EP0763705A2 - Secondary projectile for a tandem warhead - Google Patents
Secondary projectile for a tandem warhead Download PDFInfo
- Publication number
- EP0763705A2 EP0763705A2 EP96114074A EP96114074A EP0763705A2 EP 0763705 A2 EP0763705 A2 EP 0763705A2 EP 96114074 A EP96114074 A EP 96114074A EP 96114074 A EP96114074 A EP 96114074A EP 0763705 A2 EP0763705 A2 EP 0763705A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- charge
- igniter
- explosive
- active charge
- ignition
- 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
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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
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/56—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing discrete solid bodies
- F42B12/58—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles
- F42B12/62—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected parallel to the longitudinal axis of the projectile
- F42B12/625—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected parallel to the longitudinal axis of the projectile a single submissile arranged in a carrier missile for being launched or accelerated coaxially; Coaxial tandem arrangement of missiles which are active in the target one after the other
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- 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
- F42B12/32—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 the hull or case comprising a plurality of discrete bodies, e.g. steel balls, embedded therein or disposed around the explosive charge
Definitions
- the invention relates to a secondary floor for a tandem warhead according to the preamble of claim 1.
- a warhead with a tandem charge is known from EP-A1-0 583 642.
- the warhead has a main charge in the form of a shaped charge and a smaller-sized additional charge.
- the secondary projectile designed as a fragmentary projectile, penetrates the target through this channel and detonates behind the target with a splintering effect.
- the secondary storey is moved through the channel solely due to its inertia when the warhead hits.
- a separate acceleration charge for the secondary floor is not necessary.
- the fragmentation effect is caused by the explosive charge and the housing of the secondary floor. Due to the design of the secondary storey, the splintering effect is mainly in the direction of the shot, with only a small splintering effect occurring directly in the vicinity of the cover.
- an explosive charge and ogive-shaped construction splinters are also provided in the rear of the projectile.
- the rear explosive charge is ignited by a center-mounted detonator, which detonator separates the front explosive charge from the rear explosive charge.
- the front explosive charge is ignited via an ignition amplifier, while the rear explosive charge requires a transmission detonator and a downstream ignition transmitter.
- This ignition transmitter initiates the explosive charge on the rear side eccentrically, that is, on the outer edge of the explosive charge.
- This one-sided ignition of the Explosive charge designed as a hemisphere has a very different fragment density in the target area.
- the energy of the construction splinters varies accordingly.
- This transfer of the ignition should be structurally simple and inexpensive.
- Essential for the invention is the symmetrical and large-area ignition transmission to the rear active charge.
- the effectiveness of the rear active load corresponds to the front active load.
- the large-area ignition of the front active charge is an advantage.
- a functionally reliable transmission of the ignition is present in claim 1.
- the thin wall sections of the igniter, which separate the booster charge from explosives from the tongue-like explosive poles of the rear active charge, ensure the simultaneous ignition of the latter.
- a secondary storey 1 is mounted in a tube section 2 of a housing 3 of a tandem warhead 4, which is only partially drawn, and secured via a threaded connection 5.
- a steam protection is designated 6.
- the secondary storey 1 consists of two housing parts 10, 11 screwed together at 109, an igniter 12, a two-part explosive charge 13, 14 and fragmentary charges 15, 16 with casings 17, 18.
- the igniter 12 according to FIGS. 2 and 4 consists of an electrically controllable igniter 20 with a detonator 21, a thread 42 and an igniter 25 screwed to the igniter 20.
- the igniter 25 has a housing 26 with two flanges 22 and with a central pin 27 on the igniter side. In the housing 26 there are recesses 28 to 31 with an amplifier charge 32 made of explosives.
- the booster charge 32 is disc-shaped in the direction of the front active charge 13 and has a diameter 33 which almost corresponds to the diameter 34 of the front active charge 13.
- Two tongue-like explosive poles 50 are connected in one piece to the rear active charge 14. After the detonator 12 is arranged completely in a cylindrical metal sleeve 52 made of aluminum, the space required for the explosive poles 50 is created by corresponding recesses 55 on the housing part 11. The metal sleeve 52 completely encapsulates the rear active charge 14. An elastic element between the housing parts 10 is designated 110. One of the flanges 22 is pinned at 111.
- two thin-walled wall sections 59 are provided on the housing 26, so that the ignition from the booster charge 32 to the explosive poles 50 can take place - that is, in two ways.
- the cross sections of the explosive poles 50 are dimensioned such that the ignition to the explosive material block 19 of the rear active charge 14 is ensured.
- the tandem warhead 4 strikes a cover (not shown), a hollow channel is created in the cover by the shaped charge (also not shown).
- the secondary floor detached from the housing 3 penetrates through this penetration channel.
- the detonator 21 of the igniter 20 ignites the booster charge 32 on the basis of a correspondingly set time delay.
- the front active charge 13 is ignited and at the same time the explosive poles 50 are ignited, in which the housing 26 is penetrated in the overfire areas 60.
- the opposing explosive poles 50 conduct the explosive pulse symmetrically over a neck area 61 to the explosive material block 19.
- the simultaneous detonation of the front and rear active charges 13, 14 leads to both a front splinter distribution and a rear splinter distribution.
- the splinter distribution due to the rear active charge 14 is just large in the direction of the bullet channel and its surrounding field.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Air Bags (AREA)
- Ignition Installations For Internal Combustion Engines (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
Bei einem Sekundärgeschoß (1) eines Tandemgefechtskopfes (4) wird angestrebt, daß das Sekundärgeschoß (1) nach dem Durchdringen einer Deckung im unmittelbaren Bereich dieser Deckung eine große Splitterwirkung erzielt. Hierzu weist das Sekundärgeschoß (1) neben der vorderen Wirkladung (13) eine hintere Wirkladung (14) auf. Die Zündung sowohl der vorderen als auch der hinteren Wirkladung (13, 14) erfolgt durch einen einzigen Zünder (12, 20). Die Zündrichtung des Zünders (12, 20) geht in Richtung der vorderen Wirkladung (13). Aufgrund einer durch den Zünder (20) zündbaren, scheibenförmigen und mit einem großen Durchmesser (33) ausgestatteten Verstärkerladung (32) sowie aufgrund von zungenförmigen Sprengstoffpolen der hinteren Wirkladung (14) ist aufgrund eines radialen, umfangsseitig langgestreckten Überzündbereiches (60) die gleichzeitige Zündung der hinteren Wirkladung (14) sichergestellt. <IMAGE>In the case of a secondary storey (1) of a tandem warhead (4), the aim is for the secondary storey (1) to achieve a great splintering effect after penetrating a cover in the immediate area of this cover. For this purpose, the secondary storey (1) has a rear active charge (14) in addition to the front active charge (13). Both the front and the rear active charge (13, 14) are ignited by a single igniter (12, 20). The ignition direction of the igniter (12, 20) is in the direction of the front active charge (13). Because of the igniter (20) ignitable, disc-shaped and with a large diameter (33) equipped booster charge (32) and due to tongue-shaped explosive poles of the rear active charge (14), the simultaneous ignition of the is due to a radial, elongated ignition area (60) rear effective load (14) ensured. <IMAGE>
Description
Die Erfindung bezieht sich auf ein Sekundärgeschoß für einen Tandemgefechtskopf nach dem Oberbegriff des Anspruchs 1.The invention relates to a secondary floor for a tandem warhead according to the preamble of claim 1.
Beim Häuserkampf oder gegen sonstige Deckungen feindlicher Kräfte besteht ein Bedarf an kostengünstigen Waffen und Munition. Durch die EP-A1- 0 583 642 ist ein Gefechtskopf mit einer Tandemladung bekannt. Der Gefechtskopf weist eine als Hohlladung ausgebildete Hauptladung und eine kaliberkleinere Nachschußladung auf. Beim Zielaufprall des Gefechtskopfes schlägt die Hohlladung einen Kanal durch das Ziel. Das als Splittergeschoß ausgebildete Sekundärgeschoß dringt durch diesen Kanal in das Ziel ein und detoniert hinter dem Ziel mit Splitterwirkung. Das Sekundärgeschoß wird allein aufgrund seiner Massenträgheit beim Aufschlag des Gefechtskopfes durch den Kanal bewegt. Eine separate Beschleunigungsladung für das Sekundärgeschoß ist nicht erforderlich. Die Splitterwirkung wird durch die Sprengladung und durch das Gehäuse des Sekundärgeschosses bewirkt. Aufgrund der Ausbildung des Sekundärgeschosses liegt die Splitterwirkung hauptsächlich in Schußrichtung, wobei unmittelbar im Nahbereich der Deckung eine nur geringe Splitterwirkung auftritt.In house-to-house combat or against other coverings by enemy forces, there is a need for inexpensive weapons and ammunition. A warhead with a tandem charge is known from EP-A1-0 583 642. The warhead has a main charge in the form of a shaped charge and a smaller-sized additional charge. When the warhead hits the target, the shaped charge strikes a channel through the target. The secondary projectile, designed as a fragmentary projectile, penetrates the target through this channel and detonates behind the target with a splintering effect. The secondary storey is moved through the channel solely due to its inertia when the warhead hits. A separate acceleration charge for the secondary floor is not necessary. The fragmentation effect is caused by the explosive charge and the housing of the secondary floor. Due to the design of the secondary storey, the splintering effect is mainly in the direction of the shot, with only a small splintering effect occurring directly in the vicinity of the cover.
Zur Verbesserung der Splitterwirkung entgegen der Flugrichtung eines Geschosses ist es nach der DE-A1 39 41 445 vorgesehen, daß neben Splittern in einer Geschoßogive auch im Heck des Geschosses eine Sprengladung und ogivenförmig angeordnete Konstruktionsslpitter vorgesehen sind. Die Zündung der heckseitigen Sprengladung erfolgt von einem mittig gelagerten Zünder, wobei dieser Zünder die vordere Sprengladung von der hinteren Sprengladung trennt. Die vordere Sprengladung wird über einen Zündverstärker gezündet, während die hintere Sprengladung einen Übertragungsdetonator und einen nachgeordneten Zündübertrager benötigt. Dieser Zündübertrager initiert die heckseitige Sprengladung exzentrisch, also am äußeren Rand der Sprengladung. Durch diese einseitige Zündung der etwa als Halbkugel ausgebildeten Sprengladung liegt eine sehr unterschiedliche Splitterdichte im Zielraum vor. Außerdem variiert die Energie der Konstruktionssplitter entsprechend.To improve the splintering effect against the flight direction of a projectile, it is provided according to DE-A1 39 41 445 that, in addition to splinters in a storey arch, an explosive charge and ogive-shaped construction splinters are also provided in the rear of the projectile. The rear explosive charge is ignited by a center-mounted detonator, which detonator separates the front explosive charge from the rear explosive charge. The front explosive charge is ignited via an ignition amplifier, while the rear explosive charge requires a transmission detonator and a downstream ignition transmitter. This ignition transmitter initiates the explosive charge on the rear side eccentrically, that is, on the outer edge of the explosive charge. This one-sided ignition of the Explosive charge designed as a hemisphere has a very different fragment density in the target area. In addition, the energy of the construction splinters varies accordingly.
Es ist die Aufgabe der Erfindung, eine Übertragung der Zündung von einem Zünder mit nur einem Zünderausgang auf die vordere und die hintere Wirkladung eines Sekundärgeschosses vorzuschlagen, die zu einer gesteigerten Splitterwirkung führt. Diese Übertragung der Zündung soll konstruktiv einfach und kostengünstig sein.It is the object of the invention to propose a transmission of the ignition from a detonator with only one detonator output to the front and rear active charges of a secondary storey, which leads to an increased splintering effect. This transfer of the ignition should be structurally simple and inexpensive.
Die Erfindung löst diese Aufgabe entsprechend den kennzeichnenden Merkmalen des Anspruches 1.The invention solves this problem in accordance with the characterizing features of claim 1.
Vorteilhafte Weiterbildungen der Erfindung sind den Unteransprüchen zu entnehmen.Advantageous developments of the invention can be found in the subclaims.
Wesentlich für die Erfindung ist die symmetrische und großflächige Zündübertragung auf die hintere Wirkladung. Dadurch ist die Effektivität der hinteren Wirkladung entsprechend der vorderen Wirkladung.
Von Vorteil ist die großflächige Zündung der vorderen Wirkladung.Essential for the invention is the symmetrical and large-area ignition transmission to the rear active charge. As a result, the effectiveness of the rear active load corresponds to the front active load.
The large-area ignition of the front active charge is an advantage.
Ein funktionssichere Übertragung der Zündung liegt durch den Anspruch 1 vor. Die dünnen Wandabschnitte der Überzündvorrichtung, die die Verstärkerladung aus Sprengstoff von den zungenartigen Sprengstoffpolen der hinteren Wirkladung trennen, gewährleisten die gleichzeitige Zündung der letzteren.A functionally reliable transmission of the ignition is present in claim 1. The thin wall sections of the igniter, which separate the booster charge from explosives from the tongue-like explosive poles of the rear active charge, ensure the simultaneous ignition of the latter.
Konstruktive Details gehen aus den Ansprüchen 2 bis 7 hervor, wodurch eine kostengünstige und montagefreundliche Überzündvorrichtung ermöglicht wird.Structural details emerge from
Ein Ausführungsbeispiel der Erfindung ist in der Zeichnung dargestellt. Es zeigt:
- Fig. 1
- Einen Tandemgefechtskopf mit gestrichelt gezeichnetem Sekundärgeschoß in perspektivischer Darstellung,
- Fig. 2
- das Sekundärgeschoß im Längsschnitt mit einem Teil des Gehäuses des Tandemgefechtskopfes entsprechend einem Schnitt II - II nach Fig. 3,
- Fig. 3
- einen Querschnitt durch das Sekundärgeschoß entsprechend einem Schnitt III -III nach Fig. 2,
- Fig. 4
- den vollständigen Zünder nach Fig. 2 in perspektivischer Darstellung und
- Fig. 5
- eine Wirkladung in Perspektive nach Fig. 2.
- Fig. 1
- A tandem warhead with a dashed secondary floor in perspective,
- Fig. 2
- the secondary floor in longitudinal section with part of the housing of the tandem warhead according to a section II - II of FIG. 3,
- Fig. 3
- 3 shows a cross section through the secondary storey in accordance with a section III-III according to FIG. 2,
- Fig. 4
- the complete igniter of FIG. 2 in perspective and
- Fig. 5
- an active charge in perspective according to FIG. 2.
Entsprechend den Figuren 1 und 2 ist ein Sekundärgeschoß 1 in einem nur teilweise gezeichneten Rohrabschnitt 2 eines Gehäuses 3 eines Tandemgefechtskopfes 4 gelagert und über eine Gewindeverbindung 5 gesichert. Ein Schwadenschutz ist mit 6 bezeichnet.According to FIGS. 1 and 2, a secondary storey 1 is mounted in a
Das Sekundärgeschoß 1 besteht aus zwei bei 109 miteinander verschraubten Gehäuseteilen 10, 11, einem Zünder 12, einer zweiteiligen Sprengstoffladung 13, 14 und aus Splitterladungen 15, 16 mit Hüllen 17, 18.The secondary storey 1 consists of two
Der Zünder 12 nach den Figuren 2 und 4 besteht aus einem elektrisch ansteuerbaren Zünder 20 mit Detonator 21, einem Gewinde 42 und einer mit dem Zünder 20 verschrauben Überzündvorrichtung 25.The
Die Überzündvorrichtung 25 weist ein Gehäuse 26 mit zwei Flanschen 22 und mit einem zünderseitigen, zentralen Zapfen 27 auf. In dem Gehäuse 26 sind Ausnehmungen 28 bis 31 mit einer Verstärkerladung 32 aus Sprengstoff.The
Die Verstärkerladung 32 ist in Richtung auf die vordere Wirkladung 13 scheibenförmig ausgebildet und weist einen Durchmesser 33 auf, der nahezu dem Durchmesser 34 der vorderen Wirkladung 13 entspricht.The
Die hintere Wirkladung 14, siehe auch Fig. 5, nimmt den Zünder 20 in einer Bohrung 40 bis auf einen Ringabschnitt 41 auf In diesem Bereich liegt ein Gewindering 42 des Zünders 20, wobei dieser mit dem Gehäuse 26 über eine Gewindeverbindung 43 verschraubt ist.The rear
Einstückig mit der hinteren Wirkladung 14 verbunden sind zwei zungenartige Sprengstoffpole 50. Nachdem der Zünder 12 komplett in einer zylindrischen Metallhülse 52 aus Aluminium angeordnet ist, wird der für die Sprengstoffpole 50 benötigte Raum durch entsprechende Ausnehmungen 55 am Gehäuseteil 11 geschaffen. Die Metallhülse 52 kapselt die hintere Wirkladung 14 vollständig ab. Ein eleastisches Element zwischen den Gehäuseteilen 10 ist mit 110 bezeichnet. Einer der Flansche 22 ist bei 111 verstiftet.Two tongue-like
Im Überzündbereich 60 sind am Gehäuse 26 zwei dünnwandige Wandabschnitte 59 vorgesehen, so daß die Überzündung von der Verstärkerladung 32 zu den Sprengstoffpolen 50 - also auf zwei Wegen - erfolgen kann.In the
Die Querschnitte der Sprengstoffpole 50 sind so bemessen, daß die Durchzündung zum Sprengstoftblock 19 der hinteren Wirkladung 14 gewährleistet ist.The cross sections of the
Bei Aufschlag des Tandemgefechtskopfes 4 auf eine nicht dargestellte Deckung wird durch die ebenfalls nicht dargestellte Hohlladung ein Durchschußkanal in der Deckung erzeugt. Durch diesen Durchschußkanal dringt das vom Gehäuse 3 abgelöste Sekundärgeschoß. Aufgrund einer entsprechend eingestellten Zeitverzögerung zündet der Detonator 21 des Zünders 20 die Verstärkerladung 32. Ausgehend von der Verstärkerladung 32 wird die vordere Wirkladung 13 und gleichzeitig werden die Sprengstoftpole 50 gezündet, in dem in den Überzündbereichen 60 das Gehäuse 26 durchschlagen wird. Die einander gegenüberliegenden Sprengstoffpole 50 leiten dem Sprengimpuls symmetrisch über einen Halsbereich 61 zum Sprengstoftblock 19. Die gleichzeitige Detonation der vorderen und der hinteren Wirkladung 13, 14 führt sowohl zu einer vorderen Splitterverteilung als auch zu einer hinteren Splitterverteilung. Die Splitterverteilung aufgrund der hinteren Wirkladung 14 ist gerade in Richtung auf den Durchschußkanal und dessen Umgebungsfeldgroß.When the tandem warhead 4 strikes a cover (not shown), a hollow channel is created in the cover by the shaped charge (also not shown). The secondary floor detached from the
Claims (5)
dadurch gekennzeichnet,
daß eine durch den Zünder (12, 20) initierbare Verstärkerladung (32) aus Sprengstoff besteht und direkt an der vorderen Wirkladung (13) anliegt, andererseits die Verstärkerladung (32) durch dünne, überzündbare Wandabschnitte (59) eines Gehäuses (26) der Überzündvorrichtung (25) von wenigstens zwei zungenartigen Sprengstoffpolen (50) der hinteren Wirkladung (14) getrennt ist.Secondary storey (1) for a tandem warhead (4) with a front active charge (13), a rear active charge (14) and an igniter (12, 20) arranged in between, the ignition direction of which is aligned with the front active charge (13), with the ignition transmission after at the front via an amplifier charge (32) and at the rear through an igniter (25),
characterized,
that a booster charge (32) which can be initiated by the igniter (12, 20) consists of explosive and is present directly on the front active charge (13), and on the other hand the booster charge (32) through thin, ignitable wall sections (59) of a housing (26) of the igniter (25) is separated from at least two tongue-like explosive poles (50) of the rear active charge (14).
dadurch gekennzeichnet,
daß die Sprengstoffpole (50) mit der hinteren Wirkladung (14) einstückig ausgebildet sind und mit der Verstärkerladung (32) Überzündbereiche (60) bilden.Secondary storey according to claim 1,
characterized,
that the explosive poles (50) are formed in one piece with the rear active charge (14) and form over-ignition areas (60) with the booster charge (32).
dadurch gekennzeichnet,
daß die Sprengstoffpole 50 flächig an einer, den Zünder (12, 20) einhüllenden Metallhülse und zwar im Bereich des Gehäuses (26) der Überzündvorrichtung großflächig anliegen und in radialer Richtung durch das Gehäuseteil (11) der hinteren Wirkladung (14) begrenzt sind.Secondary storey according to claim 1,
characterized,
that the explosive poles 50 lie flat against a metal sleeve enveloping the detonator (12, 20), specifically in the area of the housing (26) of the igniter, and are delimited in the radial direction by the housing part (11) of the rear active charge (14).
dadurch gekennzeichnet,
daß das Gehäuseteil (11) entsprechend den Sprengstoffpolen Ausnehmungen (55) aufweist.Secondary storey according to claim 3,
characterized,
that the housing part (11) has recesses (55) corresponding to the explosive poles.
dadurch gekennzeichnet,
daß die Verstärkerladung (32) scheibenförmig ausgebildet ist und einen Durchmesser (33) aufweist, der nahezu dem Durchmesser (33) der vorderen Wirkladung (13) entspricht.Secondary storey according to claim 1,
characterized,
that the booster charge (32) is disc-shaped and has a diameter (33) which almost corresponds to the diameter (33) of the front active charge (13).
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19534211 | 1995-09-15 | ||
| DE19534211A DE19534211A1 (en) | 1995-09-15 | 1995-09-15 | Secondary storey for a tandem warhead |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| EP0763705A2 true EP0763705A2 (en) | 1997-03-19 |
| EP0763705A3 EP0763705A3 (en) | 1997-03-26 |
| EP0763705B1 EP0763705B1 (en) | 1998-12-02 |
Family
ID=7772239
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP96114074A Expired - Lifetime EP0763705B1 (en) | 1995-09-15 | 1996-09-03 | Secondary projectile for a tandem warhead |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US5594197A (en) |
| EP (1) | EP0763705B1 (en) |
| DE (2) | DE19534211A1 (en) |
| ES (1) | ES2127596T3 (en) |
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|---|---|---|---|---|
| US5686692A (en) * | 1996-09-30 | 1997-11-11 | The United States Of America As Represented By The Secretary Of The Navy | Single fuse follow-through grenade |
| DE19651170A1 (en) * | 1996-12-10 | 1998-06-18 | Diehl Gmbh & Co | Detonatorless, ballistic explosive device |
| SG82583A1 (en) * | 1997-04-23 | 2001-08-21 | Diehl Stiftung & Co | Fragmentation body for a fragmentation projectile |
| US6105505A (en) | 1998-06-17 | 2000-08-22 | Lockheed Martin Corporation | Hard target incendiary projectile |
| US6966265B2 (en) * | 2000-07-03 | 2005-11-22 | Bofors Defence Ab | Unit of ammunition with one or more warhead casings |
| SE519542C2 (en) * | 2000-07-03 | 2003-03-11 | Bofors Weapon Sys Ab | Ammunition unit with one or more action shells |
| US6962202B2 (en) * | 2003-01-09 | 2005-11-08 | Shell Oil Company | Casing conveyed well perforating apparatus and method |
| US7363862B2 (en) * | 2005-05-27 | 2008-04-29 | United States Of America As Represented By The Secretary Of The Army | Multi-purpose single initiated tandem warhead |
| US20070006768A1 (en) * | 2005-07-06 | 2007-01-11 | Rafael-Armament Development Authority Ltd. | Mushroom warhead |
| US7930978B1 (en) * | 2008-05-19 | 2011-04-26 | Raytheon Company | Forward firing fragmentation warhead |
| US8196513B1 (en) * | 2009-12-04 | 2012-06-12 | The United States Of America As Represented By The Secretary Of The Navy | Stand-off disrupter apparatus |
| KR101259734B1 (en) | 2012-01-20 | 2013-04-30 | 주식회사 한화 | Projectile with submunition |
| SE541548C2 (en) * | 2015-06-17 | 2019-10-29 | Bae Systems Bofors Ab | Procedure for pre-fragmentation of a combat part and pre-fragmented combat part |
| DE102019101762A1 (en) * | 2019-01-24 | 2020-07-30 | Rheinmetall Denel Munition (Pty) Ltd. | Explosive charge arrangement of a rocket with two different explosives |
| RU192887U1 (en) * | 2019-06-19 | 2019-10-04 | Федеральное Государственное Бюджетное Образовательное Учреждение Высшего Образования "Новосибирский Государственный Технический Университет" | High-explosive fragmentation warhead |
Citations (1)
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|---|---|---|---|---|
| DE3941445A1 (en) * | 1989-12-15 | 1991-06-20 | Diehl Gmbh & Co | Infantry projectile propels shot forward and backward - from similar hemispherical charges sepd. by transverse detonator assembly |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE317581C (en) * | ||||
| US94647A (en) * | 1869-09-07 | John d | ||
| DE2648137C2 (en) * | 1976-10-23 | 1984-04-12 | Dynamit Nobel Ag, 5210 Troisdorf | Propellant charge lighter for ammunition |
| GB2083175B (en) * | 1980-09-05 | 1984-08-08 | Gen Electric | Detonator assembly and explosive projectile |
| US4803928A (en) * | 1986-08-02 | 1989-02-14 | Stefan Kramer | Tandem charge projectile |
| DE3703773A1 (en) * | 1987-02-07 | 1988-08-18 | Diehl Gmbh & Co | Projectile, especially a mortar round |
| DE4225704A1 (en) * | 1992-08-04 | 1994-02-10 | Diehl Gmbh & Co | Warhead with a tandem charge |
-
1995
- 1995-09-15 DE DE19534211A patent/DE19534211A1/en not_active Withdrawn
- 1995-10-11 US US08/540,935 patent/US5594197A/en not_active Expired - Fee Related
-
1996
- 1996-09-03 EP EP96114074A patent/EP0763705B1/en not_active Expired - Lifetime
- 1996-09-03 DE DE59600895T patent/DE59600895D1/en not_active Expired - Fee Related
- 1996-09-03 ES ES96114074T patent/ES2127596T3/en not_active Expired - Lifetime
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3941445A1 (en) * | 1989-12-15 | 1991-06-20 | Diehl Gmbh & Co | Infantry projectile propels shot forward and backward - from similar hemispherical charges sepd. by transverse detonator assembly |
Also Published As
| Publication number | Publication date |
|---|---|
| DE59600895D1 (en) | 1999-01-14 |
| EP0763705A3 (en) | 1997-03-26 |
| DE19534211A1 (en) | 1997-03-20 |
| EP0763705B1 (en) | 1998-12-02 |
| US5594197A (en) | 1997-01-14 |
| ES2127596T3 (en) | 1999-04-16 |
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