splittergeschoß |
FR2867469A1 (fr) * | 2004-03-15 | 2005-09-16 | Alliant Techsystems Inc | Compositions reactives contenant un metal, et leur procede de production |
EP2116807A2 (fr) | 2005-10-04 | 2009-11-11 | Alliant Techsystems Inc. | Projectiles améliorés à base de matériaux réactifs et procédés apparentés |
SE0502564L (sv) * | 2005-11-23 | 2007-05-22 | Bae Systems Bofors Ab | Sätt att framställa granat som ger splitter med lägre hastighet bakåt än granatens egen flyghastighet framåt |
FR2954309B1 (fr) * | 2009-12-21 | 2012-03-23 | Eurenco France | Explosif solide malleable et son obtention |
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 (de) * | 2019-01-24 | 2020-07-30 | Rheinmetall Denel Munition (Pty) Ltd. | Sprengladungsanordnung einer Rakete mit zwei unterschiedlichen Sprengstoffen |
Family Cites Families (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1236736A (en) * | 1916-03-17 | 1917-08-14 | Thomas S Miller | Explosive device. |
NL85184C (fr) * | 1955-08-17 | |||
NL263826A (fr) * | 1960-04-21 | |||
NO134882C (fr) * | 1973-05-18 | 1976-12-29 | Raufoss Ammunisjonsfabrikker | |
NO135445C (fr) * | 1973-05-18 | 1977-04-05 | Raufoss Ammunisjonsfabrikker | |
DE2452942C1 (de) * | 1974-11-08 | 1993-12-02 | Deutsche Aerospace | Kombiniertes Geschoß mit mehreren achsgleich hintereinander angeordneten Vor- und Nachgeschossen zur Bekämpfung gepanzerter Ziele |
US4003313A (en) * | 1975-06-10 | 1977-01-18 | The United States Of America As Represented By The Secretary Of The Army | Projectile |
NO137297C (no) * | 1976-07-01 | 1978-02-01 | Raufoss Ammunisjonsfabrikker | Prosjektil. |
SE7802634L (sv) * | 1978-03-08 | 1979-09-09 | Foerenade Fabriksverken | Projektil eller bomb med utskjutbara subprojektiler |
DE3224704A1 (de) * | 1982-07-02 | 1984-01-05 | Rheinmetall GmbH, 4000 Düsseldorf | Sprenggeschoss mit einer ein- oder mehrschichtigen aussenhuelle |
DE3336853A1 (de) * | 1983-10-11 | 1985-04-25 | Rheinmetall GmbH, 4000 Düsseldorf | Mehrzweckgefechtskopf |
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 (de) * | 1987-10-30 | 1989-05-11 | Diehl Gmbh & Co | Sprenggeschoss mit einem geschosskoerper |
DE3800455A1 (de) * | 1988-01-09 | 1989-07-20 | Dynamit Nobel Ag | Zuendelement, vorzugsweise mit langer verzoegerungszeit |
DE3834491A1 (de) | 1988-10-11 | 1990-04-12 | Messerschmitt Boelkow Blohm | Projektilbildende sprengladung |
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 (fr) * | 1990-07-17 | 1992-09-25 | Manurhin Defense | Projectile a effet destructif explosant par impact. |
US5191169A (en) * | 1991-12-23 | 1993-03-02 | Olin Corporation | Multiple EFP cluster module warhead |
FR2718842B1 (fr) * | 1994-04-15 | 1996-06-28 | Luchaire Defense Sa | Projectile destiné à agresser des cibles dures. |
US5542354A (en) * | 1995-07-20 | 1996-08-06 | Olin Corporation | Segmenting warhead projectile |
DE19648355A1 (de) * | 1996-11-22 | 1999-07-15 | Diehl Stiftung & Co | Artilleriegeschoß |
DE19722698C1 (de) * | 1997-05-30 | 1998-11-05 | Rheinmetall Ind Ag | Übungsgeschoß |
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/de not_active Withdrawn
-
2001
- 2001-09-22 DE DE50108077T patent/DE50108077D1/de not_active Expired - Lifetime
- 2001-09-22 EP EP01122815A patent/EP1223404B1/fr not_active Expired - Lifetime
- 2001-09-26 NO NO20014667A patent/NO320402B1/no 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 |
---|---|
NO20014667D0 (no) | 2001-09-26 |
US20020121215A1 (en) | 2002-09-05 |
NO320402B1 (no) | 2005-11-28 |
DE10057673A1 (de) | 2002-05-23 |
US6536351B2 (en) | 2003-03-25 |
NO20014667L (no) | 2002-05-22 |
EP1223404A3 (fr) | 2003-04-09 |
DE50108077D1 (de) | 2005-12-22 |
EP1223404A2 (fr) | 2002-07-17 |
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