EP1153260B1 - Missile for combatting vehicles with active self-protection - Google Patents
Missile for combatting vehicles with active self-protection Download PDFInfo
- Publication number
- EP1153260B1 EP1153260B1 EP00904904A EP00904904A EP1153260B1 EP 1153260 B1 EP1153260 B1 EP 1153260B1 EP 00904904 A EP00904904 A EP 00904904A EP 00904904 A EP00904904 A EP 00904904A EP 1153260 B1 EP1153260 B1 EP 1153260B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- missile
- protection
- self
- active self
- vehicles
- 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
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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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
Description
Gegenstand der Erfindung ist ein Flugkörper nach dem Oberbegriff des Anspruchs 1.The invention relates to a missile according to the preamble of
Flugkörper mit einer oder mehreren Hohlladungen, z. B. in Form eines Tandemgefechtskopfes, zur Bekämpfung gepanzerter Fahrzeuge sind Stand der Technik und in unterschiedlichsten Ausführungsformen beschrieben. Nachteil dieser bekannten Ausführungsformen ist, daß sie von sogenannten aktiven Selbstschutzsystemen der gepanzerten Fahrzeuge in ihrer Wirkung abgeschwächt oder sogar wirkungslos gemacht werden können. Solche aktiven Seibstschutzsysteme sind z. B. beschrieben in
- armada international 3/1998 "Panzerstahl ist nicht alles", S. 34 - 46
europäische Sicherheit 2/98 "Schutztechnologien für Kampf- und Kampfunterstützungsfahrzeuge", Seiten 26 - 31- DE 195 05 629 A1
- armada international 3/1998 "Panzerstahl is not everything", pp. 34 - 46
-
European Safety 2/98 "Protection Technologies for Combat and Battle Support Vehicles", pages 26 - 31 - DE 195 05 629 A1
Grundprinzip der aktiven Selbstschutzsysteme ist eine Sensoranordnung an den gepanzerten Fahrzeugen, die den anfliegenden Flugkörper erfaßt und eine Platten oder Splitter verschießende Abwehrmunition, die von der Sensoranordnung ausgelöst wird und den anfliegenden Flugkörper beschädigt, zerstört oder aus der Flugbahn auslenkt.The basic principle of the active self-protection systems is a sensor arrangement on the armored vehicles, which detects the approaching missile and a plate or splitter firing defensive munitions, which is triggered by the sensor assembly and the approaching missile damaged, destroyed or deflected from the trajectory.
Ein wirksames Gegenmittel besteht darin, zwei Flugkörper kurz hintereinander auf dasselbe Ziel zu schießen. Der erste Flugkörper würde dabei das aktive Selbstschutzsystem auslösen, während der zweite Flugkörper dann auf das ungeschützte Ziel treffen würde. Ein solches Gerät ist aber von einem einzelnen Soldaten, der die Waffe z. B. von der Schulter verschießen soll, nicht einsetzbar.An effective antidote is to shoot two missiles in quick succession at the same target. The first missile would thereby trigger the active self-protection system, while the second missile would hit the unprotected target. However, such a device is of a single soldier, the weapon z. B. shoot from the shoulder, not applicable.
Vielmehr sind spezielle, schwerfällig zu handhabende Abschußgestelle erforderlich.Rather, special, cumbersome to be handled launch racks are required.
Erfindungsgemäß wird deshalb der Flugkörper zur Bekämpfung von Fahrzeugen mit aktivem Selbstschutz nach dem Oberbegriff des Anspruchs 1 mit einer an der Flugkörperspitze lösbar angebrachten, mit Eigenantrieb versehenen Vorrichtung ausgestattet, die sich in geeignetem Abstand vor dem Ziel vom Flugkörper trennt und in so weitem Abstand davon vorne herfliegt, daß das aktive Selbstschutzsystem durch die Vorrichtung ausgelöst wird, ohne den nachfolgenden Flugkörper zu gefährden.According to the invention therefore the missile for fighting vehicles with active self-protection according to the preamble of
Eine derartige Vorrichtung kann aufgrund ihrer Einfachheit und ihres geringen Gewichtes selbst von leichten Flugkörpern, z. B. Panzerabwehrhandwaffen, mitgeführt werden. Vorteilhafterweise wird die erfindungsgemäße Vorrichtung über die in der Regel an der Spitze von Panzerabwehrflugkörpern befindliche rohrförmigen Verlängerung ganz oder teilweise geschoben, so daß sich die Länge des Flugkörpers nur unwesentlich erhöht. Die erfindungsgemäße Vorrichtung kann weiterhin mit Einrichtungen zur Vergrößerung des Radarrückstrahlquerschnittes, z. B. mit einem Reflektor oder Transponder, versehen werden, um die Erkennbarkeit durch die Sensoranordnung des aktiven Selbstschutzsystems zu erhöhen.Such a device, due to its simplicity and low weight even of light missiles, z. B. antitank handguns, be carried. Advantageously, the device according to the invention is wholly or partially pushed over the usually located at the top of antitank missiles tubular extension, so that the length of the missile increases only slightly. The device according to the invention may further comprise means for increasing the Radarrückstrahlquerschnittes, z. B. with a reflector or transponder, be provided to increase the visibility by the sensor arrangement of the active self-protection system.
Der Abstand des Flugkörpers zum Ziel, bei dem sich die erfindungsgemäße Vorrichtung mittels Eigenantrieb vom Flugkörper trennt, wird beispielsweise durch einen Abstandssensor an der Vorrichtung oder am Flugkörper ermittelt. Es kann sich dabei z. B. um einen Laserentfernungsmesser, einen Radarabstandsmesser oder einen optoelektronischen Abstandssensor handeln.The distance of the missile to the target, in which the device according to the invention separates from the missile by means of self-propulsion, is determined, for example, by a distance sensor on the device or on the missile. It may be z. B. be a laser range finder, a radar distance meter or an optoelectronic distance sensor.
Wird jedoch der Flugkörper von einer Startvorrichtung verschossen, die selbst einen Laserentfernungsmesser besitzt, so wird in vorteilhafter Weise die Entfernungsinformation beim Start in den Flugkörper eingegeben, so daß dieser nach entsprechender Flugzeit die erfindungsgemäße Vorrichtung startet. Im Gegensatz zu eigenen Abstandssensoren benötigt der Flugkörper dann nur noch einen Zeitgeber.However, if the missile is fired from a launching device, which itself has a laser rangefinder, so the distance information is entered at start into the missile so that it starts the device according to the invention after a corresponding flight time. In contrast to their own distance sensors, the missile then only needs a timer.
Die Erfindung wird anhand eines Beispiels in Figur 1 näher erläutert:The invention will be explained in more detail with reference to an example in FIG.
Die Figur 1 zeigt in vier Phasen - 1A bis 1D - den Einsatz des erfindungsgemäßen Flugkörpers.Figure 1 shows in four phases - 1A to 1D - the use of the missile according to the invention.
Das Ziel in Form eines Panzers 1 ist mit einer flugkörpererkennenden Sensoranordnung 2 und splitterbildender Abwehrmunition 3, 3', 3" ausgestattet. Der Flugkörper 4 besteht aus einem Raketenmotor 5 mit Leitwerk 6 und einem Gefechtskopf 7. Am vorderen Ende 8 des Gefechtskopfes 7 ist eine mit Eigenantrieb versehene Vorrichtung 9 angeordnet.The target in the form of a
Wie in Fig. 1B dargestellt, wird die Vorrichtung 9, durch einen Raketenmotor 10 angetrieben, vom Flugkörper 4 in Richtung Panzer 1 wegbewegt. Am Flugkörper 4 ist jetzt eine rohrförmige Verlängerung 11 erkennbar, auf die vorher die Vorrichtung 9 aufgesteckt war.As shown in FIG. 1B, the
In Fig. 1C hat die Vorrichtung 9 dazu geführt, daß die Sensoranordnung 2 am Panzer 1 die Abwehrmunition 3' ausgelöst hat, welche am Ort 12 detoniert. Der Abstand 13 zwischen Vorrichtung 9 und Flugkörper 4 ist dabei so groß, daß der Flugkörper 4 durch die Splitter der detonierenden Abwehrmunition 3' nicht oder nur gering gefährdet wird.In Fig. 1C, the
In Fig. 1D ist gezeigt, wie der Gefechtskopf 7 des Flugkörpers 4 am Panzer 1 auftrifft, ohne vorher von der Abwehrmunition 3' (siehe Fig. 1 C) zerstört worden zu sein.FIG. 1D shows how the
Fig. 2 zeigt die Vorrichtung 9 aus Fig. 1 im Schnitt.Fig. 2 shows the
Sie besteht aus einem Rohr 14, das auf die rohrförmige Verlängerung 11 des Flugkörpers 4 aufsteckbar ist (siehe Fig. 1 C).It consists of a
Im vorderen Teil 15 mit Düsen 16, 16' befindet sich ein Raketentreibsatz 17, der durch einen Anzünder 18 angezündet werden kann. Zwischen vorderem Teil 15 und Rohr 14 ist ein Zeitgeber 19 angeordnet, der mit dem Anzünder 18 durch ein Kabel 20 verbunden ist. Der Zeitgeber 19 wird vor dem Start des Flugkörpers 4 über den Anschluß 21 durch eine entsprechende Elektronik am Abschußgestell eingestellt. Der Anschluß 21 kann beispielsweise eine selbstlösende Steckverbindung oder ein induktiver Empfänger sein.In the
Fig. 3 zeigt in Form eines Ablaufprogrammes die Funktion des erfindungsgemäßen Flugkörpers. Die dabei angegebenen Zeiten sind typische Werte für einen ganz bestimmten Panzerabwehrflugkörper. Die angegebenen Bezugszeichen beziehen sich auf die in den Figuren 1 und 2 dargestellten Teile des Flugkörpers 4 und der Vorrichtung 9.Fig. 3 shows in the form of a sequence program, the function of the missile according to the invention. The times given are typical values for a very specific antitank missile. The indicated reference numbers refer to the parts of the
Claims (6)
- A missile having one or more hollow charges, a rocket motor (5) with a horizontal stabilizer (6) and a warhead (7) for combating vehicles with active self-protection, characterized in that, arranged on the tip of the missite, is a removable device (9) self-propelled by a rocket drive which is plugged onto a tubular extension of the missile and becomes detached from the missile at a suitable distance from the target, flies ahead of the missile and triggers the active self-protection without said active self-protection endangering the succeeding missile; wherein the active self-protection system includes a sensor arrangement on the vehicles that detects the approaching device (9) before it hits the vehicle, and comprises a defense ammunition that fires plates or splinters and which is triggered by the sensor arrangement and damages or destroys the approaching device (9) or deflects it out of the flight path.
- The missile according to claim 1, characterized in that the device (9) has an arrangement for measuring the distance to the target, and the device (9) becomes detached from the missile at a predetermined distance.
- The missile according to claim 1 or 2, characterized in that the device (9) or the missile has a timer which can be set remotely, and at the end of the predetermined time the device (9) becomes detached from the missile.
- The missile according to claim 3, characterized in that the timer is set on the basis of a measurement of the distance from the launching frame.
- The missile according to claim 3 or 4, characterized in that the timer is set in a contact-free manner.
- The missile according to any of claims 1 to 5, characterized in that an arrangement for increasing the radar reflecting cross-section is located on the device (9).
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19905268A DE19905268A1 (en) | 1999-02-09 | 1999-02-09 | Missiles to combat vehicles with active self-protection |
DE19905268 | 1999-02-09 | ||
PCT/EP2000/000189 WO2000047945A1 (en) | 1999-02-09 | 2000-01-13 | Missile for combatting vehicles with active self-protection |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1153260A1 EP1153260A1 (en) | 2001-11-14 |
EP1153260B1 true EP1153260B1 (en) | 2005-09-21 |
Family
ID=7896894
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP00904904A Expired - Lifetime EP1153260B1 (en) | 1999-02-09 | 2000-01-13 | Missile for combatting vehicles with active self-protection |
Country Status (5)
Country | Link |
---|---|
EP (1) | EP1153260B1 (en) |
AT (1) | ATE305127T1 (en) |
DE (2) | DE19905268A1 (en) |
ES (1) | ES2246223T3 (en) |
WO (1) | WO2000047945A1 (en) |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1605365A (en) * | 1900-01-01 | |||
US2804823A (en) * | 1955-05-13 | 1957-09-03 | Jablansky Louis | Multiple unit projectile |
FR2280877A1 (en) * | 1974-07-31 | 1976-02-27 | Renard Jean | Missile launching tube system - uses missile launching tubes for or salvo firing of shells from missile |
DE2948542A1 (en) * | 1979-12-03 | 1984-04-12 | Rheinmetall GmbH, 4000 Düsseldorf | BULLET TO FIGHT MULTILAYERED, PREFERRED, ACTIVE ARMOR |
DE3004047C2 (en) * | 1980-02-05 | 1984-10-31 | Rheinmetall GmbH, 4000 Düsseldorf | Armor-piercing projectile |
DE3309147A1 (en) * | 1983-03-15 | 1984-09-20 | Rainer Dipl.-Phys. 6901 Gaiberg Berthold | Method and arrangement for correcting an ignition time |
SE449528B (en) * | 1983-05-13 | 1987-05-04 | Bofors Ab | ARM BREAKING PROJECT |
US4567829A (en) * | 1984-07-30 | 1986-02-04 | General Electric Company | Shaped charge projectile system |
US4638737A (en) * | 1985-06-28 | 1987-01-27 | The United States Of America As Represented By The Secretary Of The Army | Multi-warhead, anti-armor missile |
DE3633535C1 (en) * | 1986-10-02 | 1996-09-26 | Daimler Benz Aerospace Ag | Warhead with initial and main hollow charges |
DE4022820A1 (en) * | 1990-07-18 | 1992-01-23 | Rheinmetall Gmbh | Low calibre stabilised missile mortar for active target - sets wind resistance of leading missile to maintain spacing w.r.t. tailing missile |
DE4117871C1 (en) * | 1991-05-31 | 1999-08-19 | Diehl Stiftung & Co | Hollow charge warhead used as a 'tandem' warhead for triggering reactive armor and then forming a hollow charge spike |
DE4217185C1 (en) * | 1992-05-23 | 1993-10-21 | Deutsche Aerospace | Anti-tank projectile - has detaching head to accelerate ahead and trigger defence systems, to give clear zone for projectile to strike |
DE4331236C1 (en) * | 1993-09-15 | 1996-09-19 | Daimler Benz Aerospace Ag | Active armour-piercing warhead |
DE19505629B4 (en) | 1995-02-18 | 2004-04-29 | Diehl Stiftung & Co.Kg | Protective device against an approaching projectile |
-
1999
- 1999-02-09 DE DE19905268A patent/DE19905268A1/en not_active Withdrawn
-
2000
- 2000-01-13 ES ES00904904T patent/ES2246223T3/en not_active Expired - Lifetime
- 2000-01-13 AT AT00904904T patent/ATE305127T1/en not_active IP Right Cessation
- 2000-01-13 DE DE50011213T patent/DE50011213D1/en not_active Expired - Lifetime
- 2000-01-13 WO PCT/EP2000/000189 patent/WO2000047945A1/en active IP Right Grant
- 2000-01-13 EP EP00904904A patent/EP1153260B1/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
ATE305127T1 (en) | 2005-10-15 |
DE19905268A1 (en) | 2000-08-10 |
DE50011213D1 (en) | 2006-02-02 |
ES2246223T3 (en) | 2006-02-16 |
EP1153260A1 (en) | 2001-11-14 |
WO2000047945A1 (en) | 2000-08-17 |
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