EP1762815A1 - Munition with seeking fuze - Google Patents
Munition with seeking fuze Download PDFInfo
- Publication number
- EP1762815A1 EP1762815A1 EP06018435A EP06018435A EP1762815A1 EP 1762815 A1 EP1762815 A1 EP 1762815A1 EP 06018435 A EP06018435 A EP 06018435A EP 06018435 A EP06018435 A EP 06018435A EP 1762815 A1 EP1762815 A1 EP 1762815A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- projectile
- ammunition
- search
- rear part
- finder
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Images
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
-
- 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
Definitions
- the invention relates to a search detonator ammunition according to the preamble of claim 1.
- a search fuse ammunition and a method for controlling armored target objects by means of such a dephase-correctable search fuse ammunition is known from DE 35 16 673 C2 known.
- This known search detonator ammunition has a parachute and is characterized in that it is equipped with means for canceling or re-starting the action of the parachute and with at least one pulse generator for introducing a quasi-ballistic trajectory from a braked by the parachute sink phase.
- the DE 41 04 800 C2 describes a device for real-time field reconnaissance by means of at least one sensor which can be brought as a load body from a carrier projectile like a submunition and its information can be transmitted via a relay to a remote receiving station, each sensor and the relay as equipped with descent braking means load body are designed an artillery carrier projectile that are releasable after Verschuss over a target area to be verified from the carrier projectile.
- the relay is equipped with a braking device for a much lower rate of descent than the rotating and thereby the target area spirally narrowing scanning sensor.
- the DE 44 26 014 A1 discloses a system for protecting a target such as an armored vehicle, a bunker or the like against missiles having a launching container movably mounted on a base portion with at least one launching tube for an associated fragmentation grenade, sensor means for detecting the target to be counteracted and the alignment of the launching container the object to be combated, and a drive device connected to the sensor device via a signal processing device and a control device for aligning the firing container relative to the base part, wherein the at least one fragmentation grenade is provided with a splitter assignment and an ignition device for controlling the ignition timing.
- a reconnaissance device with a sensor unit for detecting and locating targets which is transportable and releasable together with a deployable, fall-retardant device in an artillery projectile, and which is provided with a braking screen and a Entdrallvorraum is from the DE 196 13 492 C2 known.
- a 155 mm fuselage ammunition for artillery is known as SMArt 155.
- This known search detonator ammunition has a head detonator for a back of this subsequent ejection unit, with the aid of axially successively arranged in a housing shell submunitions are ejected from the rear of the case.
- the submunitions each have an unwrapping device and a rotation parachute as a case-delaying device and sensors for target detection.
- the invention has for its object to provide a search detonator ammunition of the type mentioned, which is also formed in a dimensioning with a relatively small caliber with an optimally effective projectile-forming insert.
- the invention search fuzes ammunition is formed vollkalibrig without housing sleeve, there is the advantage that the front projectile-forming insert can be dimensioned with a relatively large diameter, so that after ignition of the projectilrelienden deposit associated explosive charge optimal projectile formation is possible because of the dimensions the insert is not limited by a housing sleeve, ie is limited.
- the search engine ammunition according to the invention has only a single projectile-forming deposit.
- the emission of the submunition is not effected by means of a detonator - such as e.g. in SMArt 155 - but by means of a bottom igniter, which is arranged in the rear part of the search detonator ammunition and associated with a peripheral around the search detonator ammunition predetermined breaking section which is formed between the search detonator ammunition and the rear part.
- search detonator ammunition Since no head detonator but a bottom detonator is used in the search detonator ammunition according to the invention, it is also possible in an advantageous manner to form the search detonator ammunition on the front side with a ballistic hood permeable to radar beams of the sensor device.
- This ballistic hood is preferably made of a suitable plastic material and can easily be penetrated by the projectile-forming insert or the projectile formed from the insert after ignition of the projectile-forming insert associated explosive charge.
- the rear part is preferably formed with a deployable tail, which is arranged underkalibrig in the inactive state of the invention search fuzed ammunition.
- a deployable tail which is arranged underkalibrig in the inactive state of the invention search fuzed ammunition.
- the search detonator ammunition according to the invention may have, for example, the caliber 120 mm. Of course, she can also have a different caliber.
- FIG. 1 shows an embodiment of the search detonator ammunition 10, which has a projectile-forming insert 12 on a projectile 44 on the front side.
- An explosive charge 14 for the projectile-forming insert 12 adjoins the insert 12 at the rear.
- the explosive charge 14 is associated with an ignition device 16. With the ignition device 16, a sensor device 18 is operatively connected, with which a target to be combated is sensed.
- the search detonator ammunition 10 also has a de-twisting device 20 and a braking device 22 for braking the falling speed of the search detonator ammunition 10. All of these components are known, for example, from the SMArt 155, so that it is unnecessary to describe them in detail; they are not the subject of the present invention.
- the subject of the present invention is in particular that the search detonator ammunition 10 is formed fully caliber without own housing sleeve in order to be able to dimension the projectile-forming insert with a correspondingly large diameter.
- the rear part 24 has an ejection tube 42. This is connected to the search detonator ammunition 10 along a circumferential predetermined breaking section 26 with a housing 44.
- the predetermined breaking section 26 can be separated by means of a bottom igniter 28 provided with discharge charge 36 in the tail section 24, in order to separate the search detonator ammunition 10 from the rear part 24.
- the predetermined breaking point 26 is gas-tight and firing resistant. It is designed either as a threaded connection or as a welded joint. It can also consist of a joining element made of plastic.
- the bottom igniter 28 is connected to a connection cable 30 in order to be able to program the bottom igniter 28 appropriately. Another possibility is to program the base igniter 28 inductively.
- the base igniter 28 ignites both the ejection charge 36 and starts the time function of the sensor and ignition device 16, 18 via a cable, not shown.
- the bottom 40 is fixedly connected to a cover 50 of the braking device 22.
- Pyrotechnically ignitable separating screws 44, 46 activate the braking device 22 and, later in time, the untwisting device 20.
- the rear part 24 has a deployable tail 32, which is drawn in the figure 1 in the established active state. In the inactive state, the wings of the tail 32 are underkalibrig at the rear part 24.
- the search detonator ammunition 10 has a ballistic hood 34 made of a suitable plastic material, which is permeable to radar beams of the sensor device 18.
- the tail 32 After completion of the search fuzes ammunition 1 from a gun barrel, the tail 32 is placed by centrifugal forces or by spring force.
- the projectile 44 On the trajectory, close to the target, the projectile 44 is discharged, see FIG. 2.
- the bottom igniter 28 ignites the ejection charge 36. Its gas pressure leads to the separation of the predetermined breaking point 26 and the ejection of the projectile 44 from the ejection tube 42.
- the braking device 22 After ignition of the separating screw 44, the braking device 22 is ejected. In this case, the lid 50 is removed with the bottom 40 in the axial direction.
- the Entdrallcrafted 20 is activated by ignition of the separating screw 46.
- the ignition of the explosive charge 14 takes place at the optimized distance with deformation of the insert 12 to a target-projectile projectile.
- the guide length 52 of the projectile 44 in the launch tube 42 corresponds to 1.1 times the Geschoßkalibers 54. This torque-free ejection of the projectile 44 and separation of the projectile 44 is ensured by the rear part 24.
Abstract
Description
Die Erfindung betrifft eine Suchzündermunition gemäß dem Oberbegriff des Anspruches 1.The invention relates to a search detonator ammunition according to the preamble of claim 1.
Eine Suchzündermunition und ein Verfahren zum Bekämpfen gepanzerter Zielobjekte mittels einer solchen Entphasen-korrigierbaren Suchzündermunition ist aus der
Die
Die
Eine Aufklärungseinrichtung mit einer Sensoreinheit zum Detektieren und Lokalisieren von Zielen, die zusammen mit einer entfaltbaren, fallverzögernden Einrichtung in einem Artilleriegeschoß transportierbar und aus diesem freigebbar ist, und die mit einem Bremsschirm und einer Entdrallvorrichtung versehen ist, ist aus der
Eine Suchzündermunition für Artillerie des Kalibers 155 mm ist als SMArt 155 bekannt. Diese bekannte Suchzündermunition weist einen Kopfzünder für eine an diesen rückseitig anschließende Ausstoßeinheit auf, mit deren Hilfe axial hintereinander in einer Gehäusehülle angeordnete Submunitionen rückseitig aus der Gehäusehülle ausgestoßen werden. Die Submunitionen weisen jeweils eine Entdralleinrichtung und einen Rotationsfallschirm als fallverzögernde Einrichtung sowie Sensoren zur Zielerfassung auf.A 155 mm fuselage ammunition for artillery is known as SMArt 155. This known search detonator ammunition has a head detonator for a back of this subsequent ejection unit, with the aid of axially successively arranged in a housing shell submunitions are ejected from the rear of the case. The submunitions each have an unwrapping device and a rotation parachute as a case-delaying device and sensors for target detection.
Die Ausbildung dieser bekannten Suchzündermunition mit in einer Gehäusehülse vorgesehenen Submunitionen, wobei jede Submunition vorderseitig eine projektilbildende Einlage aufweist, ist bei einer SMArt 155 infolge des relativ großen Durchmessers problemlos möglich. Bei einer Suchzündermunition eines kleineren Kalibers müsste jedoch bei Anwendung des gleichen Konstruktionsprinzipes mit einer Gehäusehülse der Durchmesser der projektilbildenden Einlage entsprechend reduziert sein. Eine solche Reduktion des Durchmessers der projektilbildenden Einlage würde jedoch in einer Reduktion der Eindring- bzw. Durchdringtiefe des aus der Einlage gebildeten Projektiles resultieren.The formation of this known search detonator ammunition with submunitions provided in a housing sleeve, each submunition having on the front side a projectile-forming insert, is easily possible with an SMArt 155 due to the relatively large diameter. In a search detonator ammunition of a smaller caliber, however, the diameter of the projectile-forming insert would have to be correspondingly reduced when using the same design principle with a housing sleeve. Such a reduction of the diameter of the projectile-forming insert, however, would result in a reduction of the penetration or penetration depth of the projectile formed from the insert.
In Kenntnis dieser Gegebenheiten liegt der Erfindung die Aufgabe zugrunde, eine Suchzündermunition der eingangs genannten Art zu schaffen, die auch bei einer Dimensionierung mit einem relativ kleinen Kaliber mit einer optimal wirksamen projektilbildenden Einlage ausgebildet ist.In view of these circumstances, the invention has for its object to provide a search detonator ammunition of the type mentioned, which is also formed in a dimensioning with a relatively small caliber with an optimally effective projectile-forming insert.
Diese Aufgabe wird durch die Merkmale des Anspruches 1 gelöst. Bevorzugte Aus- bzw. Weiterbildungen der erfindungsgemäßen Suchzündermunition sind in den Unteransprüchen gekennzeichnet.This object is solved by the features of claim 1. Preferred embodiments or further developments of the search detonator ammunition according to the invention are characterized in the subclaims.
Dadurch, dass die erfindungsgemäße Suchzündermunition vollkalibrig ohne Gehäusehülse ausgebildet ist, ergibt sich der Vorteil, dass die vorderseitige projektilbildende Einlage mit einem relativ großen Durchmesser dimensioniert sein kann, so dass nach Zünden der zur projetilbildenden Einlage zugehörigen Sprengladung eine optimale Projektilbildung möglich ist, weil die Dimensionierung der Einlage nicht durch eine Gehäusehülse eingeschränkt, d.h. begrenzt wird.Due to the fact that the invention search fuzes ammunition is formed vollkalibrig without housing sleeve, there is the advantage that the front projectile-forming insert can be dimensioned with a relatively large diameter, so that after ignition of the projetilbildenden deposit associated explosive charge optimal projectile formation is possible because of the dimensions the insert is not limited by a housing sleeve, ie is limited.
Die erfindungsgemäße Suchzündermunition weist nur eine einzige projektilbildende Einlage auf. Der Ausstoß der Submunition erfolgt erfindungsgemäß nicht mittels eines Kopfzünders - wie z.B. bei SMArt 155 - sondern mittels eines Bodenzünders, der im Heckteil der Suchzündermunition angeordnet und einem um die Suchzündermunition umlaufenden Sollbruchabschnitt zugeordnet ist, der zwischen der Suchzündermunition und dem Heckteil ausgebildet ist.The search engine ammunition according to the invention has only a single projectile-forming deposit. According to the invention, the emission of the submunition is not effected by means of a detonator - such as e.g. in SMArt 155 - but by means of a bottom igniter, which is arranged in the rear part of the search detonator ammunition and associated with a peripheral around the search detonator ammunition predetermined breaking section which is formed between the search detonator ammunition and the rear part.
Nachdem bei der erfindungsgemäßen Suchzündermunition kein Kopfzünder sondern ein Bodenzünder zur Anwendung gelangt, ist es in vorteilhafter Weise außerdem möglich, die Suchzündermunition vorderseitig mit einer für Radarstrahlen der Sensoreinrichtung durchlässigen ballistischen Haube auszubilden. Diese ballistische Haube besteht vorzugsweise aus einem geeigneten Kunststoffmaterial und kann nach Zünden der zur projektilbildenden Einlage zugehörigen Sprengladung von der projektilbildenden Einlage bzw. dem aus der Einlage gebildeten Projektil problemlos durchdrungen werden.Since no head detonator but a bottom detonator is used in the search detonator ammunition according to the invention, it is also possible in an advantageous manner to form the search detonator ammunition on the front side with a ballistic hood permeable to radar beams of the sensor device. This ballistic hood is preferably made of a suitable plastic material and can easily be penetrated by the projectile-forming insert or the projectile formed from the insert after ignition of the projectile-forming insert associated explosive charge.
Erfindungsgemäß ist das Heckteil vorzugsweise mit einem aufstellbaren Leitwerk ausgebildet, das im inaktiven Zustand der erfindungsgemäßen Suchzündermunition unterkalibrig angeordnet ist. Durch eine solche Ausbildung ist es in vorteilhafter Weise möglich, die Suchzündermunition aus Waffenrohren ohne Drall, wie den Waffenrohren von Kampfpanzern zu verschießen.According to the invention, the rear part is preferably formed with a deployable tail, which is arranged unterkalibrig in the inactive state of the invention search fuzed ammunition. Such a design, it is possible in an advantageous manner to shoot the search detonator ammunition from gun barrels without swirl, such as the gun barrels of main battle tanks.
Die erfindungsgemäße Suchzündermunition kann z.B. das Kaliber 120 mm besitzen. Selbstverständlich kann sie auch ein anderes Kaliber besitzen.The search detonator ammunition according to the invention may have, for example, the caliber 120 mm. Of course, she can also have a different caliber.
Weitere Einzelheiten, Merkmale und Vorteile ergeben sich aus der nachfolgenden Beschreibung eines in der Zeichnung dargestellten Ausführungsbeispieles.Further details, features and advantages will become apparent from the following description of an embodiment shown in the drawing.
Es zeigt:
- Figur 1
- eine Suchzündermunition im Längsschnitt,
- Figur 2
- die Munition nach Figur 1 während des Ausstoßes und
- Figur 3
- die ausgestoßene Munition
- FIG. 1
- a search fuse ammunition in longitudinal section,
- FIG. 2
- the ammunition of Figure 1 during the ejection and
- FIG. 3
- the ejected ammunition
Die Figur 1 zeigt eine Ausbildung der Suchzündermunition 10, die vorderseitig an einem Geschoss 44 eine projektilbildende Einlage 12 aufweist. An die Einlage 12 grenzt rückseitig eine Sprengladung 14 für die projektilbildende Einlage 12 an. Der Sprengladung 14 ist eine Zündeinrichtung 16 zugeordnet. Mit der Zündeinrichtung 16 ist eine Sensoreinrichtung 18 wirkverbunden, mit der ein zu bekämpfendes Ziel sensiert wird.FIG. 1 shows an embodiment of the
Die Suchzündermunition 10 weist außerdem eine Entdralleinrichtung 20 und eine Bremseinrichtung 22 zum Abbremsen der Fallgeschwindigkeit der Suchzündermunition 10 auf. Alle diese Komponenten sind bspw. von der SMArt 155 bekannt, so dass es sich erübrigt, diese detailliert zu beschreiben; sie sind nicht Gegenstand der vorliegenden Erfindung. Gegenstand der vorliegenden Erfindung ist insbesondere, dass die Suchzündermunition 10 vollkalibrig ohne eigene Gehäusehülse ausgebildet ist, um die projektilbildende Einlage mit einem entsprechend großen Durchmesser dimensionieren zu können.The
Das Heckteil 24 weist ein Ausstoßrohr 42 auf. Dieses ist mit der Suchzündermunition 10 entlang eines umlaufenden Sollbruchabschnittes 26 mit einem Gehäuse 44 verbunden. Der Sollbruchabschnitt 26 ist mittels eines im Heckteil 24 vorgesehenen Bodenzünders 28 mit Ausstoßladung 36 auftrennbar, um die Suchzündermunition 10 vom Heckteil 24 abzutrennen.The
Die Sollbruchstelle 26 ist gasdicht ausgebildet und abschussfest. Sie ist entweder als Gewindeverbindung oder als Schweißverbindung gestaltet. Sie kann auch aus einem Fügeelement aus Kunststoff bestehen.The predetermined
Der Bodenzünder 28 ist mit einem Anschlusskabel 30 verbunden, um den Bodenzünder 28 passend programmieren zu können. Eine andere Möglichkeit besteht darin, den Bodenzünder 28 induktiv zu programmieren.The
Der Bodenzünder 28 zündet sowohl die Ausstoßladung 36 und startet über eine nicht dargestelltes Kabel die Zeitfunktion der Sensor- und Zündeinrichtung 16, 18.The
Der Boden 40 ist mit einem Deckel 50 der Bremseinrichtung 22 fest verbunden.The
Pyrotechnisch zündbare Trennschrauben 44, 46 aktivieren die Bremseinrichtung 22 und - zeitlich später - die Entdralleinrichtung 20.Pyrotechnically ignitable separating
Das Heckteil 24 weist ein aufstellbares Leitwerk 32 auf, das in der Figur 1 im aufgestellten Aktivzustand gezeichnet ist. Im inaktiven Zustand liegen die Flügel des Leitwerks 32 unterkalibrig am Heckteil 24 an.The
Vorderseitig weist die Suchzündermunition 10 eine ballistische Haube 34 aus einem geeigneten Kunststoffmaterial auf, das für Radarstrahlen der Sensoreinrichtung 18 durchlässig ist.On the front side, the
Nach Abschluss der Suchzündermunition 1 aus einem Waffenrohr wird das Leitwerk 32 durch Fliehkräfte oder durch Federkraft aufgestellt.After completion of the search fuzes ammunition 1 from a gun barrel, the
Auf der Flugbahn, dicht vor dem Ziel, erfolgt der Ausstoß des Geschosses 44, siehe Figur 2. Hierzu zündet der Bodenzünder 28 die Ausstoßladung 36. Deren Gasdruck führt zur Auftrennung der Sollbruchstelle 26 und zum Ausstoß des Geschosses 44 aus dem Ausstoßrohr 42.On the trajectory, close to the target, the
Nach Zündung der Trennschraube 44 wird die Bremseinrichtung 22 ausgestoßen. Dabei wird der Deckel 50 mit dem Boden 40 in Achsrichtung entfernt.After ignition of the separating
Anschließend wird die Entdralleinrichtung 20 durch Zündung der Trennschraube 46 aktiviert.Subsequently, the
Nach Sensierung des Zieles erfolgt im optimierten Abstand die Zündung der Sprengladung 14 mit Umformung der Einlage 12 zu einem zielbekämpfenden Projektil.After sensing the target, the ignition of the
Die Führungslänge 52 des Geschosses 44 in dem Abschussrohr 42 entspricht dem 1,1 fachen des Geschosskalibers 54. Dadurch ist ein momentenfreier Ausstoß des Geschosses 44 bzw. Trennung des Geschosses 44 von dem Heckteil 24 sichergestellt.The
Zur stabilen Fluglage des Geschosses 44 nach der Trennung trägt der Boden 40 bei.For stable attitude of the projectile 44 after the separation of the
- 1010
- SuchzündermunitionSensor fused munition
- 1212
- Projektilbildende Einlage (von 10)Projectile Inlay (out of 10)
- 1414
- Sprengladung (für 12)Explosive charge (for 12)
- 1616
- Zündeinrichtung (für 14)Ignition device (for 14)
- 1818
- Sensoreinrichtung (von 10 für 16)Sensor device (from 10 to 16)
- 2020
- Entdralleinrichtung (von 10)Untwisting device (out of 10)
- 2222
- Bremseinrichtung (von 10)Braking device (from 10)
- 2424
- Heckteil (von 10)Tail section (out of 10)
- 2626
- Sollbruchabschnitt (zwischen 24 und 10)Breaking section (between 24 and 10)
- 2828
- Bodenzünder (in 24 für 26)Soil detonator (in 24 for 26)
- 3030
- Anschlusskabel (für 28)Connection cable (for 28)
- 3232
- Leitwerk (von 24)Tail (of 24)
- 3434
- Ballistische Haube (von 10)Ballistic Hood (from 10)
- 3636
- Ausstoßladungejection charge
- 3838
- Gasdruckgas pressure
- 4040
- Bodenground
- 4141
- Ausnehmungrecess
- 4242
- Abschussrohrlaunching tube
- 4444
- Geschossbullet
- 4646
- Trennschrauberelease screw
- 4848
- Trennschrauberelease screw
- 5050
- Deckelcover
- 5252
- Führungslängeguide length
- 5454
- Geschosskaliberbullet caliber
Claims (7)
dadurch gekennzeichnet,
dass die Suchzündermunition (10) vollkalibrig ohne Gehäusehülse ausgebildet und rückseitig mit einem Heckteil (24) verbunden ist, wobei das Heckteil (24) mit der Suchzündermunition (10) entlang eines umlaufenden Sollbruchabschnittes (26) verbunden und mittels eines im Heckteil (24) vorgesehenen Bodenzünders (28) vom Heckteil (24) abtrennbar ist.Search fuzes ammunition, the front side has a projectile-forming insert (12),
characterized,
that the search detonator ammunition (10) is formed fully caliber without housing sleeve and rear side connected to a rear part (24), wherein the rear part (24) with the search detonator ammunition (10) along a circumferential predetermined breaking portion (26) and connected by means provided in the rear part (24) Bottom igniter (28) from the rear part (24) is separable.
dadurch gekennzeichnet,
dass vorderseitig eine für Radarstrahlen durchlässige ballistische Haube (34) vorgesehen ist.Finder ammunition according to claim 1,
characterized,
in that a ballistic hood (34) permeable to radar rays is provided on the front side.
dadurch gekennzeichnet,
dass das Heckteil (24) ein aufstellbares Leitwerk (32) aufweist.Finder ammunition according to claim 1,
characterized,
that the rear part (24) has a deployable tail unit (32).
dadurch gekennzeichnet,
dass ein von der Suchzündermunition (10) abtrennbares Geschoss (44) die Einlage (12) aufweist.Finder ammunition according to claim 1,
characterized,
in that a projectile (44) which can be separated from the search detonator ammunition (10) has the insert (12).
dadurch gekennzeichnet,
dass das Heckteil (24) ein Ausstoßrohr (42) aufweist, in dem Ausstoßrohr (42) zum Transport und zum Ausstoß ein Geschoss (44) gelagert ist, und die Führungslänge (52) etwa dem Geschosskaliber (54) entspricht.Finder ammunition according to claim 1,
characterized,
in that the tail part (24) has an ejection tube (42) in which the ejection tube (42) has a projectile (44) for transport and ejection, and the guide length (52) corresponds approximately to the projectile caliber (54).
dadurch gekennzeichnet,
dass eine Ausstoßladung (36) in einer Ausnehmung (41) eines Bodens (40) des Geschosses (44) angeordnet und durch den Bodenzünder (28) zündbar ist, und der Bodenzünder (28) integraler Bestandteil des Heckteiles (24) ist.Finder ammunition according to claim 5,
characterized,
that an ejection charge (36) in a recess (41) of a bottom located (40) of the projectile (44) and through the bottom fuze (28) is ignited, and the bottom fuze (28) is an integral part of the rear part (24).
dadurch gekennzeichnet,
dass der Boden (40) mit einem Deckel (50) einer Bremseinrichtung (22) verbunden ist und die Bremseinrichtung (22) einen heckseitigen Abschnitt des Geschosses (44) bildet.Finder ammunition according to claim 6,
characterized,
that the bottom (40) with a lid (50) a braking device (22) and the braking device (22) forms a rear side portion of the projectile (44).
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102005043078A DE102005043078B4 (en) | 2005-09-10 | 2005-09-10 | Sensor fused munition |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP1762815A1 true EP1762815A1 (en) | 2007-03-14 |
| EP1762815B1 EP1762815B1 (en) | 2009-08-26 |
Family
ID=37462434
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP06018435A Expired - Fee Related EP1762815B1 (en) | 2005-09-10 | 2006-09-04 | Munition with seeking fuze |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US7415930B2 (en) |
| EP (1) | EP1762815B1 (en) |
| KR (1) | KR101320978B1 (en) |
| DE (2) | DE102005043078B4 (en) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8250984B2 (en) * | 2008-08-29 | 2012-08-28 | Lockheed Martin Corporation | Mine-defeating submunition |
| US8222583B2 (en) * | 2009-03-23 | 2012-07-17 | Lockheed Martin Corporation | Drag-stabilized water-entry projectile and cartridge assembly |
| US9383180B2 (en) * | 2012-03-12 | 2016-07-05 | Omnitek Partners Llc | Gravity dropped small weapon electronic safe arm fuze and energy harvesting device for power generation onboard gravity dropped weapons |
| US10539403B2 (en) * | 2017-06-09 | 2020-01-21 | Kaman Precision Products, Inc. | Laser guided bomb with proximity sensor |
| CN108931164A (en) * | 2017-07-13 | 2018-12-04 | 王海龙 | A kind of turn emitter |
| RU2669690C1 (en) * | 2017-08-29 | 2018-10-12 | Акционерное общество "Научно-производственное предприятие "Дельта" | Method of correction of shooting from artillery-type weapon |
| KR101960964B1 (en) * | 2018-09-17 | 2019-03-21 | 국방과학연구소 | Extended tail wing |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CH81919A (en) * | 1918-08-22 | 1918-10-01 | Hans Eberhardt | Bullet |
| FR2545923A1 (en) * | 1983-05-13 | 1984-11-16 | Bofors Ab | PROJECTILE ENSURING THE DRILLING OF SHIELDS |
| DE3418444A1 (en) * | 1983-07-08 | 1985-01-17 | Rheinmetall GmbH, 4000 Düsseldorf | ARMORED BULLET |
| FR2558585A1 (en) | 1984-01-19 | 1985-07-26 | Stauff Emile | Droppable submunitions for a projectile, especially of the anti-tank type |
| DE3414414A1 (en) | 1984-04-17 | 1985-10-17 | Dynamit Nobel Ag, 5210 Troisdorf | Missile with a remote-action warhead |
| DE3516673C2 (en) | 1985-05-09 | 1993-05-27 | Diehl Gmbh & Co, 8500 Nuernberg, De | |
| EP0609565A1 (en) | 1993-02-03 | 1994-08-10 | Buck Werke GmbH & Co | Two stage rocket whereby the second stage is decelerated by a parachute prior to ignition |
| DE4426014A1 (en) | 1994-07-22 | 1996-01-25 | Diehl Gmbh & Co | Target protection system e.g. for armoured vehicle or bunker, |
| DE4104800C2 (en) | 1991-02-16 | 1998-07-02 | Diehl Stiftung & Co | Real-time terrain reconnaissance facility |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US556632A (en) * | 1896-03-17 | Multiple projectile | ||
| NL136006C (en) | 1967-06-13 | |||
| BE740812A (en) * | 1969-10-27 | 1970-07-27 | ||
| DE2242930C2 (en) * | 1972-08-31 | 1987-01-02 | Rheinmetall GmbH, 4000 Düsseldorf | Hollow charge daughter floor |
| FR2401400A1 (en) * | 1977-08-23 | 1979-03-23 | Serat | GROUND-TO-GROUND ANTICHAR WEAPON |
| DE2831378A1 (en) * | 1978-07-17 | 1980-01-31 | Rheinmetall Gmbh | APPLICATION OF A HOLLOW CHARGE INSERT AS A REFLECTOR FOR AN ANTENNA |
| US4597333A (en) * | 1983-07-08 | 1986-07-01 | Rheinmetall G.M.B.H. | Two-part armor-piercing projectile |
| US5452864A (en) | 1994-03-31 | 1995-09-26 | Alliant Techsystems Inc. | Electro-mechanical roll control apparatus and method |
| DE19613492C2 (en) * | 1996-04-04 | 2001-10-04 | Diehl Stiftung & Co | Reconnaissance facility |
| FR2771166B1 (en) * | 1997-11-20 | 1999-12-17 | Giat Ind Sa | PROJECTILE WITH A RADIAL ACTION DIRECTION |
-
2005
- 2005-09-10 DE DE102005043078A patent/DE102005043078B4/en not_active Expired - Fee Related
-
2006
- 2006-09-04 DE DE502006004640T patent/DE502006004640D1/en active Active
- 2006-09-04 EP EP06018435A patent/EP1762815B1/en not_active Expired - Fee Related
- 2006-09-07 KR KR1020060086199A patent/KR101320978B1/en not_active IP Right Cessation
- 2006-09-07 US US11/516,863 patent/US7415930B2/en not_active Expired - Fee Related
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CH81919A (en) * | 1918-08-22 | 1918-10-01 | Hans Eberhardt | Bullet |
| FR2545923A1 (en) * | 1983-05-13 | 1984-11-16 | Bofors Ab | PROJECTILE ENSURING THE DRILLING OF SHIELDS |
| DE3418444A1 (en) * | 1983-07-08 | 1985-01-17 | Rheinmetall GmbH, 4000 Düsseldorf | ARMORED BULLET |
| FR2558585A1 (en) | 1984-01-19 | 1985-07-26 | Stauff Emile | Droppable submunitions for a projectile, especially of the anti-tank type |
| DE3414414A1 (en) | 1984-04-17 | 1985-10-17 | Dynamit Nobel Ag, 5210 Troisdorf | Missile with a remote-action warhead |
| DE3516673C2 (en) | 1985-05-09 | 1993-05-27 | Diehl Gmbh & Co, 8500 Nuernberg, De | |
| DE4104800C2 (en) | 1991-02-16 | 1998-07-02 | Diehl Stiftung & Co | Real-time terrain reconnaissance facility |
| EP0609565A1 (en) | 1993-02-03 | 1994-08-10 | Buck Werke GmbH & Co | Two stage rocket whereby the second stage is decelerated by a parachute prior to ignition |
| DE4426014A1 (en) | 1994-07-22 | 1996-01-25 | Diehl Gmbh & Co | Target protection system e.g. for armoured vehicle or bunker, |
Also Published As
| Publication number | Publication date |
|---|---|
| KR20070029564A (en) | 2007-03-14 |
| DE102005043078B4 (en) | 2007-06-14 |
| EP1762815B1 (en) | 2009-08-26 |
| DE502006004640D1 (en) | 2009-10-08 |
| DE102005043078A1 (en) | 2007-03-15 |
| US7415930B2 (en) | 2008-08-26 |
| KR101320978B1 (en) | 2013-10-22 |
| US20070107619A1 (en) | 2007-05-17 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| DE19617221C2 (en) | Steerable projectile that can be used as a mortar | |
| DE19535218C1 (en) | Ballistic projectile | |
| EP1762815B1 (en) | Munition with seeking fuze | |
| DE864527C (en) | Shaped charge projectile | |
| EP0583642A1 (en) | Warhead with tandem charge | |
| DE3626434C2 (en) | ||
| DE3416787A1 (en) | ARMORING BULLET | |
| DE19651170A1 (en) | Detonatorless, ballistic explosive device | |
| DE19917144B4 (en) | Combination action system | |
| EP0918209A1 (en) | Projectile with programmable delay fuze | |
| EP3014213B1 (en) | Detonator for a mortar grenade and a mortar grenade that can be fired from a spigot mortar having such a detonator | |
| EP0249678B2 (en) | Ammunition, especially for fighting targets provided with a reactive armour | |
| EP1001244B1 (en) | Artillery projectile | |
| DE2211524A1 (en) | Small antitank mines with sensor systems - are projected from warhead to cover wide area to act on tank hulls | |
| DE3229220C1 (en) | Sub-caliber sabot bullet | |
| DE69907791T2 (en) | Kit for converting an explosive projectile to a projectile breaking a benton structure, as well as a projectile converted in this way | |
| EP0281088B1 (en) | Submissile with an ignition device | |
| EP0698774B1 (en) | Projectile stabilized by rotation and comprising a payload | |
| DE102020001784A1 (en) | Projectile, device arrangement and method | |
| DE3430498C1 (en) | Underwater mine clearing system | |
| DE19758457B3 (en) | warhead | |
| EP0801287B1 (en) | Fragmentation projectile with base fuze and cartridge case | |
| EP1087202B1 (en) | Armour perforating ammunition | |
| DE19629394C1 (en) | Anti-helicopter munition detonation | |
| DE19758459A1 (en) | Warhead has perforation units, marking units and formed load that is made of explosive charge, casing and marking load, where marking load is arranged in floor |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
| 17P | Request for examination filed |
Effective date: 20061222 |
|
| AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE SI SK TR |
|
| AX | Request for extension of the european patent |
Extension state: AL BA HR MK YU |
|
| 17Q | First examination report despatched |
Effective date: 20070420 |
|
| AKX | Designation fees paid |
Designated state(s): DE FR GB SE |
|
| GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
| GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
| GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
| AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): DE FR GB SE |
|
| REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D Free format text: NOT ENGLISH |
|
| REF | Corresponds to: |
Ref document number: 502006004640 Country of ref document: DE Date of ref document: 20091008 Kind code of ref document: P |
|
| REG | Reference to a national code |
Ref country code: SE Ref legal event code: TRGR |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20091118 Year of fee payment: 4 |
|
| PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
| 26N | No opposition filed |
Effective date: 20100527 |
|
| REG | Reference to a national code |
Ref country code: SE Ref legal event code: EUG |
|
| GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20100904 |
|
| REG | Reference to a national code |
Ref country code: FR Ref legal event code: ST Effective date: 20110531 |
|
| REG | Reference to a national code |
Ref country code: DE Ref legal event code: R119 Ref document number: 502006004640 Country of ref document: DE Effective date: 20110401 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20110401 Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20100930 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20100904 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20091001 Year of fee payment: 4 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20100905 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: SE Payment date: 20090930 Year of fee payment: 4 |