WO2006117037A1 - Camouflage and decoy munitions for protecting objects against guided missiles - Google Patents

Camouflage and decoy munitions for protecting objects against guided missiles Download PDF

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Publication number
WO2006117037A1
WO2006117037A1 PCT/EP2006/002051 EP2006002051W WO2006117037A1 WO 2006117037 A1 WO2006117037 A1 WO 2006117037A1 EP 2006002051 W EP2006002051 W EP 2006002051W WO 2006117037 A1 WO2006117037 A1 WO 2006117037A1
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WO
WIPO (PCT)
Prior art keywords
camouflage
ammunition
hot
hot spots
deception
Prior art date
Application number
PCT/EP2006/002051
Other languages
German (de)
French (fr)
Inventor
Norbert Wardecki
Stefan Lauer
Klaus Hieke
Original Assignee
Rheinmetall Waffe Munition Gmbh
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Rheinmetall Waffe Munition Gmbh filed Critical Rheinmetall Waffe Munition Gmbh
Priority to DE502006007778T priority Critical patent/DE502006007778D1/en
Priority to EP06723251A priority patent/EP1875152B1/en
Priority to JP2008508092A priority patent/JP2008538808A/en
Priority to US11/919,460 priority patent/US20090301336A1/en
Publication of WO2006117037A1 publication Critical patent/WO2006117037A1/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B5/00Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/02Cartridges, i.e. cases with charge and missile
    • F42B5/145Cartridges, i.e. cases with charge and missile for dispensing gases, vapours, powders, particles or chemically-reactive substances
    • F42B5/15Cartridges, i.e. cases with charge and missile for dispensing gases, vapours, powders, particles or chemically-reactive substances for creating a screening or decoy effect, e.g. using radar chaff or infrared material
    • 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
    • F42B12/56Projectiles, 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
    • F42B12/70Projectiles, 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 for dispensing radar chaff or infrared material

Definitions

  • the invention relates to a camouflage and deception ammunition for the protection of objects against missiles, the fog and / or dummy targets forming agents that produce Täusch bine that affect the location of the missile.
  • camouflage and deception ammunition is used in a known manner, which forms an artificial fog or fake targets, from which the approaching missile is deflected due to target-like signals.
  • an ammunition for generating a mist which contains both a fog and an IR active mass.
  • EP 0 512 202 a method for protecting objects emitting IR radiation against missiles is known, in which the missile is located from the object to be protected, and then projectiles are launched which generate spurious radiation clouds.
  • the Störstrahlungswolke initially sends a short time a strong IR radiation from which the Aufschalt- and tracking electronics of the seeker head of the missile is disturbed. Subsequently, several large-area and homogeneous pyrotechnic, the IR signature of the object in approximately similar infrared decoy target clouds are generated.
  • Jammers are lamps that are attached to the target and emit homogeneous or pulsed light signals in the desired spectral range. It is also known, such deflection effects by To produce pyrotechnic torches or light-body, which are burned or fired at the vehicle to be protected.
  • Shed filaments have the disadvantage that they must be fired as additional ammunition with the other defenses with and thus increases the cost significantly. Furthermore, they have the disadvantage that they form a single ongoing hotspot that can be detected and suppressed by modern missile detection systems.
  • the invention is therefore based on the object to provide a camouflage and Täuschmunition for the protection of objects against missiles, which offers the broadest possible protection.
  • camouflage and Täuschmunition in addition to fog and / or sham targets forming active ingredients additionally contain pyrotechnic luminous or luminous active materials that produce a variety of distributed in space hot spots.
  • the deflection effect is integrated by hot spots in a camouflage and Täuschmunition.
  • the camouflage and deception ammunition according to the invention provides comprehensive protection by camouflaging both the threatened object, as well as the desired deception signals structuristingt. For this purpose, many hot spots are simultaneously generated as deceptive signals.
  • the deception signals can be generated directly when the ammunition is launched and / or on its trajectory and / or when dismantling the ammunition.
  • the distracting lighting effect can thus act at different locations and at different times in order to deceive different missiles with different approaches (flat approach, excessive approach, etc.).
  • lighting effects can be generated directly on the target object, for example a vehicle, or starting from the target object in the air or at a distance from the target object in the air, in particular from the disassembly point to the ground.
  • the deflection effect is independent of the flight principle in the LOS (line of sight) of the missile location.
  • the burnup is controlled so that instead of a sustained radiation pulsating radiation is emitted. This is also effective against modern tracking devices that can detect and isolate persistent signals.
  • the integration of the hot-spot builders in the stealth and deception ammunition can be realized in various ways, which can also be combined with each other:
  • the granules which supplement the ejection charge can be supplemented on the basis of phosphorus red or on the basis of flares and / or IR flares, in order to achieve optimum effect in the desired wavelength range.
  • light metals such as magnesium and / or aluminum about 5% binder such as aqueous dispersion adhesive
  • metal powder such as silicon and / or boron
  • binders such as rubber accroides, polyvinyl butyrate Second
  • binders such as rubber accroides, polyvinyl butyrate
  • Example for the formulation of granules or pellets 50-80% barium nitrate 20-50% magnesium 0-10% binder
  • light metals such as magnesium and / or aluminum
  • binder such as aqueous dispersion adhesive

Abstract

The invention relates to camouflage and decoy munitions for protecting objects against guided missiles comprising mist and/or target-imitation forming active materials and additional pyrotechnical lighting bodies producing a plurality of hot spots dispersed in the space. The hot-spot producing active material can be embodied in such a way that it is provided with pulsed fire.

Description

B E S C H R E I B U N G DESCRIPTION
Tarn- und Täuschmunition zum Schutz von Objekten gegen LenkflugkörperCamouflage and deception ammunition for the protection of objects against missiles
Die Erfindung betrifft eine Tarn- und Täuschmunition zum Schutz von Objekten gegen Lenkflugkörper, die Nebel und/oder Scheinziele bildende Wirkstoffe enthält, die Täuscheffekte erzeugen, welche die Eigenortung der Lenkflugkörper beeinflussen.The invention relates to a camouflage and deception ammunition for the protection of objects against missiles, the fog and / or dummy targets forming agents that produce Täuscheffekte that affect the location of the missile.
Zum Schutz von Objekten gegen Lenkflugkörper wird bekannter Weise Tarn- und Täuschmunition eingesetzt, die einen künstlichen Nebel oder Scheinziele bildet, von denen der anfliegende Flugkörper aufgrund zielähnlicher Signale abgelenkt wird.To protect objects against missiles, camouflage and deception ammunition is used in a known manner, which forms an artificial fog or fake targets, from which the approaching missile is deflected due to target-like signals.
So ist aus der DE 100 65 816 A eine Munition zur Erzeugung eines Nebels bekannt, die sowohl eine Nebel- als auch eine IR-Wirkmasse enthält. Aus der EP 0 512 202 ist ein Verfahren zum Schützen von einer IR-Strahlung abgebenden Objekten gegen Flugkörper bekannt, bei dem vom zu schützenden Objekt aus der Flugkörper geortet und anschließend Wurfkörper abgeschossen werden, die Störstrahlungswolken erzeugen. Die Störstrahlungswolke sendet zunächst kurzzeitig eine starke IR-Strahlung aus, von der die Aufschalt- und Verfolgungselektronik des Suchkopfes des Flugkörpers gestört wird. Anschließend werden mehrere großflächige und homogene pyrotechnische, der IR-Signatur des Objekts in etwa ähnelnde Infrarot- Scheinzielwolken erzeugt.Thus, from DE 100 65 816 A an ammunition for generating a mist is known, which contains both a fog and an IR active mass. From EP 0 512 202, a method for protecting objects emitting IR radiation against missiles is known, in which the missile is located from the object to be protected, and then projectiles are launched which generate spurious radiation clouds. The Störstrahlungswolke initially sends a short time a strong IR radiation from which the Aufschalt- and tracking electronics of the seeker head of the missile is disturbed. Subsequently, several large-area and homogeneous pyrotechnic, the IR signature of the object in approximately similar infrared decoy target clouds are generated.
Werden Lenkflugkörper beim Zielanflug durch Anmessen von Hot-Spots im Heck der Rakete geortet und in Abhängigkeit von der jeweiligen Position ins Ziel gesteuert, so ist es bekannt, durch Erzeugung von Hot-Spots, die im gleichen Wellenbereich wirken, das Steuersystem der Rakete zu täuschen. Durch das Anmessen eines falschen Hot-Spots wird ein falsches Steuersignal erzeugt, und die Rakete wird abgelenkt.When guided missiles are tracked on target approach by sensing hot spots in the tail of the missile and steered to the target depending on the particular position, it is known to deceive the missile's control system by creating hot spots acting in the same waveband , Sensing a wrong hotspot will generate an incorrect control signal and deflect the missile.
Um derartige Ablenkeffekte zu erzeugen, sind sogenannte Jammer bekannt. Jammer sind Lampen, die am Ziel angebracht sind und im gewünschten Spektralbereich homogene oder getaktete Leuchtsignale aussenden. Ebenso ist es bekannt, derartige Ablenkeffekte durch pyrotechnische Fackeln oder Leuchtflugkörper zu erzeugen, die am zu schützenden Fahrzeug abgebrannt oder von diesen verschossen werden.In order to produce such deflection effects, so-called jammers are known. Jammers are lamps that are attached to the target and emit homogeneous or pulsed light signals in the desired spectral range. It is also known, such deflection effects by To produce pyrotechnic torches or light-body, which are burned or fired at the vehicle to be protected.
Elektronische Jammer und pyrotechnische Fackeln haben den Nachteil, dass sie nur einen Ablenkpunkt darstellen. Auch können diese ortsfesten Jammer und pyrotechnischen Fackeln ausgeklärt und als besondere Zielsignatur verwendet werden. Bei überhöhtem Anflug der Flugkörper bietet diese Maßnahme daher auch keinen Schutz.Electronic jammers and pyrotechnic torches have the disadvantage that they only represent a deflection point. These stationary jamming and pyrotechnic torches can also be clarified and used as a special target signature. With excessive approach of the missile, this measure therefore also provides no protection.
Verschossene Leuchtkörper haben den Nachteil, dass sie als zusätzliche Munition mit den anderen Abwehrmaßnahmen mit verschossen werden muss und sich damit der Aufwand deutlich erhöht. Weiterhin haben sie den Nachteil, dass sie einen einzigen andauernden Hot- Spot bilden, der durch moderne Raketenortungssysteme erkannt und unterdrückt werden kann.Shed filaments have the disadvantage that they must be fired as additional ammunition with the other defenses with and thus increases the cost significantly. Furthermore, they have the disadvantage that they form a single ongoing hotspot that can be detected and suppressed by modern missile detection systems.
Der Erfindung liegt daher die Aufgabe zu Grunde, eine Tarn- und Täuschmunition zum Schutz von Objekten gegen Lenkflugkörper bereitzustellen, die einen möglichst umfassenden Schutz bietet.The invention is therefore based on the object to provide a camouflage and Täuschmunition for the protection of objects against missiles, which offers the broadest possible protection.
Diese Aufgabe wird nach der Erfindung dadurch gelöst, dass die Tarn- und Täuschmunition neben Nebel und/oder Scheinziele bildenden Wirkstoffen zusätzlich pyrotechnische Leuchtkörper oder Leuchtwirkmassen enthalten, die eine Vielzahl von im Raum verteilten Hot- Spots erzeugen.This object is achieved according to the invention in that the camouflage and Täuschmunition in addition to fog and / or sham targets forming active ingredients additionally contain pyrotechnic luminous or luminous active materials that produce a variety of distributed in space hot spots.
Nach der Erfindung wird somit die Ablenkwirkung durch Hot-Spots in eine Tarn- und Täuschmunition integriert. Die Tarn- und Täuschmunition nach der Erfindung bietet einen umfassenden Schutz, indem sie sowohl das bedrohte Objekt tarnt, als auch die gewünschten Täuschsignale ausbringt. Dazu werden gleichzeitig viele Hot-Spots als Täuschsignale erzeugt. Dabei lassen sich die Täuschsignale unmittelbar beim Abschuss der Munition und/oder auf deren Flugbahn und/oder beim Zerlegen der Munition erzeugen. Die ablenkende Leuchtwirkung kann so an unterschiedlichen Orten und zu unterschiedlichen Zeiten wirken, um verschiedene Flugkörper mit verschiedenen Anflugbahnen (flacher Anflug, überhöhter Anflug etc.) zu täuschen. Somit können Leuchtwirkungen direkt am Zielobjekt, beispielsweise einem Fahrzeug, erzeugt werden, oder vom Zielobjekt ausgehend in die Luft oder auch mit Abstand vom Zielobjekt in der Luft, insbesondere vom Zerlegungspunkt bis hin zum Boden. Somit lässt sich sicherstellen, dass die Ablenkwirkung unabhängig vom Flugprinzip in der LOS (Line of Sight) der Flugkörperortung erfolgt. In einer besonderen Ausführung wird der Abbrand so gesteuert, dass anstelle einer anhaltenden Strahlung eine pulsierende Strahlung abgegeben wird. Diese ist auch gegen moderne Ortungsgeräte wirksam, die anhaltende Signale detektieren und aussondern können.According to the invention thus the deflection effect is integrated by hot spots in a camouflage and Täuschmunition. The camouflage and deception ammunition according to the invention provides comprehensive protection by camouflaging both the threatened object, as well as the desired deception signals auszustingt. For this purpose, many hot spots are simultaneously generated as deceptive signals. The deception signals can be generated directly when the ammunition is launched and / or on its trajectory and / or when dismantling the ammunition. The distracting lighting effect can thus act at different locations and at different times in order to deceive different missiles with different approaches (flat approach, excessive approach, etc.). Thus, lighting effects can be generated directly on the target object, for example a vehicle, or starting from the target object in the air or at a distance from the target object in the air, in particular from the disassembly point to the ground. Thus, it can be ensured that the deflection effect is independent of the flight principle in the LOS (line of sight) of the missile location. In a particular embodiment of the burnup is controlled so that instead of a sustained radiation pulsating radiation is emitted. This is also effective against modern tracking devices that can detect and isolate persistent signals.
Die Integration der Hot-Spot-Bildner in die Tarn- und Täuschmunition lässt sich auf verschiedene Weisen realisieren, die auch miteinander kombiniert werden können:The integration of the hot-spot builders in the stealth and deception ammunition can be realized in various ways, which can also be combined with each other:
1.1.
Ergänzung der Ausstoßladung der Munition um ein Hot-Spot-Granulat, das in dem gewünschte Wellenbereich wirkt:Complementing the discharge charge of the ammunition by a hot-spot granule, which acts in the desired wave range:
Das die Ausstoßladung ergänzende Granulat kann dabei auf Basis Phosphor rot oder auf Basis von Leuchtsätzen und/oder IR-Leuchtsätzen ergänzt werden, um im gewünschten Wellenbereich optimale Wirkung zu erzielen.The granules which supplement the ejection charge can be supplemented on the basis of phosphorus red or on the basis of flares and / or IR flares, in order to achieve optimum effect in the desired wavelength range.
Beispiel für Leuchtkörper auf Basis Phosphor rot:Example of luminous bodies based on phosphorus red:
60-80% Phosphor rot60-80% phosphorus red
30-10% Nitrate der ersten und zweiten Hauptgruppe30-10% nitrates of the first and second main groups
5-10% Leichtmetalle wie Magnesium und/oder Aluminium ca.5% Bindemittel wie wässriger Dispersionskleber5-10% light metals such as magnesium and / or aluminum about 5% binder such as aqueous dispersion adhesive
Beispiel für Leuchtkörper auf Basis IR-Leuchtsatz:Example of luminaires based on IR illuminant:
50-70% Kaliumnitrat50-70% potassium nitrate
20-10% Hexamethylentetramin20-10% hexamethylenetetramine
5-10% Diazidicarbonamid5-10% diazidicarbonamide
1-5% Metallpulver wie Silizium und/oder Bor1-5% metal powder such as silicon and / or boron
1-5% Bindemittel wie Gummi accroides, Polyvinylbutyrat 2.1-5% binders such as rubber accroides, polyvinyl butyrate Second
Anbringung eines Pellets zur Erzeugung einer Leuchtspur in Form von Hot-Spots an der zu verschießenden Patrone.Attaching a pellet to create a trail of light in the form of hot spots on the cartridge to be fired.
Beispiel für die Rezeptur von Pellets:Example for the recipe of pellets:
50-70% Kaliumnitrat50-70% potassium nitrate
20-10% Hexamethylentetramin20-10% hexamethylenetetramine
5-10% Diazidicarbonamid5-10% diazidicarbonamide
2-5% Metallpulver wie Silizium und/oder Bor2-5% metal powders such as silicon and / or boron
1-5% Bindemittel wie Gummi accroides, Polyvinylbutyrat1-5% binders such as rubber accroides, polyvinyl butyrate
3.Third
Zugabe von Granulaten oder Pellets zu der Zerlegerladung, die im gewünschten Wellenlängenbereich Hot-Spots erzeugen:Adding granules or pellets to the disintegrator charge that produce hot spots in the desired wavelength range:
Beispiel für die Rezeptur von Granulaten oder Pellets: 50-80% Bariumnitrat 20-50% Magnesium 0-10% BindemittelExample for the formulation of granules or pellets: 50-80% barium nitrate 20-50% magnesium 0-10% binder
4.4th
Einlaborieren von Hot-Spots erzeugenden Flares oder Pellets in die Nebel oder Scheinziele bildenden Wirkstoffe.Laboratory preparation of hotspots producing flares or pellets in the nebulas or sham targets.
Beispiel für die Rezeptur von Flares oder Pellets: 60-80% Phosphor rotExample for the formulation of flares or pellets: 60-80% phosphorus red
5-20% Nitrate der ersten und zweiten Hauptgruppe5-20% nitrates of the first and second main groups
0-10% Leichtmetalle wie Magnesium und/oder Aluminium0-10% light metals such as magnesium and / or aluminum
5-20% Bindemittel wie wässriger Dispersionskleber 5-20% binder such as aqueous dispersion adhesive

Claims

P A T E N T A N S P R Ü C H E PATENT APPLICATIONS
1.1.
Tarn- und Täuschmunition zum Schutz von Objekten gegen Lenkflugkörper, die Nebel und/oder Scheinziele bildende Wirkstoffe enthält, dadurch gekennzeichnet, dass die Munition zusätzlich pyrotechnische Leuchtkörper enthält, die eine Vielzahl von im Raum verteilten Hot-Spots erzeugen.Camouflage and deception ammunition for the protection of objects against missiles, the fog and / or dummy targets forming active ingredients, characterized in that the ammunition additionally contains pyrotechnic luminous bodies that produce a variety of hot spots distributed in space.
2.Second
Tarn- und Täuschmunition nach Patentanspruch 1 , dadurch gekennzeichnet, dass die Ausstoßladung der Munition um ein Hot-Spot-Granulat ergänzt ist, das in dem gewünschten Wellenbereich wirkt.Camouflage and deception ammunition according to claim 1, characterized in that the ejection charge of the ammunition is supplemented by a hot-spot granules which acts in the desired wavelength range.
3.Third
Tarn- und Täuschmunition nach Patentanspruch 1 oder 2, dadurch gekennzeichnet, dassCamouflage and Täuschmunition according to claim 1 or 2, characterized in that
Pellets zur Erzeugung von Hot-Spots an der zu verschießenden Patrone angebracht sind.Pellets for generating hot spots are attached to the cartridge to be fired.
4.4th
Tarn- und Täuschmunition nach einem der Patentansprüche 1 bis 3, dadurch gekennzeichnet, dass der Zerlegerladung der Munition Granulate oder Pellets zugegeben sind, die im gewünschten Wellenlängenbereich Hot-Spots erzeugen.Camouflage and Täuschmunition according to one of the claims 1 to 3, characterized in that the burster charge of the ammunition granules or pellets are added, which produce hot spots in the desired wavelength range.
5.5th
Tarn- und Täuschmunition nach einem der Patentansprüche 1 bis 4, dadurch gekennzeichnet, dass Hot-Spots erzeugende Flares oder Pellets in die Nebel oder Scheinziele bildenden Wirkstoffe der Munition einlaboriert sind.Camouflage and deception ammunition according to one of the claims 1 to 4, characterized in that hot-spots generating flares or pellets are incorporated into the nebulosic or sham-forming agents of ammunition.
6.6th
Tarn- und Täuschmunition nach einem der Patentansprüche 1 bis 5, dadurch gekennzeichnet, dass die Hot-Spots erzeugende Wirkmasse nicht kontinuierlich, sondern pulsierend abbrennt. Camouflage and Täuschmunition according to one of the claims 1 to 5, characterized in that the hot spots generating active mass burns not pulsating but continuously.
PCT/EP2006/002051 2005-04-29 2006-03-07 Camouflage and decoy munitions for protecting objects against guided missiles WO2006117037A1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
DE502006007778T DE502006007778D1 (en) 2005-04-29 2006-03-07 TARN AND DOCKING AMMUNITION FOR THE PROTECTION OF OBJECTS AGAINST HANDLEBAR BODIES
EP06723251A EP1875152B1 (en) 2005-04-29 2006-03-07 Camouflage and decoy munitions for protecting objects against guided missiles
JP2008508092A JP2008538808A (en) 2005-04-29 2006-03-07 Camouflage and decoy munitions to protect targets from guided missiles
US11/919,460 US20090301336A1 (en) 2005-04-29 2006-03-07 Camouflage and decoy munitions for protecting objects against guided missiles

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102005020159.8 2005-04-29
DE102005020159A DE102005020159B4 (en) 2005-04-29 2005-04-29 Camouflage and deception ammunition for the protection of objects against missiles

Publications (1)

Publication Number Publication Date
WO2006117037A1 true WO2006117037A1 (en) 2006-11-09

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Country Link
US (1) US20090301336A1 (en)
EP (1) EP1875152B1 (en)
JP (1) JP2008538808A (en)
DE (2) DE102005020159B4 (en)
WO (1) WO2006117037A1 (en)

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EP1875152A1 (en) 2008-01-09
DE102005020159B4 (en) 2007-10-04

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