EP0433544B1 - Fragmentation missile - Google Patents

Fragmentation missile Download PDF

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Publication number
EP0433544B1
EP0433544B1 EP90114529A EP90114529A EP0433544B1 EP 0433544 B1 EP0433544 B1 EP 0433544B1 EP 90114529 A EP90114529 A EP 90114529A EP 90114529 A EP90114529 A EP 90114529A EP 0433544 B1 EP0433544 B1 EP 0433544B1
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EP
European Patent Office
Prior art keywords
casing
projectile
explosive
shell
fragmentation
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Expired - Lifetime
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EP90114529A
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German (de)
French (fr)
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EP0433544A1 (en
Inventor
Hendrik Lips
Herbert Weisshaupt
Hans Orth
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Rheinmetall Industrie AG
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Rheinmetall Industrie AG
Rheinmetall GmbH
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Publication of EP0433544A1 publication Critical patent/EP0433544A1/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/36Projectiles, 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
    • F42B12/44Projectiles, 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 of incendiary type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/20Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
    • F42B12/22Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type with fragmentation-hull construction
    • F42B12/24Projectiles, 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 with grooves, recesses or other wall weakenings

Definitions

  • the invention relates to a fragmentary projectile as defined by the preamble of claim 1.
  • Such fragments are known for example from US-A-3,566,794.
  • a plurality of casings abutting one another are arranged around the centrally arranged explosive, each of which has V-shaped predetermined breaking points in order to produce the largest possible number of fragments.
  • the predetermined breaking points of the casing closest to the explosive are provided with the predetermined breaking points on the explosive side.
  • a multi-shell fragmentary projectile in which the shell closest to the explosive has V-shaped grooves on the explosive side which do not change the wall thickness of the shell.
  • the grooves are designed such that the corresponding groove walls act like local shaped charge inserts. This means that the V-shaped groove walls on the explosives side directly from explosives must be surrounded and must therefore be arranged in any case on the side of the shell facing the explosives.
  • the local shaped charges act on the outer shell, which then first tears along those areas which lie opposite the V-shaped grooves.
  • US-A-4,106,411 discloses a fragmentary projectile which has several casings with structural zones. Areas are filled with explosives between the inner casings and areas with a fire mass between the outer casings. In these explosive projectiles too, the fire mass reaches the target practically simultaneously with the shell fragments, so that ignition of the combustible liquid of a target cannot be ensured.
  • a splinter floor is shown in Fig. 2, which also consists of several shell casings. In this case, however, the splinter shell and the zirconium shell causing the fire effect are separate units.
  • a disadvantage of this invention is the fact that a large number of undefined fragments arise. There is no reproducible splinter distribution.
  • the object of the present invention is, based on US 3,566,794, to further develop a splinter projectile in such a way that the actual splinter casing is particularly easy to manufacture, and that in addition a desired fire effect, e.g. B. when fighting aircraft tanks.
  • the invention is therefore based on the idea of generating an optimization of the splintering and fire effects in that the structural zones of the inner shell consist of areas of smaller wall thickness than the parts of the shell surrounding the structural zones.
  • the wall thicknesses, casing materials and the number of casings determine the shape and mass distribution of the fragments and - depending on the intended use - can be optimally adapted to the target requirements.
  • the fragmentary floor consisting of several shell casings is designated by 1.
  • the shell is composed of the outer shell 2 and 3 and the inner shell 4.
  • Structural zones 7 are located in the inner shell 4 on the side facing away from the explosive 5. These structural zones 7 are selected such that the remaining wall thickness of the shell 4 at these points is less than the wall thickness of the parts of the shell 4 surrounding the structural zones.
  • FIG. 4 and 4a and 5 and 5a two further exemplary embodiments of the inner shell 4 ', 4' 'with structural zones 7', 7 '' are shown.
  • 4 shows a top view
  • FIG. 4a shows a cross section of the inner shell 4 'with a structure zone distribution which is selected such that the parts of the shell 4' surrounding the structure zones have an approximately rectangular shape.
  • 5 shows the top view of a projectile casing 4 ′′ with structural zones 7 ′′, which have a sawtooth-shaped course (see FIG. 5a).
  • FIG. 6 shows the inner shell 4, the structural zones 7 and the adjacent outer shell 3.
  • the resulting shock wave pulse is locally coupled into the casing 3 at the contact points 8.
  • the corresponding waves are reflected at the transition of the material of the casing 4 to the air.
  • the energy coupled in at the contact points 8 accelerates partial regions of the outer shell 3 or induces voltage gradients in this shell. This leads to the formation of splinters whose geometry corresponds to the pattern made on the inner shell.
  • the shape, size and number of chips as well as the speed of the chips can be adjusted by suitable structuring of the inner shell 4.

Description

Die Erfindung betrifft ein Splittergeschoß, wie es durch den Gattungsbegriff des Anspruchs 1 definiert ist.The invention relates to a fragmentary projectile as defined by the preamble of claim 1.

Derartige Splittergeschosse sind beispielsweise aus der US-A-3,566,794 bekannt. Bei diesen Geschossen sind um den zentral angeordneten Sprengstoff mehrere aneinander anliegende Hüllen angeordnet, die jeweils V-förmige Sollbruchstellen aufweisen, um eine möglichst große Anzahl von Splittern zu erzeugen. Dabei sind die Sollbruchstellen der dem Sprengstoff nächsten Hülle sprengstoffseitig mit den Sollbruchstellen versehen.Such fragments are known for example from US-A-3,566,794. In the case of these projectiles, a plurality of casings abutting one another are arranged around the centrally arranged explosive, each of which has V-shaped predetermined breaking points in order to produce the largest possible number of fragments. The predetermined breaking points of the casing closest to the explosive are provided with the predetermined breaking points on the explosive side.

Abgesehen davon, daß diese bekannten Splittergeschosse mehrere relativ aufwendige Hüllenstrukturen erfordern, ergeben sich bei Verwendung dieser Geschosse besonders dann Probleme, wenn die Hüllen mit Brandmassen versehen werden, um eine entzündbare Flüssigkeit (z.B. eines Flugzeugtanks) zu entzünden. Denn häufig erlöscht die Brandmasse beim Eintauchen der entsprechenden Splitter in die Flüssigkeit.In addition to the fact that these known fragmentary projectiles require several relatively complex casing structures, problems arise when using these projectiles, in particular if the casings are provided with fire masses in order to ignite an inflammable liquid (e.g. an aircraft tank). Because the fire mass often extinguishes when the corresponding splinters are immersed in the liquid.

Aus der US-A-3,000,309 ist ein aus mehreren Hüllen bestehendes Splittergeschoß bekannt, bei dem die dem Sprengstoff nächste Hülle sprengstoffseitig V-förmige Nuten aufweist, welche die Wandstärke der Hülle nicht verändern. Die Nuten sind dabei derart ausgebildet, daß die entsprechenden Nutenwände wie lokale Hohlladungseinlagen wirken. Dieses bedeutet, daß die V-förmigen Nutenwände sprengstoffseitig direkt von Sprengstoff umgeben sein müssen und somit in jedem Fall auf der dem Sprengstoff zugewandten Seite der Hülle anzuordnen sind. Bei der Detonation wirken die lokalen Hohlladungen auf die Außenhülle, die dann zunächst entlang derjenigen Bereiche reißt, die den V-förmigen Nuten gegenüber liegen.From US-A-3,000,309 a multi-shell fragmentary projectile is known, in which the shell closest to the explosive has V-shaped grooves on the explosive side which do not change the wall thickness of the shell. The grooves are designed such that the corresponding groove walls act like local shaped charge inserts. This means that the V-shaped groove walls on the explosives side directly from explosives must be surrounded and must therefore be arranged in any case on the side of the shell facing the explosives. During the detonation, the local shaped charges act on the outer shell, which then first tears along those areas which lie opposite the V-shaped grooves.

Nachteilig bei diesem bekannten Geschoß ist ebenfalls, daß eine aufwendige und damit teure Hüllenstruktur erforderlich ist. Außerdem läßt sich bei diesem Geschoß keine Brandmasse auf der dem Sprengstoff zugewandten Hüllenwand aufbringen, weil sonst die Funktion der V-förmigen Nuten als Hohlladung verloren gehen würde.Another disadvantage of this known projectile is that a complex and therefore expensive casing structure is required. In addition, no fire can be applied to the shell wall facing the explosive in this projectile, because otherwise the function of the V-shaped grooves as a shaped charge would be lost.

Aus der US-A-4.381,692 ist ferner bekannt, eine mit Kerben versehene Brandmasse auf der Innenseite der Geschoßhülle von Splittergeschossen anzuordnen. Mit einer derartigen Anordnung ist allerdings der Nachteil verbunden, daß die Brandmasse praktisch gleichzeitig mit den Hüllensplittern in das Ziel gelangt, was vermieden werden soll, weil die Splitter zusammen mit den Brandmassen in die entzündbare Flüssigkeit eintauchen und häufig sofort erlöschen.From US-A-4,381,692 it is also known to arrange a notched fire mass on the inside of the shell of fragmentary projectiles. With such an arrangement, however, there is the disadvantage that the fire mass reaches the target practically simultaneously with the shell fragments, which should be avoided because the splinters are immersed in the flammable liquid together with the fire masses and often go out immediately.

Die US-A-4,106,411 offenbart ein Splittergeschoß, welches mehrere Hüllen mit Strukturzonen besitzt. Dabei sind zwischen den inneren Hüllen Bereiche mit Sprengstoff und zwischen den äußeren Hüllen Bereiche mit einer Brandmasse ausgefüllt. Auch bei diesen Sprenggeschossen gelangt die Brandmasse praktisch gleichzeitig mit den Hüllensplittern in das Ziel, so daß eine Entzündung der brennbaren Flüssigkeit eines Zieles nicht sichergestellt werden kann.US-A-4,106,411 discloses a fragmentary projectile which has several casings with structural zones. Areas are filled with explosives between the inner casings and areas with a fire mass between the outer casings. In these explosive projectiles too, the fire mass reaches the target practically simultaneously with the shell fragments, so that ignition of the combustible liquid of a target cannot be ensured.

In der DE-B-23 39 386 wird in Fig. 2 ein Splittergeschoß dargestellt, welches ebenfalls aus mehreren Geschoßhüllen besteht. Allerdings sind in diesem Fall die Splitterhülle und die die Brandwirkung verursachende Zirkoniumhülle getrennte Einheiten.In DE-B-23 39 386 a splinter floor is shown in Fig. 2, which also consists of several shell casings. In this case, however, the splinter shell and the zirconium shell causing the fire effect are separate units.

Zum einen besteht bei diesen bekannten Geschossen der Nachteil, daß keine gerichtete Splitterwirkung gegeben ist, sondern daß die Splitterverteilung annähernd zylindersymmetrisch ist. Zum anderen ist die Wirksamkeit der leichten Zirkoniumsplitter, insbesondere bei größeren Zielentfernungen, sehr fraglich, da die Penetrationswirkung dieser Splitter gering ist.On the one hand, there is the disadvantage with these known projectiles that there is no directional splintering effect, but that the splinter distribution is approximately cylinder-symmetrical. On the other hand, the effectiveness of the light zirconium splinters is very questionable, especially with larger target distances, since the penetration effect of these splinters is low.

Aus der US-A-4,089,267 ist ein Splittergeschoß bekannt, bei dem zur Erhöhung der Splitteranzahl der Sprengstoff von zwei Hüllen umgeben ist. Zwischen den beiden Hüllen muß ein Spalt bestehen, der mit einem Material geringer Dichte (Luft, Schaum) ausgefüllt wird. Nach der Zündung des Sprengstoffes drückt die Innenhülle schlagartig auf die Außenhülle, so daß es zu einer relativ hohen Splitterbildung kommt.From US-A-4,089,267 a fragmentary projectile is known in which the explosive is surrounded by two shells to increase the number of fragments. There must be a gap between the two shells, which is filled with a low-density material (air, foam). After the explosive is detonated, the inner shell suddenly presses on the outer shell, so that there is a relatively high formation of fragments.

Nachteilig bei dieser Erfindung ist die Tatsache, daß eine große Anzahl undefinierter Splitter entsteht. Es ergibt sich keine reproduzierbare Splitterverteilung.A disadvantage of this invention is the fact that a large number of undefined fragments arise. There is no reproducible splinter distribution.

Die Aufgabe der vorliegenden Erfindung besteht darin, ausgehend von der US 3,566,794, ein Splittergeschoß so weiterzuentwickeln, daß die eigentliche Splitterhülle besonders einfach zu fertigen ist, und daß sich zusätzlich eine erwünschte Brandwirkung, z. B. beim Bekämpfen von Flugzeugtanks, ergibt.The object of the present invention is, based on US 3,566,794, to further develop a splinter projectile in such a way that the actual splinter casing is particularly easy to manufacture, and that in addition a desired fire effect, e.g. B. when fighting aircraft tanks.

Diese Aufgabe wird erfindungsgemäß durch die Merkmale des kennzeichnenden Teiles des Anspruchs 1 gelöst.This object is achieved by the features of the characterizing part of claim 1.

Weitere besonders vorteilhafte Ausgestaltungen ergeben sich aus den Unteransprüchen.Further particularly advantageous configurations result from the subclaims.

Der Erfindung liegt also der Gedanke zugrunde, eine Optimierung der Splitter- und Brandwirkung dadurch zu erzeugen, daß die Strukturzonen der Innenhülle aus Bereichen geringerer Wandstärke bestehen, als die die Strukturzonen umgebenden Teile der Hülle. Die Wanddicken, Hüllenwerkstoffe und die Hüllenanzahl bestimmen die Gestalt und Massenverteilung der Splitter und können - je nach Verwendungszweck - optimal an die Zielanforderungen angepaßt werden.The invention is therefore based on the idea of generating an optimization of the splintering and fire effects in that the structural zones of the inner shell consist of areas of smaller wall thickness than the parts of the shell surrounding the structural zones. The wall thicknesses, casing materials and the number of casings determine the shape and mass distribution of the fragments and - depending on the intended use - can be optimally adapted to the target requirements.

Der Nachteil bei herkömmlichen Splittergefechtsköpfen, bei denen die pyrophore Brandmasse mit den Splittern ins Ziel gebracht wird, und bei denen die relativ kleinen Splitter sofort in die zu entzündende Flüssigkeit eintauchen und dadurch erlöschen, ist bei der vorliegenden Erfindung nicht gegeben. Vielmehr fliegen durch Verwendung der Mehrfachhülle mehrere Splitter gestaffelt vor den mit der Brandmasse versehenen Splittern in das Ziel und bereiten den Treibstoff für eine optimale Entzündung durch die beim Eintritt entstehende Kavitationsblase oder durch Auslaufen vor.The disadvantage with conventional splinter warheads, in which the pyrophoric fire mass is brought to the target with the splinters, and in which the relatively small splinters immediately immerse in the liquid to be ignited and thereby extinguish, does not exist in the present invention. Rather, by using the multiple shell, several splinters fly in a staggered manner in front of the splinters provided with the fire mass and prepare the fuel for optimal ignition through the cavitation bubble that forms when it enters or through leakage.

Weitere Einzelheiten der Erfindung werden im folgenden anhand von Ausführungsbeispielen und mit Hilfe von Figuren beschrieben.Further details of the invention are described below on the basis of exemplary embodiments and with the aid of figures.

Es zeigen:

Fig. 1
einen Teil eines erfindungsgemäßen Splittergeschosses, wobei der Sprengstoff von drei Geschoßhüllen umgeben ist;
Fig. 2
die Darstellung des Querschnittes des Geschosses nach Fig. 1;
Fig. 3
eine Draufsicht auf die mit Strukturzonen versehene innere Geschoßhülle;
Fig. 4,4a und Fig. 5,5a,
die Draufsicht bzw. den Querschnitt zwei weiterer Ausführungsbeispiele der inneren Geschoßhülle mit Strukturzonen und
Fig. 6
einen Ausschnitt der inneren Geschoßhülle mit Strukturzonen mit einer angrenzenden äußeren Geschoßhülle zur Erläuterung der Erfindung.
Show it:
Fig. 1
part of a fragmentary projectile according to the invention, the explosive being surrounded by three projectile casings;
Fig. 2
the representation of the cross section of the projectile according to Fig. 1;
Fig. 3
a plan view of the inner shell provided with structural zones;
FIGS. 4,4a and 5,5a,
the top view or the cross section of two further embodiments of the inner projectile shell with structural zones and
Fig. 6
a section of the inner shell with structural zones with an adjacent outer shell to explain the invention.

In Fig. 1 ist mit 1 das aus mehreren Geschoßhüllen bestehende Splittergeschoß bezeichnet. Die Geschoßhülle setzt sich aus den äußeren Geschoßhüllen 2 und 3 sowie aus der inneren Geschoßhülle 4 zusammen. Mit 5 ist der Sprengstoff des Splittergeschosses und mit 6 die auf der inneren Geschoßhülle 4 aufgebrachte Brandmasse bezeichnet. In der inneren Geschoßhülle 4 befinden sich auf der dem Sprengstoff 5 abgewandten Seite Strukturzonen 7. Diese Strukturzonen 7 werden so gewählt, daß die verbleibende Wandstärke der Geschoßhülle 4 an diesen Stellen geringer ist als die Wandstärke der die Strukturzonen umgebenden Teile der Hülle 4.In Fig. 1, the fragmentary floor consisting of several shell casings is designated by 1. The shell is composed of the outer shell 2 and 3 and the inner shell 4. With 5 the explosive of the fragmentary bullet and with 6 the fire mass applied to the inner shell 4 is designated. Structural zones 7 are located in the inner shell 4 on the side facing away from the explosive 5. These structural zones 7 are selected such that the remaining wall thickness of the shell 4 at these points is less than the wall thickness of the parts of the shell 4 surrounding the structural zones.

In den Fig. 4 und 4a sowie 5 und 5a sind zwei weitere Ausführungsbeispiele der inneren Geschoßhülle 4',4'' mit Strukturzonen 7',7'' dargestellt. Dabei zeigt die Fig. 4 eine Draufsicht und die Fig. 4a einen Querschnitt der inneren Hülle 4' mit einer Strukturzonenverteilung, die so gewählt ist, daß die die Strukturzonen umgebenen Teile der Hülle 4' eine etwa rechteckförmige Gestalt ausweisen. In Fig. 5 ist die Draufsicht auf eine Geschoßhülle 4'' mit Strukturzonen 7'' dargestellt, die einen sägezahnförmigen Verlauf aufweisen (vergl. Fig. 5a).4 and 4a and 5 and 5a, two further exemplary embodiments of the inner shell 4 ', 4' 'with structural zones 7', 7 '' are shown. 4 shows a top view and FIG. 4a shows a cross section of the inner shell 4 'with a structure zone distribution which is selected such that the parts of the shell 4' surrounding the structure zones have an approximately rectangular shape. 5 shows the top view of a projectile casing 4 ″ with structural zones 7 ″, which have a sawtooth-shaped course (see FIG. 5a).

Im folgenden wird näher auf die Wirkungsweise der Erfindung eingegangen. Hierzu ist in Fig. 6 ein Ausschnitt aus Fig. 1 dargestellt, der die innere Geschoßhülle 4, die Strukturzonen 7 sowie die angrenzende äußere Geschoßhülle 3 zeigt.The mode of operation of the invention is discussed in more detail below. For this purpose, a section from FIG. 1 is shown in FIG. 6, which shows the inner shell 4, the structural zones 7 and the adjacent outer shell 3.

Bei der Detonation des Sprengstoffes 5 (Fig. 1) wird der entstehende Stoßwellenimpuls lokal an den Kontaktstellen 8 in die Hülle 3 eingekoppelt. In den durch die Strukturzonen 7 definierten Zwischenräumen erfolgt hingegen keine Stoßwelleneinkoppelung, da die entsprechenden Wellen am Übergang des Werkstoffes der Hülle 4 zur Luft reflektiert werden.During the detonation of the explosive 5 (FIG. 1), the resulting shock wave pulse is locally coupled into the casing 3 at the contact points 8. In contrast, in the spaces defined by the structural zones 7 there is no shock wave coupling, since the corresponding waves are reflected at the transition of the material of the casing 4 to the air.

Die an den Kontaktstellen 8 eingekoppelte Energie beschleunigt Teilbereiche der äußeren Hülle 3 bzw. induziert in dieser Hülle Spannungsgradienten. Dieses führt zur Ausbildung von Splittern, die in ihrer Geometrie dem auf die innere Hülle eingebrachten Muster entsprechen.The energy coupled in at the contact points 8 accelerates partial regions of the outer shell 3 or induces voltage gradients in this shell. This leads to the formation of splinters whose geometry corresponds to the pattern made on the inner shell.

Bei einer vorteilhaften Anordnung wurde als innere Hülle 4 eine Stahlhülle verwendet und als Außenhülle 3 ein Werkstoff mit hohem Impedanzwert ρ . c ( ρ = Dichte, c = Geschwindigkeit, der durch die Detonation bewirkten Stoßwelle), z. B. Wolfram. Denn für den an den Kontaktstellen 8 eingekoppelten Schalldruck p für die Dichtewellen gilt:

Figure imgb0001

wobei:

po =
Schalldruck der einlaufenden Welle
ρ₁ c₁ =
Impedanz der inneren Hülle
ρ₂ c₂ =
Impedanz der äußeren Hülle
Da für die Kombination Wolfram/ Stahl gilt (ρ₁ c₁ / ρ₂ c₂) <1 wird p groß. Andererseits genügt bei Wolfram bzw. Wolframschwermetall eine kurzfristige Überschreitung der kritischen Spannungswerte, da diese Werkstoffe spröde und rißanfällig sind.In an advantageous arrangement, a steel shell was used as the inner shell 4 and a material with a high impedance value ρ as the outer shell 3. c (ρ = density, c = velocity of the shock wave caused by the detonation), z. B. Tungsten. The following applies to the sound pressure p coupled in at the contact points 8 for the density waves:
Figure imgb0001

in which:
po =
Sound pressure of the incoming wave
ρ₁ c₁ =
Inner envelope impedance
ρ₂ c₂ =
Outer shell impedance
Since the combination of tungsten / steel applies (ρ₁ c₁ / ρ₂ c₂) <1 p becomes large. On the other hand, a short-term exceedance of the critical stress values is sufficient for tungsten or tungsten heavy metal, since these materials are brittle and prone to cracking.

Bei Verwendung duktiler Werkstoffe für die Hülle 3 muß zusätzlich noch Verformungsarbeit bis zum Bruch aufgebracht werden.When using ductile materials for the shell 3, deformation work must also be applied until breakage.

Die Splitterform, Splittergröße und Splitteranzahl sowie die Splittergeschwindigkeit lassen sich durch geeignete Strukturierung der inneren Hülle 4 einstellen.The shape, size and number of chips as well as the speed of the chips can be adjusted by suitable structuring of the inner shell 4.

Claims (3)

  1. Fragmentation projectile in which the explosive material (5) is surrounded by at least two projectile casings (2,3,4',4''), the casing (4,4',4'') nearest to the explosive having a preselected fragmentation structure (structure zones)(7,7',7'') as a result of which the projectile (1), on detonation, generates reproducible fragments, the structure zones (7,7',7'') consisting of preselected regions of smaller wall thickness than those parts of the casing (4,4',4'') which surround the structure zones, characterised by the fact that the structure zones (7,7',7'') are situated on that side of the casing (4,4',4'') which is further away from the explosive (5) so that the shock wave occurring on the detonation is transmitted with a localised time delay to the next casings (2,3), thus transmitting thereto the intended fragment shape, and that combustive substance (6) is provided on that side of the casing (4,4',4'') which faces towards the explosive (5).
  2. Fragmentation projectile in accordance with Claim 1, characterised by the fact that the casing (4,4',4'') provided with structure zones (7,7',7'') has a far lower impedance ρ.c than the adjacent outer casing (3), ρ being the density of the corresponding material and c the velocity of the shock wave in the relevant material caused by the detonation.
  3. Fragmentation projectile in accordance with Claim 2, characterised by the fact that the casing (4,4',4'') provided with structure zones (7,7',7'') consists of steel and the adjacent outer zone (3) is of tungsten or a tungsten heavy metal.
EP90114529A 1989-12-07 1990-07-28 Fragmentation missile Expired - Lifetime EP0433544B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3940462 1989-12-07
DE3940462A DE3940462A1 (en) 1989-12-07 1989-12-07 SPLITTER FLOOR

Publications (2)

Publication Number Publication Date
EP0433544A1 EP0433544A1 (en) 1991-06-26
EP0433544B1 true EP0433544B1 (en) 1994-03-02

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USH1367H (en) * 1991-02-07 1994-11-01 The United States Of America As Represented By The Secretary Of The Navy Wire assault weapon warhead
US5567906B1 (en) * 1995-05-15 1998-06-09 Western Atlas Int Inc Tungsten enhanced liner for a shaped charge
FR2741437B1 (en) * 1995-11-16 1997-12-19 Poudres & Explosifs Ste Nale METHOD OF MANUFACTURING EXPLOSIVE ELEMENT WITH CONTROLLED FRAGMENTATION
DE19600167C1 (en) * 1996-01-04 2003-07-17 Diehl Stiftung & Co Penetrator, used in explosive charge, comprises housing made from thin steel shell and heavy metal inner part containing charge and ignition system
DE19809181C1 (en) 1998-03-04 1999-07-29 Daimler Benz Aerospace Ag Fragmentation warhead for munition
FR2785672B1 (en) * 1998-11-05 2005-08-26 Tda Armements Sas PROJECTILE WITH CALIBRATED FRAGMENTATION
US6186070B1 (en) * 1998-11-27 2001-02-13 The United States Of America As Represented By The Secretary Of The Army Combined effects warheads
DE10025055C2 (en) * 2000-05-23 2003-12-24 Eads Deutschland Gmbh Splinter-producing warhead to combat semi-hard technical targets
EP1167914A1 (en) * 2000-06-19 2002-01-02 SM Schweizerische Munitionsunternehmung AG Self-propelled projectile with armour-piercing core
FR2812385B1 (en) * 2000-07-28 2003-02-21 Giat Ind Sa EXPLOSIVE AMMUNITION WITH FRAGMENTABLE BODY
US20050087088A1 (en) * 2003-09-30 2005-04-28 Lacy E. W. Ordnance device for launching failure prone fragments
US6817299B1 (en) 2003-12-10 2004-11-16 The United States Of America As Represented By The Secretary Of The Navy Fragmenting projectile having threaded multi-wall casing
BG969U1 (en) * 2006-12-19 2007-12-28 "Арсенал" Ад Fragmentation grenade
US7743707B1 (en) * 2007-01-09 2010-06-29 Lockheed Martin Corporation Fragmentation warhead with selectable radius of effects
IL189612A (en) * 2008-02-19 2012-10-31 Rafael Advanced Defense Sys Pyrophoric arrows-type warhead
US9255774B2 (en) * 2008-06-30 2016-02-09 Battelle Memorial Institute Controlled fragmentation of a warhead shell
US8015924B1 (en) * 2009-05-29 2011-09-13 The United States Of America As Represented By The Secretary Of The Air Force Linear cellular bomb case
US8061275B1 (en) * 2010-01-08 2011-11-22 The United States Of America As Represented By The Secretary Of The Army Warhead selectively releasing fragments of varied sizes and shapes
US8522685B1 (en) * 2010-02-22 2013-09-03 The United States Of America As Represented By The Secretary Of The Army Multiple size fragment warhead
US8720342B1 (en) * 2010-03-23 2014-05-13 The United States Of America As Represented By The Secretary Of The Army Low collateral damage fragmentation warhead
US8387539B1 (en) * 2010-05-10 2013-03-05 The United States Of America As Represented By The Secretary Of The Air Force Sculpted reactive liner with semi-cylindrical linear open cells
RU2450239C1 (en) * 2010-11-18 2012-05-10 Владимир Викторович Черниченко Destructing agent of cassette ammunition
US8616129B1 (en) 2011-08-19 2013-12-31 The United States Of America As Represented By The Secretary Of The Navy Cartridge actuator and method of manufacture thereof
US9291437B2 (en) * 2012-06-01 2016-03-22 Orbital Atk, Inc. Radial firing warhead system and method
IL222989A (en) * 2012-11-12 2016-02-29 Israel Aerospace Ind Ltd Warhead
WO2015175039A2 (en) 2014-02-11 2015-11-19 Raytheon Company Munition with nose kit connecting to aft casing connector
AT515209B1 (en) * 2014-03-14 2015-07-15 Hirtenberger Defence Systems Gmbh & Co Kg bullet
US9810513B2 (en) 2014-08-04 2017-11-07 Raytheon Company Munition modification kit and method of modifying munition
US9739583B2 (en) 2014-08-07 2017-08-22 Raytheon Company Fragmentation munition with limited explosive force
US9909848B2 (en) 2015-11-16 2018-03-06 Raytheon Company Munition having penetrator casing with fuel-oxidizer mixture therein
US10066915B1 (en) * 2016-09-21 2018-09-04 The United States Of America As Represented By The Secretary Of The Army Multi-purpose state changing munition
US11226181B2 (en) * 2017-03-06 2022-01-18 Omnitek Partners, L.L.C. High explosive fragmentation mortars
US11454480B1 (en) 2019-06-12 2022-09-27 Corvid Technologies LLC Methods for forming munitions casings and casings and munitions formed thereby
FR3098292B1 (en) * 2019-07-04 2021-07-23 Cta Int Telescoped ammunition including a shell
GB202003965D0 (en) * 2020-03-19 2020-05-06 Secr Defence Casing for a fragmentation weapon, fragmentation weapon, and method of manufacture

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR454818A (en) * 1912-03-02 1913-07-16 Edoardo Agudio Projectile ricocheting and bursting at a distance from its point of arrival
US3000309A (en) * 1943-01-30 1961-09-19 Zapf Louis Fragmentation projectile
US3566794A (en) * 1958-11-26 1971-03-02 Us Navy Controlled fragmentation of multi-walled warheads
CH485194A (en) * 1968-01-25 1970-01-31 Oerlikon Buehrle Ag Bullet with fragmentation jacket
US4745864A (en) * 1970-12-21 1988-05-24 Ltv Aerospace & Defense Company Explosive fragmentation structure
US4106411A (en) * 1971-01-04 1978-08-15 Martin Marietta Corporation Incendiary fragmentation warhead
US3799054A (en) * 1972-05-08 1974-03-26 Armament Syst Inc Controlled fragmentation explosive device
US3820464A (en) * 1973-03-09 1974-06-28 Us Navy Variable sized fragment explosive projectile
DE2339386B1 (en) * 1973-08-03 1975-01-30 Diehl Fa Explosive charge for projectiles
US4089267A (en) * 1976-09-29 1978-05-16 The United States Of America As Represented By The Secretary Of The Army High fragmentation munition
US4381692A (en) * 1977-05-11 1983-05-03 Quantic Industries, Inc. Method of making an incendiary munition
US4989493A (en) * 1985-10-21 1991-02-05 The United States Of America As Represented By The Secretary Of The Air Force Explosive attenuating structure for use inside missiles and the like
DE3725091A1 (en) * 1987-07-29 1989-02-16 Diehl Gmbh & Co FIRE EFFECT PROJECTILE, METHOD FOR PUTTING THE FIRE INTO THE PROJECTILE AND DEVICE FOR EXERCISING THE PROCESS
US5054399A (en) * 1988-07-05 1991-10-08 The United States Of America As Represented By The Secretary Of The Air Force Bomb or ordnance with internal shock attenuation barrier

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US5131329A (en) 1992-07-21
DE59004778D1 (en) 1994-04-07
EP0433544A1 (en) 1991-06-26
DE3940462A1 (en) 1991-06-13

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