EP1873475B1 - Blank ammunition - Google Patents

Blank ammunition Download PDF

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Publication number
EP1873475B1
EP1873475B1 EP07012428A EP07012428A EP1873475B1 EP 1873475 B1 EP1873475 B1 EP 1873475B1 EP 07012428 A EP07012428 A EP 07012428A EP 07012428 A EP07012428 A EP 07012428A EP 1873475 B1 EP1873475 B1 EP 1873475B1
Authority
EP
European Patent Office
Prior art keywords
propellant charge
projectile
propellant
replica
maneuver
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.)
Not-in-force
Application number
EP07012428A
Other languages
German (de)
French (fr)
Other versions
EP1873475A3 (en
EP1873475A2 (en
Inventor
Stephan Kerk
Peter Kreutzer
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.)
Diehl BGT Defence GmbH and Co KG
Original Assignee
Diehl BGT Defence GmbH and Co KG
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 Diehl BGT Defence GmbH and Co KG filed Critical Diehl BGT Defence GmbH and Co KG
Publication of EP1873475A2 publication Critical patent/EP1873475A2/en
Publication of EP1873475A3 publication Critical patent/EP1873475A3/en
Application granted granted Critical
Publication of EP1873475B1 publication Critical patent/EP1873475B1/en
Not-in-force 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
    • F42B8/00—Practice or training ammunition
    • F42B8/02—Cartridges
    • F42B8/04—Blank cartridges, i.e. primed cartridges without projectile but containing an explosive or combustible powder charge

Definitions

  • the invention relates to a Manövermunition according to the preamble of claim 1.
  • Such Manövermunition is from the DE 4128050 known.
  • maneuver ammunition is known for example as a maneuver cartridge DM 128.
  • the maneuver ammunition is designed as a telescopically insertable ammunition, i. the protruding projectile from the propellant charge projectile into the propellant charge sleeve hineinbewegbar.
  • the propellant charge is provided in the propellant charge case in bulk. From this loose charge of the propellant charge fluctuations in gas pressure can result. This affects the constancy of performance, reliability and safety against possible personal injury.
  • the invention has for its object to provide a maneuver ammunition of the type mentioned above, which has a higher reliability and safety against personal injury and has a relatively constant performance.
  • the maneuvering ammunition according to the invention has the advantages that it is simple and comparatively inexpensive to produce, and that the propellant charge is fixed in the space between the bottom of the propellant charge shell and a diaphragm provided on the rear side of the middle part, with this determination of the propellant charge powder constant power and a higher Reliability and increased safety against personal injury results.
  • the functional reliability is also ensured by the locking of a front part forming bullet simulation on the fixed part in the propellant charge sleeve.
  • the propellant charge is located defined in the rear region of the propellant charge sleeve between the bottom and the diaphragm of the fixed in the propellant charge sleeve middle part, gas pressure fluctuations are negligible.
  • the propellant charge tube is cut off in a certain area.
  • the Figures 1 and 2 illustrate longitudinally sectioned an embodiment of the maneuver ammunition 10 with a propellant charge shell 12.
  • the propellant charge shell 12 has a shell 14 and a bottom 16, through which the propellant charge shell 12 is closed at the back.
  • a primer 18 is arranged for a propellant charge 20 provided in the propellant charge case 12.
  • the propellant charge 20 is a propellant charge powder.
  • a projectile 22 projectile which is combined with a central portion 24.
  • the middle part 24 is fixed in the propellant charge sleeve 12.
  • This attachment can be, for example, a material-locking attachment, ie a bond.
  • a mechanical connection of the central part 24 with the jacket 14 of the propellant charge sleeve 12 is possible.
  • the middle part 24 is formed on its inner surface 26 on the front side with a first latching groove 28 and on the rear side with a second latching groove 30.
  • the projectile 22 forming a front part is formed on the back with resilient latching fingers 32, which in the in FIG. 1 designated state of the maneuver ammunition before the function in the front-side first locking groove 28 and in the in FIG. 2 drawn operating position after the function of the maneuver ammunition 10 are engaged in the rear side second locking groove 30.
  • the projectile 22 is formed with a central through hole 34 and the outside with a stop collar 36.
  • the fixed in the propellant charge sleeve 12 central part 24 has the rear side in the vicinity of the second locking groove 30, a diaphragm 38.
  • the propellant charge 20 formed by propellants is fixed in the space between the bottom 16 of the propellant charge case 12 and the diaphragm 38 of the middle portion 24.
  • the front-side projectile 22 and the attached in the propellant charge shell 12 middle part 24 are preferably made of suitable plastic material.
  • the projectile replica 22 is defined from the middle part 24, wherein the resilient latching fingers 32 of the projectile replica 22 are engaged in the front-side first latching groove 28 of the central part 24.
  • the front projecting bullet replica 22 When inserting the Manövermunition 10 in a chamber of a maneuver cartridge device, the front projecting bullet replica 22 is inserted into the middle part 24, wherein the resilient latching fingers 32 of the projectile replica 22 engage in the rear second latching groove 30 of the central part 24, so that the projectile replica 22 in the inserted rear Position is locked. If the primer cap 18 is then ignited, the propellant charge 20 defined between the base 16 of the propellant charge casing 12 and the diaphragm 38 of the central part 24 is ignited. As a result, the diaphragm 38 of the central part 24 is destroyed and the gas pressure generated by the ignited propellant charge powder can escape through the central through hole 34 of a front part forming missile replica 22 forward, whereby the weapon is driven.
  • the thus formed maneuver ammunition 10 is inexpensive realizable. Their safe function is ensured by the resilient locking of a front part forming projectile replica 22. Characterized in that the propellant charge 20 at the rear of the propellant charge shell 12 - defined by the membrane 38 front side - defined defined, gas pressure fluctuations are negligible, resulting in a constant performance, higher reliability and a higher safety against personal injury results - as already stated has been.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
  • Containers And Packaging Bodies Having A Special Means To Remove Contents (AREA)

Abstract

The maneuver ammunition (10) for supplying into the patron bearing of a maneuver patron device comprises a propellant case for igniting a propellant by means of a percussion cap intended in a base, and a projectile replica projecting from the propellant case. The projectile replica is combined with a middle part, which is fastened in the propellant case. The projectile replica is projected from the middle part and movably led into the middle part. The projectile replica is lockable in the projecting and in the respective position moved into the middle part. The maneuver ammunition (10) for supplying into the patron bearing of a maneuver patron device comprises a propellant case for igniting a propellant by means of a percussion cap intended in a base, and a projectile replica projecting from the propellant case. The projectile replica is combined with a middle part, which is fastened in the propellant case. The projectile replica is projected from the middle part and movably led into the middle part. The projectile replica is lockable in the projecting and in the respective position moved into the middle part. The propellant is determined in the space between the base of the propellant case and a membrane (38) intended at the middle part in the rear-side manner. The middle part consists of a front-sided first locking groove (28) and a rear-sided second locking groove (30) at its inner surface and the projectile replica consists of a rear-sided suspended locking finger (32). The projectile replica is formed with a central through hole (34) and a front side with a stop collar. The projectile replica and the middle part consist of plastic material.

Description

Die Erfindung betrifft eine Manövermunition gemäß dem Oberbegriff des Anspruches 1. Eine solche Manövermunition ist aus der DE 4128050 bekannt.The invention relates to a Manövermunition according to the preamble of claim 1. Such Manövermunition is from the DE 4128050 known.

Eine weitere derartige Manövermunition ist beispielsweise als Manöverpatrone DM 128 bekannt.Another such maneuver ammunition is known for example as a maneuver cartridge DM 128.

Aus Funktionsgründen und aufgrund der technischen Anforderungen, die bei der Zuführung der Manövermunition in das Patronenlager eines Manöverpatronengerätes und beim Auswerfen der Treibladungshülse vorgegeben sind, ist die Manövermunition als teleskopartig einschiebbare Munition ausgebildet, d.h. die aus der Treibladungshülse vorstehende Geschossnachbildung in die Treibladungshülse hineinbewegbar.For functional reasons and due to the technical requirements, which are given in the supply of maneuver ammunition in the chamber of a maneuver cartridge device and the ejection of the propellant charge sleeve, the maneuver ammunition is designed as a telescopically insertable ammunition, i. the protruding projectile from the propellant charge projectile into the propellant charge sleeve hineinbewegbar.

Bei der bekannten Manövermunition der oben genannten Art ist die Treibladung in der Treibladungshülse in loser Schüttung vorgesehen. Aus dieser losen Schüttung der Treibladung können Schwankungen beim Gasdruck resultieren. Das wirkt sich auf die Konstanz der Leistung, auf die Zuverlässigkeit und die Sicherheit gegen mögliche Personenschäden aus.In the known maneuver ammunition of the above type, the propellant charge is provided in the propellant charge case in bulk. From this loose charge of the propellant charge fluctuations in gas pressure can result. This affects the constancy of performance, reliability and safety against possible personal injury.

Der Erfindung liegt die Aufgabe zugrunde, eine Manövermunition der eingangs genannten Art zu schaffen, die eine höhere Zuverlässigkeit und Sicherheit gegen Personenschäden besitzt und die eine vergleichsweise konstante Leistung aufweist.The invention has for its object to provide a maneuver ammunition of the type mentioned above, which has a higher reliability and safety against personal injury and has a relatively constant performance.

Diese Aufgabe wird bei einer Manövermunition der eingangs genannten Art erfindungsgemäß durch die Merkmale des Kennzeichenteiles des Anspruches 1 gelöst.This object is achieved according to the invention in a Manövermunition of the type mentioned by the features of the characterizing part of claim 1.

Bevorzugte Aus- bzw. Weiterbildungen der erfindungsgemäßen Manövermunition sind in den Unteransprüchen gekennzeichnet.Preferred embodiments or further developments of the maneuver ammunition according to the invention are characterized in the subclaims.

Die erfindungsgemäße Manövermunition weist die Vorteile auf, dass sie einfach und vergleichsweise kostengünstig herstellbar ist, und dass die Treibladung im Raum zwischen dem Boden der Treibladungshülse und einer am Mittelteil rückseitig vorgesehenen Membrane festgelegt ist, wobei durch diese Festlegung des Treibladungspulvers eine konstante Leistung und eine höhere Zuverlässigkeit und eine erhöhte Sicherheit gegen Personenschäden resultiert. Die Funktionssicherheit wird auch durch die Verrastung der ein Frontteil bildenden Geschossnachbildung an dem in der Treibladungshülse befestigten Mittelteil sichergestellt. Dadurch, dass die Treibladung im hinteren Bereich der Treibladungshülse zwischen deren Boden und der Membrane des in der Treibladungshülse fixierten Mittelteils definiert lokalisiert ist, sind Gasdruckschwankungen vernachlässigbar gering. Bei der erfindungsgemäßen Manövermunition ist ggf. auch eine Weiterverwendung delaborierter Treibladungshülsen und/oder Anzündhütchen realisierbar. Zu diesem Zwecke wird die Treibladungshülse in einem bestimmten Bereich abgeschnitten.The maneuvering ammunition according to the invention has the advantages that it is simple and comparatively inexpensive to produce, and that the propellant charge is fixed in the space between the bottom of the propellant charge shell and a diaphragm provided on the rear side of the middle part, with this determination of the propellant charge powder constant power and a higher Reliability and increased safety against personal injury results. The functional reliability is also ensured by the locking of a front part forming bullet simulation on the fixed part in the propellant charge sleeve. Characterized in that the propellant charge is located defined in the rear region of the propellant charge sleeve between the bottom and the diaphragm of the fixed in the propellant charge sleeve middle part, gas pressure fluctuations are negligible. In the case of the maneuvering ammunition according to the invention, it is optionally also possible to implement a further use of delabored propellant charge cases and / or primer caps. For this purpose, the propellant charge tube is cut off in a certain area.

Weitere Einzelheiten, Merkmale und Vorteile ergeben sich aus der nachfolgenden Beschreibung eines in der Zeichnung dargestellten Ausführungsbeispieles der erfindungsgemäßen Manövermunition.Further details, features and advantages will become apparent from the following description of an embodiment of the invention Manövermunition shown in the drawing.

Es zeigen:

Figur 1
einen Längsschnitt durch die Manövermunition vor der Funktion, und
Figur 2
einen Längsschnitt der Manövermunition gemäß Figur 1 nach der Funktion.
Show it:
FIG. 1
a longitudinal section through the maneuver ammunition before the function, and
FIG. 2
a longitudinal section of the maneuver ammunition according to FIG. 1 after the function.

Die Figuren 1 und 2 verdeutlichen längsgeschnitten eine Ausbildung der Manövermunition 10 mit einer Treibladungshülse 12. Die Treibladungshülse 12 weist einen Mantel 14 und einen Boden 16 auf, durch den die Treibladungshülse 12 rückseitig geschlossen ist. Im Boden 16 der Treibladungshülse 12 ist ein Zündhütchen 18 für eine in der Treibladungshülse 12 vorgesehene Treibladung 20 angeordnet. Bei der Treibladung 20 handelt es sich um ein Treibladungspulver.The Figures 1 and 2 illustrate longitudinally sectioned an embodiment of the maneuver ammunition 10 with a propellant charge shell 12. The propellant charge shell 12 has a shell 14 and a bottom 16, through which the propellant charge shell 12 is closed at the back. In the bottom 16 of the propellant charge case 12, a primer 18 is arranged for a propellant charge 20 provided in the propellant charge case 12. The propellant charge 20 is a propellant charge powder.

Aus der Treibladungshülse steht vor der Funktion der Manövermunition 10 (siehe Figur 1) eine Geschossnachbildung 22 vor, die mit einem Mittelteil 24 kombiniert ist. Das Mittelteil 24 ist in der Treibladungshülse 12 befestigt. Bei dieser Befestigung kann es sich beispielsweise um eine materialschlüssige Befestigung, d.h. um eine Verklebung, handeln. Desgleichen ist es möglich, das Mittelteil 24 im Mantel 14 der Treibladungshülse 12 formschlüssig zu befestigen, d.h. das Mittelteil 24 speziell zu gestalten, um eine zusätzliche Verankerung mit der Treibladungshülse 12 zu verwirklichen. Auch eine mechanische Verbindung des Mittelteiles 24 mit dem Mantel 14 der Treibladungshülse 12 ist möglich.From the propellant charge sleeve is before the function of Manövermunition 10 (see FIG. 1 ) a projectile 22 projectile, which is combined with a central portion 24. The middle part 24 is fixed in the propellant charge sleeve 12. This attachment can be, for example, a material-locking attachment, ie a bond. Likewise, it is possible to secure the middle part 24 in the shell 14 of the propellant charge shell 12 in a form-fitting manner, ie to make the central part 24 special in order to realize an additional anchoring to the propellant charge shell 12. Also, a mechanical connection of the central part 24 with the jacket 14 of the propellant charge sleeve 12 is possible.

Das Mittelteil 24 ist an seiner Innenfläche 26 vorderseitig mit einer ersten Rastnut 28 und rückseitig mit einer zweiten Rastnut 30 ausgebildet. Die ein Frontteil bildende Geschossnachbildung 22 ist rückseitig mit federnden Rastfingern 32 ausgebildet, die in dem in Figur 1 bezeichneten Zustand der Manövermunition vor der Funktion in die vorderseitige erste Rastnut 28 und die in der in Figur 2 gezeichneten Betriebsstellung nach der Funktion der Manövermunition 10 in die rückseitige zweite Rastnut 30 eingerastet sind.The middle part 24 is formed on its inner surface 26 on the front side with a first latching groove 28 and on the rear side with a second latching groove 30. The projectile 22 forming a front part is formed on the back with resilient latching fingers 32, which in the in FIG. 1 designated state of the maneuver ammunition before the function in the front-side first locking groove 28 and in the in FIG. 2 drawn operating position after the function of the maneuver ammunition 10 are engaged in the rear side second locking groove 30.

Die Geschossnachbildung 22 ist mit einem zentralen Durchgangsloch 34 und vorderseitig außen mit einem Anschlagbund 36 ausgebildet.The projectile 22 is formed with a central through hole 34 and the outside with a stop collar 36.

Das in der Treibladungshülse 12 fixierte Mittelteil 24 weist rückseitig in der Nachbarschaft der zweiten Rastnut 30 eine Membrane 38 auf. Die von Treibladungspulver gebildete Treibladung 20 ist in dem Raum zwischen dem Boden 16 der Treibladungshülse 12 und der Membrane 38 des Mittelteils 24 festgelegt. Durch diese definierte Fixierung der Treibladung 20 im hinteren Teil der Treibladungshülse 12 wird sichergestellt, das Gasdruck-Schwankungen nur sehr gering bzw. vernachlässigbar klein sind.The fixed in the propellant charge sleeve 12 central part 24 has the rear side in the vicinity of the second locking groove 30, a diaphragm 38. The propellant charge 20 formed by propellants is fixed in the space between the bottom 16 of the propellant charge case 12 and the diaphragm 38 of the middle portion 24. By this defined fixation of the propellant charge 20 in the rear part of the propellant charge sleeve 12 ensures that the gas pressure fluctuations are only very small or negligible.

Die vorderseitige Geschossnachbildung 22 und das in der Treibladungshülse 12 befestigte Mittelteil 24 bestehen vorzugsweise aus geeignetem Kunststoffmaterial.The front-side projectile 22 and the attached in the propellant charge shell 12 middle part 24 are preferably made of suitable plastic material.

Vor der Funktion der Manövermunition 10 steht die Geschossnachbildung 22 definiert aus dem Mittelteil 24 vor, wobei die federnden Rastfinger 32 der Geschossnachbildung 22 in die vorderseitige erste Rastnut 28 des Mittelteils 24 eingerastet sind.Before the function of the maneuver ammunition 10, the projectile replica 22 is defined from the middle part 24, wherein the resilient latching fingers 32 of the projectile replica 22 are engaged in the front-side first latching groove 28 of the central part 24.

Beim Einführen der Manövermunition 10 in ein Patronenlager eines Manöverpatronengeräts wird die vorderseitig vorstehende Geschossnachbildung 22 in das Mittelteil 24 eingeschoben, wobei die federnden Rastfinger 32 der Geschossnachbildung 22 in die rückseitige zweite Rastnut 30 des Mittelteils 24 einrasten, so dass die Geschossnachbildung 22 in der eingeschobenen hinteren Position arretiert wird. Wird dann das Anzündhütchen 18 gezündet, so wird die zwischen dem Boden 16 der Treibladungshülse 12 und der Membrane 38 des Mittelteils 24 festgelegte Treibladung 20 gezündet. Hierdurch wird die Membrane 38 des Mittelteiles 24 zerstört und der vom gezündeten Treibladungspulver generierte Gasdruck kann durch das zentrale Durchgangsloch 34 der ein Frontteil bildenden Geschossnachbildung 22 nach vorne entweichen, wodurch die Waffe angetrieben wird.When inserting the Manövermunition 10 in a chamber of a maneuver cartridge device, the front projecting bullet replica 22 is inserted into the middle part 24, wherein the resilient latching fingers 32 of the projectile replica 22 engage in the rear second latching groove 30 of the central part 24, so that the projectile replica 22 in the inserted rear Position is locked. If the primer cap 18 is then ignited, the propellant charge 20 defined between the base 16 of the propellant charge casing 12 and the diaphragm 38 of the central part 24 is ignited. As a result, the diaphragm 38 of the central part 24 is destroyed and the gas pressure generated by the ignited propellant charge powder can escape through the central through hole 34 of a front part forming missile replica 22 forward, whereby the weapon is driven.

Die solchermaßen ausgebildete Manövermunition 10 ist preisgünstig realisierbar. Ihre sichere Funktion wird durch die federnde Verrastung der ein Frontteil bildenden Geschossnachbildung 22 sichergestellt. Dadurch, dass die Treibladung 20 im hinteren Bereich der Treibladungshülse 12 - durch die Membrane 38 vorderseitig begrenzt - definiert festgelegt ist, sind Gasdruck-Schwankungen vernachlässigbar gering, woraus eine konstante Leistung, eine höhere Zuverlässigkeit und eine höhere Sicherheit gegen Personenschäden resultiert - wie bereits ausgeführt worden ist.The thus formed maneuver ammunition 10 is inexpensive realizable. Their safe function is ensured by the resilient locking of a front part forming projectile replica 22. Characterized in that the propellant charge 20 at the rear of the propellant charge shell 12 - defined by the membrane 38 front side - defined defined, gas pressure fluctuations are negligible, resulting in a constant performance, higher reliability and a higher safety against personal injury results - as already stated has been.

Bezugsziffernliste:List of reference numerals:

1010
Manövermunitionmaneuver ammunition
1212
Treibladungshülse (von 10)Propellant charge case (from 10)
1414
Mantel (von 12)Coat (of 12)
1616
Boden (von 12)Floor (from 12)
1818
Zündhütchen (in 16 für 20)Primer (in 16 for 20)
2020
Treibladung (von 10)Propellant charge (out of 10)
2222
Geschossnachbildung/Frontteil (von 10)Bullet replica / front part (out of 10)
2424
Mittelteil (von 10 in 12)Middle section (from 10 to 12)
2626
Innenfläche (von 24)Inner surface (from 24)
2828
erste Rastnut (in 26)first detent groove (in 26)
3030
zweite Rastnut (in 26)second detent groove (in 26)
3232
federnde Rastfinger (von 22)resilient snap fingers (from 22)
3434
zentrales Durchgangsloch (in 22)central through hole (in 22)
3636
Anschlagbund (von 22)Stop collar (from 22)
3838
Membrane (von 24)Membrane (from 24)

Claims (5)

  1. Blank round having a propellant charge casing (12) in which a propellant charge (20) is provided, which can be initiated by means of a firing cap (18) provided in the base (16) of the propellant charge casing (12), and having a simulated projectile (22) which projects out of the propellant charge casing (12),
    characterized
    in that the simulated projectile (22) is combined with a centre part (24) which is mounted in the propellant charge casing (12), wherein the simulated projectile (22) projects out of the centre part (24), can be moved in a guided manner into the centre part (24) and can in each case be latched in the projecting position and in the position in which it has been moved into the centre part (24), and in that the propellant charge (20) is fixed in the space between the base (16) of the propellant charge casing (12) and a membrane (38) which is provided on the rear face of the centre part (24).
  2. Blank round according to Claim 1,
    characterized
    in that, at the front on its inner surface (26), the centre part (24) has a first latching groove (28) and, at the rear, has a second latching groove (30), and in that the simulated projectile (22) has sprung latching fingers (32) at the rear.
  3. Blank round according to Claim 1 or 2,
    characterized
    in that the simulated projectile (22) has a central hole (34) through it.
  4. Blank round according to one of Claims 1 to 3,
    characterized
    in that the simulated projectile (22) has a stop collar (36) at the front.
  5. Blank round according to one of Claims 1 to 4,
    characterized
    in that the simulated projectile (22) and the centre part (24) are composed of plastic material.
EP07012428A 2006-07-01 2007-06-26 Blank ammunition Not-in-force EP1873475B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102006030515A DE102006030515B4 (en) 2006-07-01 2006-07-01 Maneuver ammunition with a guided movable missile simulation

Publications (3)

Publication Number Publication Date
EP1873475A2 EP1873475A2 (en) 2008-01-02
EP1873475A3 EP1873475A3 (en) 2008-05-21
EP1873475B1 true EP1873475B1 (en) 2010-06-09

Family

ID=38508891

Family Applications (1)

Application Number Title Priority Date Filing Date
EP07012428A Not-in-force EP1873475B1 (en) 2006-07-01 2007-06-26 Blank ammunition

Country Status (4)

Country Link
EP (1) EP1873475B1 (en)
AT (1) ATE470834T1 (en)
DE (1) DE102006030515B4 (en)
ES (1) ES2345061T3 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE202008017412U1 (en) 2008-04-15 2009-09-24 Rheinmetall Waffe Munition Gmbh Maneuver cartridge or maneuver ammunition

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1138341B (en) * 1959-07-14 1962-10-18 Gustav Genschow & Co Ag Blank cartridge without splinters
FR2394779A1 (en) * 1977-06-14 1979-01-12 France Etat BLANK SHOOTING CARTRIDGE FOR AUTOMATIC INERTIAL CYLINDER HEAD WEAPONS
US5677505A (en) * 1990-03-22 1997-10-14 Dittrich; William A. Reduced energy cartridge
DE4128050C2 (en) * 1991-08-23 1996-08-01 Rheinmetall Ind Gmbh Maneuver cartridge
TW430736B (en) * 2000-07-10 2001-04-21 Combined Service Forces 205Th Bullets for use in training exercises

Also Published As

Publication number Publication date
EP1873475A3 (en) 2008-05-21
ES2345061T3 (en) 2010-09-14
DE102006030515A1 (en) 2008-01-03
EP1873475A2 (en) 2008-01-02
ATE470834T1 (en) 2010-06-15
DE102006030515B4 (en) 2008-05-29

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