EP2031342A1 - Target marking ammunition - Google Patents

Target marking ammunition Download PDF

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Publication number
EP2031342A1
EP2031342A1 EP08011649A EP08011649A EP2031342A1 EP 2031342 A1 EP2031342 A1 EP 2031342A1 EP 08011649 A EP08011649 A EP 08011649A EP 08011649 A EP08011649 A EP 08011649A EP 2031342 A1 EP2031342 A1 EP 2031342A1
Authority
EP
European Patent Office
Prior art keywords
projectile
ogive
gas cartridge
marking
container
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
Application number
EP08011649A
Other languages
German (de)
French (fr)
Other versions
EP2031342B1 (en
Inventor
Andreas Blache
Bernd Michael Bippes
Ferdinand Panknin
Michael Köpf
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rheinmetall Waffe Munition GmbH
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 SI200831805A priority Critical patent/SI2031342T1/en
Publication of EP2031342A1 publication Critical patent/EP2031342A1/en
Application granted granted Critical
Publication of EP2031342B1 publication Critical patent/EP2031342B1/en
Priority to HRP20170842TT priority patent/HRP20170842T1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F42B12/40—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 of target-marking, i.e. impact-indicating type

Definitions

  • the invention relates to a target ammunition, in particular for mortars and artillery.
  • Inert exercises without terminal effects are used to carry out exercises in such areas. This is particularly problematic in target practice with observers in the target area, since the point of impact / meeting point of the projectile can not or only with difficulty be located. A feedback from the observer to the shooting team to the direction of the weapon system is thus difficult.
  • the practice floor has a hollow ogive in the head area, in which a first chemically inactive and a second chemically active marker are taken.
  • the first marker produces a color effect
  • the second marker a light effect.
  • the ogive itself must burst.
  • the invention has the object to provide an ammunition that marks the impact point in the impact point by a temporary visual marker on a simple way.
  • the invention is based on the idea, to mark the impact point of a projectile on a target in the Ogiven Scheme of the projectile a container (3) is involved, which includes a means for marking the target.
  • the container is broken upon impact of the projectile on the target, so that the means of marking over in the ogive or in the rear part introduced holes can escape.
  • an overpressure is generated in the projectile, which is realized by a gas cartridge with a triggering mechanism or a reciprocating piston or the like.
  • a piston and / or a gas cartridge is incorporated, through which an internal pressure is built up during the impact of the projectile and a preferably luminescent liquid is discharged via bores.
  • This liquid is characterized in that it can be used for day and night targeting.
  • the reciprocating piston is moved either via a gas cartridge or mechanically by a preferably defined deformation of the projectile body axially to build up the internal pressure.
  • the gas cartridge is pierced by a trigger mechanism, which in turn is triggered when striking the bullet directly or via a detonator.
  • the destroyed fluid container releases the fluid through holes in the ogive or tail section.
  • the application of the preferably luminescent mass is carried out without pyrotechnic means or decomposition of the projectile body with splinter formation.
  • the defined deformation for the reciprocating piston can be created by the front side embedded in the projectile detonator.
  • the advantages are u. a. in that there is no risk of fire and a good visibility of the coronary impact point is created during the day and at night, without a color marking and a lighting effect must be generated. Furthermore, splintering of the ogive is not necessary.
  • the projectiles have a simple and safe handling and have a ballistic equality to existing floors.
  • Fig. 1 is a projectile 10, here an exercise mortar, slightly stylistically represented with a gas cartridge 7 with a trigger mechanism 8 for the gas cartridge 7 in section. 1 designates an igniter, with 2 at least one, preferably a plurality of bores, with 3 a container, here a fluid container containing a fluid. The latter is due to the overall system enclosing protective ogive 4, which further includes an inert mass 5. This serves to ensure ballistic equality.
  • the stern 6 are, as in a mortar shell known, various holes through which the propellant charge, not shown, is ignited.
  • the holes 2 are preferably symmetrically spaced apart on the circumference of the ogive 4 or distributed distributed in the rear area.

Abstract

The munition (11) includes a marking agent. This leaves through bores (2) made in the front of the ogive (4), or in the rear region. To cause ejection, increased pressure is caused inside the munition. The marking agent is a powder or liquid. It is a luminescent liquid. The container (3) is ruptured by a gas cartridge (7) and release mechanism (8), which lie ahead of it. The gas cartridge produces the required pressure increase. A detonator is incorporated at the tip of the ogive.

Description

Die Erfindung betrifft eine Zielmarkierungsmunition insbesondere für Mörser und Artillerie.The invention relates to a target ammunition, in particular for mortars and artillery.

Insbesondere bei Übungen in brandgefährdeten Gebieten besteht durch bekannte Übungsmunitionen mit Zielmarkierung auf pyrotechnischer Basis (heiße brennende Partikel) oder bei scharfer Munition, wie beispielsweise HE-, Nebel- und Leuchtmunition, die Gefahr der Entzündung und damit verbunden von Bränden, insbesondere Bodenbränden. Hier spielt auch die so genannte Waldbrandgefahr im Gebiet eine große Rolle.In particular, in exercises in fire-prone areas by known practice munitions with target marking on pyrotechnic base (hot burning particles) or live ammunition, such as HE, fog and light ammunition, the risk of inflammation and associated with fires, especially ground fires. Here also the so-called forest fire danger in the area plays a large role.

Zur Durchführung von Übungen in derartigen Gebieten werden Inertgeschosse ohne terminale Wirkung eingesetzt. Dies ist insbesondere bei Zielübungen mit Beobachtern im Zielgebiet problematisch, da der Aufschlagpunkt / Treffpunkt des Geschosses nicht oder nur schwer lokalisiert werden kann. Eine Rückmeldung des Beobachters an die Schießmannschaft zur Richtung der Waffenanlage ist somit schwer gegeben.Inert exercises without terminal effects are used to carry out exercises in such areas. This is particularly problematic in target practice with observers in the target area, since the point of impact / meeting point of the projectile can not or only with difficulty be located. A feedback from the observer to the shooting team to the direction of the weapon system is thus difficult.

Aus der DE 10 2005 053 A1 ist ein Geschoss mit Markierung des Auftreffpunktes bekannt. Das Übungsgeschoss weist im Kopfbereich eine hohle Ogive auf, in der ein erster chemisch inaktiver und ein zweiter chemisch aktiver Markierungsstoff aufgenommen sind. Der erste Markierungsstoff erzeugt einen Farbeffekt, der zweite Markierungsstoff einen Lichteffekt. Die Ogive selbst muss dazu bersten.From the DE 10 2005 053 A1 is a bullet with mark the impact point known. The practice floor has a hollow ogive in the head area, in which a first chemically inactive and a second chemically active marker are taken. The first marker produces a color effect, the second marker a light effect. The ogive itself must burst.

Hier stellt sich die Erfindung die Aufgabe, eine Munition zu schaffen, die im Aufschlagpunkt durch eine temporäre visuelle Markierung auf einfachem Weg den Aufschlagpunkt markiert.Here, the invention has the object to provide an ammunition that marks the impact point in the impact point by a temporary visual marker on a simple way.

Gelöst wird die Aufgabe durch die Merkmale des Patentanspruchs 1. Vorteilhafte Ausführungen sind in den Unteransprüchen enthalten.The object is achieved by the features of claim 1. Advantageous embodiments are contained in the subclaims.

Der Erfindung liegt die Idee zugrunde, zur Markierung des Auftreffpunktes eines Geschosses auf ein Ziel im Ogivenbereich des Geschosses einen Behälter (3) einzubinden ist, welcher ein Mittel zur Markierung des Zieles beinhaltet. Der Behälter wird beim Auftreffen des Geschosses auf das Ziel zerbrochen, so dass das Mittel zur Markierung über in der Ogive oder im Heckteil eingebrachte Bohrungen austreten kann. Damit es in dieser Form austreten kann, wird im Geschoss ein Überdruck erzeugt, was durch eine Gaskartusche mit Auslösemechanismus oder einen Hubkolben oder dergleichen realisiert wird.The invention is based on the idea, to mark the impact point of a projectile on a target in the Ogivenbereich of the projectile a container (3) is involved, which includes a means for marking the target. The container is broken upon impact of the projectile on the target, so that the means of marking over in the ogive or in the rear part introduced holes can escape. In order that it can escape in this form, an overpressure is generated in the projectile, which is realized by a gas cartridge with a triggering mechanism or a reciprocating piston or the like.

Im Geschosskörper wird also einen Kolben und / oder eine Gaskartusche eingebunden, durch welche beim Aufschlag des Geschosses ein Innendruck aufgebaut und eine vorzugsweise lumineszierende Flüssigkeit über Bohrungen ausgebracht wird. Diese Flüssigkeit zeichnet sich dadurch aus, dass diese für Tag- und Nachtzielmarkierung verwendet werden kann.Thus, in the projectile body, a piston and / or a gas cartridge is incorporated, through which an internal pressure is built up during the impact of the projectile and a preferably luminescent liquid is discharged via bores. This liquid is characterized in that it can be used for day and night targeting.

Der Hubkolben wird entweder über eine Gaskartusche oder mechanisch durch eine vorzugsweise definierte Deformierung des Geschosskörpers axial zum Aufbau des Innendrucks verschoben. Die Gaskartusche wird dabei durch einen Auslösemechanismus angestochen, der seinerseits beim Auftreffen des Geschosses direkt oder über einen Zünder angestoßen wird. Der zerstörte Fluidbehälter gibt das Fluid über Bohrungen in der Ogive oder im Heckteil zur Markierung frei. Die Ausbringung der vorzugsweise lumineszierenden Masse erfolgt ohne pyrotechnische Mittel oder Zerlegung des Geschosskörpers mit Splitterbildung. Die definierte Deformierung für den Hubkolben kann durch den stirnseitig im Geschoss eingebetteten Zünder geschaffen werden.The reciprocating piston is moved either via a gas cartridge or mechanically by a preferably defined deformation of the projectile body axially to build up the internal pressure. The gas cartridge is pierced by a trigger mechanism, which in turn is triggered when striking the bullet directly or via a detonator. The destroyed fluid container releases the fluid through holes in the ogive or tail section. The application of the preferably luminescent mass is carried out without pyrotechnic means or decomposition of the projectile body with splinter formation. The defined deformation for the reciprocating piston can be created by the front side embedded in the projectile detonator.

Die Vorteile liegen u. a. darin, dass keine Brandgefahr mehr besteht und eine gute Sichtbarkeit des kranzartigen Aufschlagpunktes am Tag und bei Nacht geschaffen wird, ohne das eine Farbmarkierung und ein Lichteffekt erzeugt werden müssen. Des Weiteren ist eine Splitterbildung der Ogive nicht notwendig. Die Geschosse besitzen eine einfache und sichere Handhabung und weisen eine ballistische Gleichheit zu bestehenden Geschossen auf.The advantages are u. a. in that there is no risk of fire and a good visibility of the coronary impact point is created during the day and at night, without a color marking and a lighting effect must be generated. Furthermore, splintering of the ogive is not necessary. The projectiles have a simple and safe handling and have a ballistic equality to existing floors.

Anhand eines Ausführungsbeispiels mit Zeichnung soll die Erfindung näher erläutert werden. Es zeigt:

Fig. 1
ein Geschoss mit Gaskartusche im Schnitt,
Fig. 2
ein Geschoss mit Hubkolben im Schnitt.
Reference to an embodiment with drawing, the invention will be explained in more detail. It shows:
Fig. 1
a projectile with gas cartridge in the section,
Fig. 2
a projectile with reciprocating pistons on average.

In Fig. 1 ist ein Geschoss 10, hier ein Übungsmörser, mit einer Gaskartusche 7 mit einem Auslösemechanismus 8 für die Gaskartusche 7 im Schnitt leicht stilistisch dargestellt. Mit 1 ist ein Zünder gekennzeichnet, mit 2 wenigstens eine, bevorzugt mehrere Bohrungen, mit 3 ein Behälter, hier ein ein Fluid enthaltener Fluidbehälter. Letzteres wird durch eine das Gesamtsystem schützende Ogive 4 umschlossen, die des Weiteren eine inerte Masse 5 beinhaltet. Diese dient zur Sicherstellung der ballistischen Gleichheit. Im Heck 6 befinden sich, wie bei einem Mörsergeschoss bekannt, diverse Bohrungen, durch welche die nicht weiter dargestellte Treibladung gezündet wird.In Fig. 1 is a projectile 10, here an exercise mortar, slightly stylistically represented with a gas cartridge 7 with a trigger mechanism 8 for the gas cartridge 7 in section. 1 designates an igniter, with 2 at least one, preferably a plurality of bores, with 3 a container, here a fluid container containing a fluid. The latter is due to the overall system enclosing protective ogive 4, which further includes an inert mass 5. This serves to ensure ballistic equality. In the stern 6 are, as in a mortar shell known, various holes through which the propellant charge, not shown, is ignited.

Die Bohrungen 2 sind vorzugsweise symmetrisch voneinander beabstandet am Umfang der Ogive 4 oder im Heckbereich verteilt eingebunden.The holes 2 are preferably symmetrically spaced apart on the circumference of the ogive 4 or distributed distributed in the rear area.

Fig. 2 zeigt ein weiteres Geschoss 11, ebenfalls ein Übungsmörser, welcher anstelle der Gaskartusche 7 mit Auslösemechanismus 8 einen Hubkolben 9 aufweist.
Die Funktion ist wie folgt:

  • Beim Auftreffen des Geschosses 10 bzw. 11 wird durch den Aufschlagpuls die Gaskartusche 7 durch den Auslösemechanismus 8 angestochen bzw. der Hubkolben 9 in Bewegung gesetzt. Durch den Überdruck im Inneren des Geschosses 10, 11 wird der Fluidbehälter 3 zerstört. Das darin befindliche vorzugsweise lumineszierende Fluid vermischt sich beim Austritt durch die Bohrungen 2 aus der Ogive 4. Durch diesen Vorgang wird die Zielmarkierung im Zielgebiet praktisch zeitgleich mit dem Aufschlag des Geschosses 10, 11 ausgelöst und für einen nicht näher dargestellten Beobachter visuell angezeigt.
Fig. 2 shows a further projectile 11, also an exercise mortar, which has a reciprocating piston 9 instead of the gas cartridge 7 with triggering mechanism 8.
The function is as follows:
  • Upon impact of the projectile 10 or 11, the gas cartridge 7 is pierced by the triggering mechanism 8 or the reciprocating piston 9 is set in motion by the impact pulse. Due to the pressure in the interior of the projectile 10, 11 of the fluid container 3 is destroyed. The therein preferably luminescent fluid mixes when exiting through the holes 2 from the Ogive 4. Through this process, the target mark in the target area practically simultaneously triggered with the impact of the projectile 10, 11 and displayed visually for an observer, not shown.

Zur Unterstützung der Funktion der Gaskartusche 7 bzw. des Hubkolbens 9 ist stirnseitig in der Ogive 4 der Zünder eingebunden.To support the function of the gas cartridge 7 and the reciprocating piston 9 is the front side in the Ogive 4 of the detonator involved.

Claims (6)

Geschoss (10, 11), insbesondere Übungsgeschoss, mit einem Markierungsstoff zum Markieren des Auftreffpunktes des Geschosses (10, 11) auf ein Ziel, wobei im Ogivenbreich des Geschosses (10, 11) wenigstens ein Behälter (3) eingebunden ist, welcher wenigstens ein Mittel zur Markierung des Zieles beinhaltet, und der Behälter (3) beim Auftreffen des Geschosses (10, 11) auf das Ziel zerstört wird, dadurch gekennzeichnet, dass das Mittel zur Markierung über in der Ogive (4) oder im Heckbereich eingebrachte Bohrungen (2) austritt, wozu im Geschoss (10, 11) ein Überdruck erzeugt wird.Projectile (10, 11), in particular training projectile, with a marking substance for marking the impact point of the projectile (10, 11) on a target, wherein in Ogivenbreich of the projectile (10, 11) at least one container (3) is integrated, which at least one Includes means for marking the target, and the container (3) upon impact of the projectile (10, 11) is destroyed on the target, characterized in that the means for marking on introduced in the ogive (4) or at the rear bores (2 ), for which an overpressure is generated in the projectile (10, 11). Geschoss nach Anspruch 1, dadurch gekennzeichnet, dass das Mittel zur Markierung ein Fluid und/oder ein Pulver ist.Projectile according to claim 1, characterized in that the means for marking is a fluid and / or a powder. Geschoss nach Anspruch 2, dadurch gekennzeichnet, dass das Fluid ein luminezierendes Fluid ist.Projectile according to Claim 2, characterized in that the fluid is a luminescent fluid. Geschoss nach einem der Ansprüche 1 bis 4, dadurch gekennzeichnet, dass der Behälter (3) durch eine davor befindliche Gaskartusche (7) mit Auslösemechanismus (8) zerstört wird, wobei die Gaskartusche (7) den Überdruck erzeugt.Projectile according to one of Claims 1 to 4, characterized in that the container (3) is destroyed by a gas cartridge (7) with a triggering mechanism (8) in front of it, the gas cartridge (7) generating the overpressure. Geschoss nach einem der Ansprüche 1 bis 4, dadurch gekennzeichnet, dass der Behälter (3) durch einen davor befindlichen Hubkolben (9) zerstört wird, wobei der Hubkolben (9) den Überdruck erzeugt.Projectile according to one of claims 1 to 4, characterized in that the container (3) is destroyed by a piston located in front of it (9), wherein the lifting piston (9) generates the overpressure. Geschoss nach einem der Ansprüche 1 bis 5, dadurch gekennzeichnet, dass ein Zünder (1) an der Spitze der Ogive (4) eingebunden ist.Projectile according to one of claims 1 to 5, characterized in that an igniter (1) is incorporated at the top of the ogive (4).
EP08011649.4A 2007-07-20 2008-06-27 Target marking ammunition Active EP2031342B1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
SI200831805A SI2031342T1 (en) 2007-07-20 2008-06-27 Target marking ammunition
HRP20170842TT HRP20170842T1 (en) 2007-07-20 2017-06-01 Target marking ammunition

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE200710034546 DE102007034546A1 (en) 2007-07-20 2007-07-20 Target marking ammunition

Publications (2)

Publication Number Publication Date
EP2031342A1 true EP2031342A1 (en) 2009-03-04
EP2031342B1 EP2031342B1 (en) 2017-03-08

Family

ID=40149120

Family Applications (1)

Application Number Title Priority Date Filing Date
EP08011649.4A Active EP2031342B1 (en) 2007-07-20 2008-06-27 Target marking ammunition

Country Status (7)

Country Link
EP (1) EP2031342B1 (en)
CA (1) CA2637872C (en)
DE (1) DE102007034546A1 (en)
DK (1) DK2031342T3 (en)
HR (1) HRP20170842T1 (en)
PL (1) PL2031342T3 (en)
SI (1) SI2031342T1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2616758B1 (en) 2010-09-16 2018-05-30 Advanced Material Engineering Pte Ltd Projectile with strike point marking

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102011107960B3 (en) * 2011-07-20 2012-03-22 Rheinmetall Waffe Munition Gmbh Ammunition, particularly blank ammunition, has projectile body which comprises projectile casing, where charge is held to be exploded in air
DE102015007617A1 (en) * 2015-06-16 2016-12-22 Diehl Bgt Defence Gmbh & Co. Kg Ammunition for marking a target person

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DE3327945A1 (en) 1983-08-03 1985-02-21 Rheinmetall GmbH, 4000 Düsseldorf BULLET WITH A PAYLOAD PART AND A DRIVE PART
EP0101795B1 (en) 1982-07-02 1986-01-02 Rheinmetall GmbH Fragmentation projectile with splinter effect
DE3804351A1 (en) 1988-02-12 1989-08-24 Rheinmetall Gmbh BLasted up
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JPH0791898A (en) 1993-09-21 1995-04-07 Nissan Motor Co Ltd Missile
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JP2001059451A (en) 1999-08-18 2001-03-06 Ishikawajima Harima Heavy Ind Co Ltd Method for transferring gelled propellant
EP1310659A1 (en) 2001-11-08 2003-05-14 The Boeing Company Apparatus and method for initiating a combustion reaction with slurry fuel
EP1321505A2 (en) 2001-12-22 2003-06-25 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Gelled propellant, process for the preparation of a gelled propellant and its use
CH693543A5 (en) * 1998-10-02 2003-09-30 Nico Pyrotechnik Grenade shell has piston sealing channels between high pressure chamber containing propellant charge surrounded by low pressure chamber, and which is moved upwards by propellant gases when shell is fired
DE102004020838B3 (en) * 2004-04-08 2005-06-23 Nico-Pyrotechnik Hanns-Jürgen Diederichs GmbH & Co. KG Medium-caliber cartridge munition used for practice, includes passages through casing from chamber containing propellant charge, which are filled with melting alloy
WO2005098345A1 (en) * 2004-04-08 2005-10-20 Nico Pyrotechnik Hanns-Jürgen Diederichs Gmbh & Co. Kg Projectile featuring marking of the point of impact
DE102005053491A1 (en) * 2005-11-09 2007-05-10 Rheinmetall Waffe Munition Gmbh Projectile with marking of the impact point

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Publication number Priority date Publication date Assignee Title
US3208385A (en) 1962-12-24 1965-09-28 Diehl Incendiary shell
DE3319541C1 (en) 1982-05-28 1997-10-16 Royal Ordnance Plc Plastic fuel compositions and process for their preparation
EP0101795B1 (en) 1982-07-02 1986-01-02 Rheinmetall GmbH Fragmentation projectile with splinter effect
DE3327945A1 (en) 1983-08-03 1985-02-21 Rheinmetall GmbH, 4000 Düsseldorf BULLET WITH A PAYLOAD PART AND A DRIVE PART
DE3804351A1 (en) 1988-02-12 1989-08-24 Rheinmetall Gmbh BLasted up
US4932672A (en) * 1989-01-17 1990-06-12 Tippmann Dennis J Nonlethal hand grenade
DE3924858A1 (en) 1989-07-27 1991-02-07 Messerschmitt Boelkow Blohm Ramjet engine with gaseous fuel generators - has bulkhead to protect auxiliary generates from heat of main generators
JPH0791898A (en) 1993-09-21 1995-04-07 Nissan Motor Co Ltd Missile
CH693543A5 (en) * 1998-10-02 2003-09-30 Nico Pyrotechnik Grenade shell has piston sealing channels between high pressure chamber containing propellant charge surrounded by low pressure chamber, and which is moved upwards by propellant gases when shell is fired
DE19917649A1 (en) * 1999-04-19 2000-11-02 Nico Pyrotechnik Practice floor for an automatic rapid-fire weapon
JP2001059451A (en) 1999-08-18 2001-03-06 Ishikawajima Harima Heavy Ind Co Ltd Method for transferring gelled propellant
EP1310659A1 (en) 2001-11-08 2003-05-14 The Boeing Company Apparatus and method for initiating a combustion reaction with slurry fuel
EP1321505A2 (en) 2001-12-22 2003-06-25 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Gelled propellant, process for the preparation of a gelled propellant and its use
DE102004020838B3 (en) * 2004-04-08 2005-06-23 Nico-Pyrotechnik Hanns-Jürgen Diederichs GmbH & Co. KG Medium-caliber cartridge munition used for practice, includes passages through casing from chamber containing propellant charge, which are filled with melting alloy
WO2005098345A1 (en) * 2004-04-08 2005-10-20 Nico Pyrotechnik Hanns-Jürgen Diederichs Gmbh & Co. Kg Projectile featuring marking of the point of impact
DE102005053491A1 (en) * 2005-11-09 2007-05-10 Rheinmetall Waffe Munition Gmbh Projectile with marking of the impact point

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2616758B1 (en) 2010-09-16 2018-05-30 Advanced Material Engineering Pte Ltd Projectile with strike point marking
EP2616758B2 (en) † 2010-09-16 2021-07-28 Advanced Material Engineering Pte Ltd Projectile with strike point marking

Also Published As

Publication number Publication date
PL2031342T3 (en) 2017-09-29
DE102007034546A1 (en) 2009-01-22
EP2031342B1 (en) 2017-03-08
HRP20170842T1 (en) 2017-08-25
CA2637872A1 (en) 2009-01-20
SI2031342T1 (en) 2017-06-30
CA2637872C (en) 2017-05-02
DK2031342T3 (en) 2017-06-06

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