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EP0950870B1 - Combination type warhead - Google Patents

Combination type warhead Download PDF

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Publication number
EP0950870B1
EP0950870B1 EP99107139A EP99107139A EP0950870B1 EP 0950870 B1 EP0950870 B1 EP 0950870B1 EP 99107139 A EP99107139 A EP 99107139A EP 99107139 A EP99107139 A EP 99107139A EP 0950870 B1 EP0950870 B1 EP 0950870B1
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EP
European Patent Office
Prior art keywords
warhead
combination
penetrator
warhead according
shaped charge
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
Application number
EP99107139A
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German (de)
French (fr)
Other versions
EP0950870A3 (en
EP0950870A2 (en
Inventor
Helmut Dr. Muthig
Werner Dr. Arnold
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TDW Gesellschaft fuer Verteidigungstechnische Wirksysteme mbH
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TDW Gesellschaft fuer Verteidigungstechnische Wirksysteme mbH
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Publication of EP0950870A2 publication Critical patent/EP0950870A2/en
Publication of EP0950870A3 publication Critical patent/EP0950870A3/en
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Publication of EP0950870B1 publication Critical patent/EP0950870B1/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
    • F42B12/04Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type
    • F42B12/10Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with shaped or hollow charge
    • F42B12/16Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with shaped or hollow charge in combination with an additional projectile or charge, acting successively on the target
    • 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

Definitions

  • the invention relates to a combination warhead according to claim 1.
  • Warheads In use as active systems for guided missiles, submunitions or other Warheads are in the majority special, on the respective Use case optimized warheads. These are, for example, in anti-tank defense, at which has a high penetration rate compared to armored steel (possibly with additional reactive armor) is required, the well-known shaped charge systems (short: HL systems).
  • Splinter charges for use. These are usually pressure / splinter charges in the destination control.
  • semi-hard targets e.g. Radar positions, trucks, etc.
  • HL or P charge systems used as so-called multi-purpose warheads.
  • the fight against hard armor is made by the hollow or projectile-forming Ensures cargo and the simultaneous combat of surrounding semi-hard targets by completed the additional splinter coat applied. Both mechanisms of action are considered this kind of multi-purpose systems ignited together and simultaneously. The effect occurs at the same time.
  • the use of only one of the two types of action is not provided.
  • the hard concrete targets like bunkers, Airplane shelters, runways etc. as well as from other destinations where the main effect of the Explosive charge should only be achieved after penetrating a first hard layer, such as. in ships, attack helicopters or in combating all of the above Goals "in cover", i.e. behind walls or inside buildings, they are suitable Penetrator warheads. These are filled with explosives and high Penetration excellent metal body that only after entering or Penetrate the first hard layer and then ignite its pressure or Develop a splintering effect.
  • the combination active system is universally designed for all required operating modes at the same time.
  • the peculiarity in the Application is due to the different use of the different Ignition system components accomplished.
  • the ignition is made by a Distance detonators at the optimal distance, in the second case through an intelligent penetrator ignition system.
  • FIG. 1 The basic structure of the combination warhead according to the invention is shown in FIG. 1 shown.
  • a conventional penetrator 1 with an optimized tip and optimized lengths Diameter ratio (L / D) is not completely filled with explosive 2, but contains at its tip an additional cavity 3, which is suitable for the formation of a To ensure shaped charge spikes.
  • This room 3 is against the one behind it Explosives 2 separated with a shaped charge lining 4.
  • the shockproof version this lining and its support on the penetrator 5 and the Explosives containment are designed to match the warhead.
  • the securing device 6 contains the ignition stage for the explosive charge 2 and as the first pyrotechnic elements of the ignition chain the detonator and, if applicable, transformer or Amplifier charges.
  • the combination warhead is triggered as follows:
  • the appropriate Distance ignited by the distance fuse of the warhead. It forms a shaped charge spike, which still has to penetrate the tip of the penetrator. Then can he can act unhindered on the target and his high penetration in armored steel deliver.
  • FIGS. 2 to 13 Possible ones in FIGS. 2 to 13 are possible Refinements of this concept are shown that facilitate implementation or depending on Target requirement enable the optimization of shaped charge or penetrator performance. she are to be seen as exemplary, as well as other combinations of the different constructive measures, as the ones just shown in the drawing, a sensible one Warhead design result.
  • Fig. 4 shows another measure to improve the HL performance.
  • the warhead is in different compartments 9 and 10 divided, depending on the operating mode be ignited.
  • Fig.5 is exemplified that the shaped charge lining 4 on the special Use in combination warhead compared to a pure, non-penetrating one Hollow charge is optimized with regard to position, material, wall thickness, opening angle etc. she also takes into account the special L / D situation in the combination warhead as well as the greater insulation of the load through the penetrator casing 5.
  • FIG. 6 is an example the lining 11 of an EFP load is shown.
  • Fig. 7 shows a solution to this Problems appropriate formation of the pentrator tip, which has an inner cavity 12 in the Has peak.
  • Fig. 10 represents a way to increase the stability of the penetrator by the Cavity 3 in front of the shaped charge lining with an incompressible medium 15 is filled out.
  • this material gives the penetrator increased strength, in the "hollow charge” mode it can be lowered or with the Removing the penetrator tip can be removed.
  • This medium can, if appropriate Design may also a secondary effect such as Fire or similar cause.
  • a pretreated penetrator sleeve 16 can be used to increase the splintering effect be pre-embossed or otherwise pretreated such that the natural splinters of the Have predefined geometries. This is shown in Fig. 11. Here is one too Adjustment of the optimum with regard to penetrator performance (smooth casing) or splinter performance (embossed sleeve) possible.
  • Fig. 12 shows that in the warhead according to the invention also internal, preformed Splitter 17 can be used to optimize the splitting effect.
  • the conscious Broken rows of fragments are intended to symbolize that "patterns" between Preformed and natural shell splinters used to optimize the effect on the target can be.
  • FIG. 13 an external splinter jacket 18 is shown, which the splinter effect in the Distance ignition increased, but also before the charge detonated by a separating agent 19 can be separated if this is necessary to avoid collateral damage should.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Inorganic Compounds Of Heavy Metals (AREA)

Description

Die Erfindung betrifft einen Kombinationsgefechtskopf gemäß Anspruch 1.The invention relates to a combination warhead according to claim 1.

In der Anwendung als Wirksysteme für Lenkflugkörper, Submunitions- oder sonstige Gefechtsköpfe befinden sich heute in der Mehrzahl spezielle, auf den jeweiligen Anwendungsfall optimierte Gefechtsköpfe. Dies sind zum Beispiel bei der Panzerabwehr, bei der eine hohe Durchschlagsleistung gegenüber Panzerstahl (eventuell mit zusätzlicher reaktiver Panzerung) erforderlich ist, die bekannten Hohlladungssysteme (kurz: HL-Systeme).In use as active systems for guided missiles, submunitions or other Warheads are in the majority special, on the respective Use case optimized warheads. These are, for example, in anti-tank defense, at which has a high penetration rate compared to armored steel (possibly with additional reactive armor) is required, the well-known shaped charge systems (short: HL systems).

Für einen größeren Bekämpfungsabstand, d.h. bei einem Vorbeiflug des Gefechtskopfes am Ziel, werden z. B. im Einsatz als Suchzündermunition eher projektilbildende Ladungen (kurz: P-Ladungssysteme) mit geringeren Durchschlagsleistungen als bei Hohlladungen, aber einer Wirkung aus größerem Abstand, verwendet. Auch Zwischenformen zwischen HL-Systemen und P-Ladungssystemen sind bekannt (z.B. "Hemispheres").For a larger control distance, i.e. when the warhead flies by Target, z. B. used as search fuse ammunition rather projectile-forming charges (short: P-charge systems) with lower breakdown capacities than shaped charges, but one Effect from a distance, used. Also intermediate forms between HL systems and P-charging systems are known (e.g. "Hemispheres").

Zusätzlich zu diesen axial gerichteten Ladungstypen kommen radial wirkende Splitterladungen zum Einsatz. In der Flugzielbekämpfung sind dies in der Regel Druck/Splitter-Ladungen. Zur Bekämpfung räumlich verteilter halbharter Ziele (z.B. Radarstellungen, LKW etc.) werden neben der reinen Splitterladung auch Kombinationen mit den HL- oder P-Ladungs-Systemen als sogenannte Mehrzweckgefechtsköpfe eingesetzt. Dabei wird die Bekämpfung der harten Panzerungen von der Hohl- oder projektilbildenden Ladung gewährleistet und die gleichzeitige Bekämpfung umliegender halbharter Ziele durch den zusätzlich aufgebrachten Splittermantel vollzogen. Beide Wirkmechanismen werden bei dieser Art von Mehrzweck-Systemen gemeinsam und gleichzeitig gezündet. Die Wirkung tritt gleichzeitig ein. Die Anwendung nur einer der beiden Wirkungsarten (Splitter oder Hohlladung) ist nicht vorgesehen.In addition to these axially directed charge types, there are radial ones Splinter charges for use. These are usually pressure / splinter charges in the destination control. To combat spatially distributed semi-hard targets (e.g. Radar positions, trucks, etc.) are not only pure fragmentary loads, but also combinations the HL or P charge systems used as so-called multi-purpose warheads. The fight against hard armor is made by the hollow or projectile-forming Ensures cargo and the simultaneous combat of surrounding semi-hard targets by completed the additional splinter coat applied. Both mechanisms of action are considered this kind of multi-purpose systems ignited together and simultaneously. The effect occurs at the same time. The use of only one of the two types of action (splinter or Shaped charge) is not provided.

Für die Bekämpfung einer weiteren Zielklasse, den harten Betonzielen wie Bunker, Flugzeugshelter, Startbahnen etc. sowie von anderen Zielen, bei denen die Hauptwirkung der Sprengladung erst nach dem Durchdringen einer ersten harten Schicht erzielt werden soll, wie z.B. bei Schiffen, Kampfhubschraubern oder bei der Bekämpfung aller oben angegebenen Ziele "in Deckung", d.h. hinter Mauern oder innerhalb von Gebäuden eigenen sich die Penetrator- Gefechtsköpfe. Dies sind mit Sprengstoff gefüllte und durch hohe Durchdringungsleistung ausgezeichnete Metallkörper, die erst nach dem Ein- oder Durchdringen der ersten harten Schicht gezündet werden und dann ihre Druck- oder Splitterwirkung entfalten.For fighting another target class, the hard concrete targets like bunkers, Airplane shelters, runways etc. as well as from other destinations where the main effect of the Explosive charge should only be achieved after penetrating a first hard layer, such as. in ships, attack helicopters or in combating all of the above Goals "in cover", i.e. behind walls or inside buildings, they are suitable Penetrator warheads. These are filled with explosives and high Penetration excellent metal body that only after entering or Penetrate the first hard layer and then ignite its pressure or Develop a splintering effect.

Aus der DE 38 00 975 A1 ist ein Panzergeschoß bekannt geworden, in dem eine Hohlladung angeordnet ist. Nach dem Durchschlagen einer ersten harten Schicht leitet der Zünder die Detonation der in Flugrichtung orientierten Hohlladung ein. Ein Hinweis auf weitere Wirkungsmöglichkeiten ist nicht angegeben.From DE 38 00 975 A1 an armored projectile has become known, in which a shaped charge is arranged. After striking a first hard layer, the detonator conducts the Detonation of the shaped charge oriented in the direction of flight. A reference to others Impact is not specified.

Bei neuen Flugkörperprogrammen wir zunehmend mehr als nur die Bekämpfung nur einer der oben genannten Zielklassen gefordert. Die dementsprechenden Wirksysteme sollen gegen eine Mischung verschiedenster Ziele gleichzeitig wirksam sein. Sie sollen ein breites Spektrum der möglichen Anwendungsfälle abdecken. Dagegen soll die Typenvielfalt aus logistischen und Kostengründen gering sein. Diese Forderung ist mit den bekannten speziell optimierten Wirksystemen nicht zu erfüllen.With new missile programs, we are increasingly doing more than just fighting one of the target classes mentioned above. The corresponding active systems should counter a mixture of different goals can be effective at the same time. You are supposed to be a broad Cover spectrum of possible applications. In contrast, the variety of types should logistical and cost reasons to be low. This requirement is special with the known ones not to meet optimized active systems.

Es ist deshalb Aufgabe der Erfindung, ein Wirksystem zu entwerfen, das die Nachteile der bekannten Systeme vermeidet und das bezüglich der Wirkung und des Zündzeitpunktes zielangepaßt einstellbar ist.It is therefore an object of the invention to design an active system which has the disadvantages of known systems avoids and that with regard to the effect and the ignition timing can be adjusted to suit the target.

Diese Aufgabe wird erfindungsgemäß durch die Merkmale des Patentanspruchs 1 gelöst. Weiterbildungen der Erfindung sind in den Unteransprüchen angegeben.This object is achieved by the features of claim 1. Developments of the invention are specified in the subclaims.

Die besonderen Vorteile der Erfindung liegen darin, daß das Kombinationswirksystem universell für alle geforderten Betriebsarten gleichzeitig ausgelegt ist. Die Besonderheit in der Anwendung wird durch den unterschiedlichen Einsatz der verschiedenen Zündsystemkomponenten bewerkstelligt. Im ersten Fall erfolgt die Zündung durch einen Abstandszünder im optimalen Abstand, im zweiten Fall durch ein intelligentes Penetrator-Zündsystem.The particular advantages of the invention are that the combination active system is universally designed for all required operating modes at the same time. The peculiarity in the Application is due to the different use of the different Ignition system components accomplished. In the first case, the ignition is made by a Distance detonators at the optimal distance, in the second case through an intelligent penetrator ignition system.

Anhand der Zeichnung wird ein Ausführungsbeispiel der Erfindung näher erläutert.

  • Fig. 1 zeigt das Prinzip eines Kombinationsgefechtskopfs,
  • Fig.2 zeigt die passive Detonationswellenlenkung zur Optimierung der Hohlladungsleistung,
  • Fig.3 zeigt die Zündortanpassung zur Optimierung der Hohlladungsleistung,
  • Fig.4 zeigt die Aufteilung des Gesamtgefechtskopfes in verschiedene Kompartments mit eigener Zündung,
  • Fig. 5 zeigt die Anpassung der Hohlladungsauskleidung zur Optimierung der Hohlladungsleistung,
  • Fig. 6 zeigt die Ausprägung der Auskleidung allgemein als Hohlladung, EFP-Ladung oder Zwischenform davon,
  • Fig.7 zeigt die Anpassung der Penetratorspitze zur Optimierung der Hohlladungsleistung,
  • Fig. 8 zeigt die Vor-Hohlladung zum Öffnen der Penetratorspitze,
  • Fig.9 zeigt die absprengbare Penetratorspitze bei Verwendung als Hohlladung,
  • Fig. 10 zeigt den mit einem inkompressiblen Medium gefüllten Hohlraum zur Erhöhung der Festigkeit des Penetrators,
  • Fig. 11 zeigt eine geprägte Penetratorhülle zur Optimierung der Splitterbildung,
  • Fig. 12 zeigt in Form und Größe optimierbare, innenliegende, vorgeformte Splitter und
  • Fig. 13 zeigt einen additiven Splittermantel aus vorgeformten Splittern, der optional absprengbar ist.
  • An embodiment of the invention is explained in more detail with reference to the drawing.
  • 1 shows the principle of a combination warhead,
  • 2 shows the passive detonation wave guidance for optimizing the shaped charge performance,
  • 3 shows the ignition location adaptation to optimize the shaped charge performance,
  • 4 shows the division of the overall warhead into different compartments with their own ignition,
  • 5 shows the adaptation of the shaped charge lining to optimize the shaped charge performance,
  • 6 shows the shape of the lining generally as a shaped charge, EFP charge or intermediate form thereof,
  • 7 shows the adaptation of the penetrator tip to optimize the shaped charge performance,
  • 8 shows the pre-shaped charge for opening the penetrator tip,
  • 9 shows the detachable penetrator tip when used as a shaped charge,
  • 10 shows the cavity filled with an incompressible medium to increase the strength of the penetrator,
  • 11 shows an embossed penetrator sleeve for optimizing the formation of fragments,
  • Fig. 12 shows in terms of shape and size, internal, preformed splinters and
  • 13 shows an additive splinter jacket made of preformed splinters, which can optionally be blasted off.
  • Der prinzipielle Aufbau des erfindungsgemäßen Kombinationsgefechtskopfs ist in Fig. 1 dargestellt. Ein herkömmlicher Penetrator 1 mit optimierter Spitze und optimiertem Längenzu Durchmesserverhältnis (L/D) ist nicht komplett mit Sprengstoff 2 gefüllt, sondern enthält an seiner Spitze einen zusätzlichen Hohlraum 3, der geeignet ist, die Ausbildung eines Hohlladungsstachels zu gewährleisten. Dazu ist dieser Raum 3 gegen den dahinterliegenden Sprengstoff 2 mit einer Hohlladungsauskleidung 4 abgetrennt. Die schockfeste Ausführung dieser Auskleidung sowie deren Abstützung an der Penetratorhülle 5 und die Sprengstoffverdämmung sind konstruktiv auf den Gefechtskopf abgestimmt.The basic structure of the combination warhead according to the invention is shown in FIG. 1 shown. A conventional penetrator 1 with an optimized tip and optimized lengths Diameter ratio (L / D) is not completely filled with explosive 2, but contains at its tip an additional cavity 3, which is suitable for the formation of a To ensure shaped charge spikes. This room 3 is against the one behind it Explosives 2 separated with a shaped charge lining 4. The shockproof version this lining and its support on the penetrator 5 and the Explosives containment are designed to match the warhead.

    Die Sicherungsvorrichtung 6 enthält die Zündstufe für die Sprengladung 2 sowie als erste pyrotechnische Elemente der Zündkette den Detonator und ggf. Übertrager- oder Verstärkerladungen.The securing device 6 contains the ignition stage for the explosive charge 2 and as the first pyrotechnic elements of the ignition chain the detonator and, if applicable, transformer or Amplifier charges.

    Ausgelöst wird der Kombinationsgefechtskopf wie folgt :The combination warhead is triggered as follows:

    In der Hohlladungsbetriebsart bei der Bekämpfung von gepanzerten Zielen wird im geeigneten Abstand ("Stand off") durch den Abstandszünder der Gefechtskopf gezündet. Es bildet sich ein Hohlladungsstachel aus, der erst noch die Penetratorspitze durchdringen muß. Dann kann er ungehindert auf das Ziel einwirken und seine hohe Durchschlagsleistung in Panzerstahl abliefern.In the shaped charge mode when fighting armored targets, the appropriate Distance ("Stand off") ignited by the distance fuse of the warhead. It forms a shaped charge spike, which still has to penetrate the tip of the penetrator. Then can he can act unhindered on the target and his high penetration in armored steel deliver.

    In der Penetratorbetriebsart bei der Bekämpfung von harten Schichtzielen wird nicht im Abstand gezündet, sondern erst die Penetration zumindest der ersten harten Schicht abgewartet, bevor ein (ggf. intelligenter) Penetratorzünder (ebenfalls in der Sicherungsvorrichtung untergebracht) den geeigneten Zündzeitpunkt berechnet und den Gefechtskopf auslöst. Er kann als Nebeneffekt immer noch eine nach vorne gerichtete Hohlladungswirkung aufweisen, die aufgrund möglicher schockbedingter Verformungen der Auskleidung gegenüber einem nichtpenetrierenden, reinen Hohlladungs-Gefechtskopf eingeschränkt sein kann. Die Hauptwirkung wird in diesem Fall aber durch Druck- und Splittereffekte der Penetratorhülle erreicht.In the penetrator mode when fighting hard shift targets is not in Ignited distance, but only the penetration of at least the first hard layer waited before a (possibly intelligent) penetrator detonator (also in the Safety device) calculates the appropriate ignition timing and the Warhead triggers. As a side effect, it can still be a forward-facing one Have shaped charge effect due to possible shock-related deformations of the Lining against a non-penetrating, pure shaped charge warhead may be restricted. The main effect in this case is through pressure and Splinter effects of the penetrator shell achieved.

    Neben diesem in Fig. 1 gezeigtem Grundprinzip sind in Fig.2 bis Fig. 13 mögliche Ausgestaltungen dieses Konzepts dargestellt, die eine Realisierung erleichtern bzw. je nach Zielanforderung die Optimierung von Hohlladungs- oder Penetratorleistung ermöglichen. Sie sind insofern als exemplarisch zu sehen, als auch andere Kombinationen der verschiedenen konstruktiven Maßnahmen, als die gerade zeichnerisch dargestellten, eine sinnvolle Gefechtskopfauslegung ergeben.In addition to this basic principle shown in FIG. 1, possible ones in FIGS. 2 to 13 are possible Refinements of this concept are shown that facilitate implementation or depending on Target requirement enable the optimization of shaped charge or penetrator performance. she are to be seen as exemplary, as well as other combinations of the different constructive measures, as the ones just shown in the drawing, a sensible one Warhead design result.

    In Fig.2 ist die Möglichkeit einer passiven Detonationswellenlenkung 7 für die Ausbildung eines optimalen Hohlladungsstachels dargestellt. Solche Maßnahmen können wichtig sein, weil einerseits für den Penetrator 1 ein großes Länge/Durchmesserverhältnis (L/D) von ca. 4...8 günstig ist, andererseits für die reine Hohlladung ein L/D von ca. 1 das Optimum darstellt. Die passive Detonationswellenlenkung 7 kann diese gegenläufigen Forderungen in bestimmten Grenzen ausgleichen. Wenn diese passive Maßnahme nicht ausreicht, kann durch die Wahl eines oder mehrerer näher an der Auskleidung liegenden Detonationsortes, z.B. mit zusätzlichem Detonator 8, für die Betriebsart "Hohlladung" deren Leistung im Sinne einer "aktiven Detonationswellenlenkung" erhöht werden; siehe Fig.3.2 shows the possibility of passive detonation wave guidance 7 for training an optimal shaped charge spike. Such measures can be important because on the one hand a large length / diameter ratio (L / D) of approx. 4 ... 8 is cheap, on the other hand an L / D of approx. 1 is the optimum for the pure shaped charge represents. The passive detonation wave steering 7 can meet these opposing requirements in balance certain limits. If this passive measure is not sufficient, can by choosing one or more detonation sites closer to the lining, e.g. with additional detonator 8, for the "hollow charge" mode, its performance in the sense an "active detonation wave steering" can be increased; see Fig. 3.

    Fig.4 zeigt eine weitere Maßnahme zur Verbesserung der HL-Leistung. Der Gefechtskopf ist in unterschiedliche Kompartments 9 und 10 aufgeteilt, die je nach Betriebsart unterschiedlich gezündet werden.Fig. 4 shows another measure to improve the HL performance. The warhead is in different compartments 9 and 10 divided, depending on the operating mode be ignited.

    In Fig.5 ist exemplarisch dargestellt, daß die Hohlladungsauskleidung 4 auf die spezielle Anwendung im Kombinationsgefechtskopf gegenüber einer reinen, nicht penetrierenden Hohlladung hinsichtlich Position, Material, Wandstärke, Öffnungswinkel etc. optimiert ist. Sie berücksichtigt auch die besondere L/D-Situation im Kombinationsgefechtskopf sowie die stärkere Verdämmung der Ladung durch die Penetratorhülle 5.In Fig.5 is exemplified that the shaped charge lining 4 on the special Use in combination warhead compared to a pure, non-penetrating one Hollow charge is optimized with regard to position, material, wall thickness, opening angle etc. she also takes into account the special L / D situation in the combination warhead as well as the greater insulation of the load through the penetrator casing 5.

    Grundsätzlich kann eine hohe Durchschlagsleistung gegen Panzerstahl nicht nur durch eine Hohlladung, sondern in abgeschwächter Form auch durch EFP-Ladungen oder durch Zwischenformen zwischen beiden Ladungstypen erreicht werden. In Fig.6 ist exemplarisch die Auskleidung 11 einer EFP-Ladung aufgezeigt.In principle, a high penetration rate against armored steel cannot be achieved only by one Shaped charge, but in a weakened form also by EFP charges or by Intermediate forms between the two types of charge can be achieved. Figure 6 is an example the lining 11 of an EFP load is shown.

    Ein Haupthindernis für die Ausbildung eines stabilen Hohlladungsstachels stellt die Penetratorspitze selbst dar. Durch geeignete Maßnahmen ist einerseits die Durchdringung durch den HL-Stachel zu erleichtern, andererseits muß die mechanische Stabilität der Spitze zur Erzielung der Penetrationsleistung gewährleistet sein. Fig.7 zeigt eine zur Lösung dieses Problems geeignete Ausbildung der Pentratorspitze, die eine innere Aushöhlung 12 in der Spitze aufweist.A major obstacle to the formation of a stable shaped charge spike is the Penetrator tip itself. On the one hand, the appropriate measures are the penetration by the HL spike, on the other hand, the mechanical stability of the tip be guaranteed to achieve the penetration performance. Fig. 7 shows a solution to this Problems appropriate formation of the pentrator tip, which has an inner cavity 12 in the Has peak.

    Wenn die Maßnahme gem. Fig. 7 nicht ausreicht, um eine Beeinträchtigung des Hohlladungsstachels durch die Penetratorspitze hinreichend gering zu halten, kann durch eine weitere Maßnahme, wie z.B. das Zünden einer Vor-Hohlladung 13, kurz vor Zielerreichung eine Öffnung in die Penetratorspitze gesprengt werden. Diese Ladung räumt auch andere vor dem Penetrator angeordnete Komponenten des Lenkflugkörpers, wie z.B. die Suchkopfelektronik, aus dem Weg und sichert die Ausbildung eines ungestörten HL-Stachels. In Fig.8 ist diese Möglichkeit aufgezeigt.If the measure according to Fig. 7 is not sufficient to impair the Keeping shaped charge spikes through the tip of the penetrator sufficiently low can be achieved by another measure, such as the ignition of a pre-shaped charge 13, shortly before An opening in the tip of the penetrator can be blasted. This charge clears also other components of the guided missile arranged in front of the penetrator, such as e.g. the Seeker electronics, out of the way and ensures the formation of an undisturbed HL spike. This possibility is shown in FIG.

    In Fig. 9 ist eine Weiterbildung der Erfindung mit einer abtrennbaren Penetratorspitze gezeigt, wobei die Abtrennmittel 14 prinzipiell vor der Zielannäherung wirksam werden, um mit dem Gefechtskopf eine ungehinderte Hohlladungswirkung zu erzielen.9 shows a further development of the invention with a detachable penetrator tip, the separation means 14 in principle take effect before the target approach in order to with the Warhead to achieve an unhindered shaped charge effect.

    Fig. 10 stellt eine Möglichkeit dar, die Stabilität des Penetrators zu erhöhen, indem der Hohlraum 3 vor der Hohlladungsauskleidung mit einem inkompressiblen Medium 15 ausgefüllt ist. Bei der Betriebsart "Penetrator" verleiht dieses Material dem Penetrator erhöhte Festigkeit, in der Betriebsart "Hohlladung" kann es abgelassen werden oder mit dem Abtrennen der Penetratorspitze entfernt werden. Dieses Medium kann bei geeigneter Ausgestaltung u.U. auch noch eine Sekundärwirkung wie z.B. Brand o.ä. verursachen.Fig. 10 represents a way to increase the stability of the penetrator by the Cavity 3 in front of the shaped charge lining with an incompressible medium 15 is filled out. In the operating mode "penetrator", this material gives the penetrator increased strength, in the "hollow charge" mode it can be lowered or with the Removing the penetrator tip can be removed. This medium can, if appropriate Design may also a secondary effect such as Fire or similar cause.

    Zur Steigerung der Splitterwirkung kann eine vorbehandelte Penetratorhülle 16 verwendet sein, die vorgeprägt oder anderweitig derart vorbehandelt ist, daß die natürlichen Splitter der Hülle vordefinierte Geometrien aufweisen. Dies ist in Fig. 11 dargestellt. Auch hier ist eine Anpassung des Optimums hinsichtlich Penetratorleistung (glatte Hülle) oder Splitterleistung (geprägte Hülle) möglich.A pretreated penetrator sleeve 16 can be used to increase the splintering effect be pre-embossed or otherwise pretreated such that the natural splinters of the Have predefined geometries. This is shown in Fig. 11. Here is one too Adjustment of the optimum with regard to penetrator performance (smooth casing) or splinter performance (embossed sleeve) possible.

    Fig. 12 zeigt, daß in dem erfindungsgemäßen Gefechtskopf auch innenliegende, vorgeformte Splitter 17 verwendet werden können, um die Splitterwirkung zu optimieren. Die bewußt unterbrochen gezeichneten Splitterreihen sollen symbolisieren, daß auch "Muster" zwischen vorgeformten und natürlichen Hüllen-Splittern zur Optimierung der Wirkung im Ziel verwendet werden können.Fig. 12 shows that in the warhead according to the invention also internal, preformed Splitter 17 can be used to optimize the splitting effect. The conscious Broken rows of fragments are intended to symbolize that "patterns" between Preformed and natural shell splinters used to optimize the effect on the target can be.

    In Fig. 13 ist ein außenliegender Splittermantel 18 dargestellt, der die Splitterwirkung bei der Abstandszündung erhöht, aber auch vor der Detonation der Ladung durch ein Abtrennmittel 19 abgetrennt werden kann, wenn dies zur Vermeidung von Kollateralschäden notwendig sein sollte.In Fig. 13, an external splinter jacket 18 is shown, which the splinter effect in the Distance ignition increased, but also before the charge detonated by a separating agent 19 can be separated if this is necessary to avoid collateral damage should.

    Es sei betont, daß auch alle anderen Kombinationen der voranstehend beschriebenen Maßnahmen als die gezeichneten möglich sind (z.B. abtrennbare Penetratorspitze mit außenliegendem Splittermantel o.ä.)It should be emphasized that all other combinations of those described above Measures than the ones shown are possible (e.g. detachable penetrator tip with external splinter jacket or similar)

    Claims (15)

    1. A combination warhead which is in the form of a penetrator (1), is filled with explosive (2) and has a safety device (6) with a penetrator igniter, and in which a cavity separated by a shaped charge lining (4) is formed in the penetrator (1 ) additionally to the explosive (2), either the warhead being ignited at a suitable distance from the target by a proximity fuse or, when combating hard laminated targets, a penetrator igniter triggering the warhead after penetration of the least the first hard layer.
    2. A combination warhead according to Claim 1, characterised in that a passive detonation wave guidance element (7) is integrated in the explosive (2).
    3. A combination warhead according to Claim 1 or 2, characterised in that an additional detonator (8), spaced away from the safety device (6) and closer than the latter to the shaped charge lining (4), is integrated in the explosive (2) for active detonation wave guidance.
    4. A combination warhead according to Claim 1, characterised in that the explosive (2) is located in two compartments (9 and 10) arranged one behind the other, each of which has separate ignition.
    5. A combination warhead according to any one of claims 1 to 4, characterised in that the shaped charge lining (4) is adapted with regard to position, material, wall thickness and aperture angle to the particular length/diameter ratio and the damming situation of the combination warhead.
    6. A combination warhead according to any one of claims 1 to 5, characterised in that to achieve adequate penetration of steel armour, instead of a pure shaped charge, an EFP charge, or intermediate forms between these two charge types, is/are used.
    7. A combination warhead according to any one of claims 1 to 6, characterised in that the penetrator tip has an internal hollow section (12).
    8. A combination warhead according to any one of claims 1 to 7, characterised in that the warhead has a shaped pre-charge (13) whereby an opening can be blasted in the penetrator tip and further components ahead of the penetrator can be removed.
    9. A combination warhead according to any one of claims 1 to 8, characterised in that the penetrator (1) has separation means (14) whereby the penetrator tip can be separated during the approach to the target.
    10. A combination warhead according to any one of claims 1 to 9, characterised in that the cavity (3) is filled with an incompressible medium (15) which, when the warhead is used as a shaped charge, is discarded before the approach to the target or is removed with the penetrator tip.
    11. A combination warhead according to Claim 10, characterised in that the released incompressible medium causes secondary effects, e.g. fire.
    12. A combination warhead according to any one of claims 1 to 11, characterised in that the penetrator casing (5) is pre-embossed or otherwise pre-treated to produce a defined fragmentation effect.
    13. A combination warhead according to any one of claims 1 to 12, characterised in that the warhead has internal, pre-formed fragments (17).
    14. A combination warhead according to any one of claims 1 to 13, characterised in that the warhead has an external fragmentation jacket (18).
    15. A combination warhead according to Claim 14, characterised in that the external fragmentation jacket (18) can be removed by separation means (19) before the target is reached.
    EP99107139A 1998-04-18 1999-04-13 Combination type warhead Expired - Lifetime EP0950870B1 (en)

    Applications Claiming Priority (2)

    Application Number Priority Date Filing Date Title
    DE19817266 1998-04-18
    DE19817266 1998-04-18

    Publications (3)

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    EP0950870A2 EP0950870A2 (en) 1999-10-20
    EP0950870A3 EP0950870A3 (en) 2000-11-22
    EP0950870B1 true EP0950870B1 (en) 2003-12-03

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    EP99107139A Expired - Lifetime EP0950870B1 (en) 1998-04-18 1999-04-13 Combination type warhead

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    DE (2) DE59907908D1 (en)

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    DE10018285C2 (en) * 2000-04-13 2002-07-11 Daimler Chrysler Ag Splinter warhead to combat technical objectives
    DE10025055C2 (en) 2000-05-23 2003-12-24 Eads Deutschland Gmbh Splinter-producing warhead to combat semi-hard technical targets
    WO2004003460A1 (en) * 2002-06-26 2004-01-08 Geke Technologie Gmbh Projectile or warhead
    DE10332257A1 (en) * 2003-07-16 2005-02-03 Rheinmetall W & M Gmbh warhead
    US7418905B2 (en) 2003-12-19 2008-09-02 Raytheon Company Multi-mission payload system
    EP1832838B1 (en) * 2006-03-09 2015-07-08 Saab AB A method for reducing the amount of ammunition types to be used and an ammunition device
    DE102007035551B4 (en) 2007-07-28 2010-04-22 TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH Support device for an explosive charge of a penetrator
    DE102007063681B4 (en) * 2007-07-28 2013-04-25 TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH Support device consists of front and rear-ward section loading located in shell with separating wall and initiator to trigger separating wall
    DE102011012850A1 (en) * 2011-02-10 2012-08-16 TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH Hohlladungspenetrator
    DE102012012409B4 (en) 2012-06-25 2015-05-13 TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH Penetrator with a shaped charge
    CN105043170B (en) * 2015-08-04 2016-08-24 北京航天长征飞行器研究所 A kind of monoblock type warhead
    DE102018006741B4 (en) * 2018-08-24 2022-06-15 TDW Gesellschaft für verteidigungstecchnische Wirksysteme mbH Tandem charge for a missile

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    Also Published As

    Publication number Publication date
    EP0950870A3 (en) 2000-11-22
    EP0950870A2 (en) 1999-10-20
    DE59907908D1 (en) 2004-01-15
    DE19917144B4 (en) 2004-09-23
    DE19917144A1 (en) 1999-12-09

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