EP0361412A2 - Subcalibre ammunition - Google Patents

Subcalibre ammunition Download PDF

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Publication number
EP0361412A2
EP0361412A2 EP89117800A EP89117800A EP0361412A2 EP 0361412 A2 EP0361412 A2 EP 0361412A2 EP 89117800 A EP89117800 A EP 89117800A EP 89117800 A EP89117800 A EP 89117800A EP 0361412 A2 EP0361412 A2 EP 0361412A2
Authority
EP
European Patent Office
Prior art keywords
projectile
core
sabot
storey
tubular
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.)
Withdrawn
Application number
EP89117800A
Other languages
German (de)
French (fr)
Other versions
EP0361412A3 (en
Inventor
Dietrich Dr. Dipl.-Math. Hoffmann
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.)
Mauser Werke Oberndorf GmbH
Original Assignee
Mauser Werke Oberndorf 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 Mauser Werke Oberndorf GmbH filed Critical Mauser Werke Oberndorf GmbH
Publication of EP0361412A2 publication Critical patent/EP0361412A2/en
Publication of EP0361412A3 publication Critical patent/EP0361412A3/en
Withdrawn legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B14/00—Projectiles or missiles characterised by arrangements for guiding or sealing them inside barrels, or for lubricating or cleaning barrels
    • F42B14/06—Sub-calibre projectiles having sabots; Sabots therefor
    • F42B14/064—Sabots enclosing the rear end of a kinetic energy projectile, i.e. having a closed disk shaped obturator base and petals extending forward from said base
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/34—Tubular projectiles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/02—Cartridges, i.e. cases with charge and missile
    • F42B5/03—Cartridges, i.e. cases with charge and missile containing more than one missile

Definitions

  • the invention relates to a sub-caliber ammunition, in particular for aircraft cannons, with a sub-caliber projectile core and a sabot.
  • a sabot designed as a sabot is connected to the sub-caliber projectile core by means of a spring ring provided as a centrifugal force lock.
  • the spring ring expands under the action of the swirl of the projectile, so that the projectile core leaves the sabot.
  • the sabot has a high flow resistance, so that it remains behind the core of the projectile. There is a risk that both the sabot and plastic parts of the hood will hit the shooting aircraft and damage it.
  • DE-OS 35 08 053 describes a sub-caliber floor with a segmented sabot. After the launch, the sabot is broken down into its segments due to its high flow resistance, so that the core of the projectile becomes free. If such a projectile is fired from an aircraft, there is a risk that the aircraft will fly into the sabot segments.
  • the object of the invention is to propose ammunition of the type mentioned in the introduction, in which the sabot separating from the projectile core does not lead to any dangers on the firing side.
  • the above object is achieved in the case of ammunition of the type mentioned at the outset in that the sabot is designed as a secondary projectile which is stable in itself and which has a predictable trajectory.
  • the sabot flies like a bullet after being separated from the core. On the one hand, this ensures that a shooting aircraft cannot hit the sabot. On the other hand, the effect of the ammunition is increased, since in addition to the core of the projectile, the sabot can also have a projectile effect. A particular advantage is that the trajectory of the sabot can be calculated. Furthermore, higher impact energies and shorter target times mean higher target effects are achieved due to the sub-caliber.
  • the sabot as a secondary storey can be designed in the embodiment of the invention as a tubular storey in which the projectile body is arranged coaxially.
  • the sabot can be a projectile core on which an effective tubular projectile is arranged coaxially.
  • the centrifugal force safety device is designed as a seal between the tubular projectile and the projectile core. This eliminates the need for additional measures with which the projectile core guided in the tube storey is to be sealed with respect to this, in order to avoid an undesired passage of propellant gas between the tube storey and the storey core.
  • FIG. 1 is a sub-caliber ammunition with a tube storey 15 trained sabot provided in which a projectile core 16 is inserted.
  • the tube storey 15 also has a ballistically shaped tip 17 as does the projectile core 16 with the tip 18.
  • the tube projectile is also effective with this combination.
  • the sabot 19 is designed as a projectile core with a base body 20 and a ballistic tip 21 formed thereon.
  • a guide band 22 is provided on the lateral surface of the base body 20 in a corresponding annular groove.
  • a tube storey 1 has a guide band 2.
  • the front end 3 of the tubular storey 1 is tapered by a bevel 4.
  • a sub-caliber projectile core 6 is inserted flush.
  • a spring ring 7 is provided for connecting the projectile core 6 to the tubular projectile 1. This lies partly in an annular groove 8 of the projectile core 6 and partly in an annular groove 9 of the tubular storey 1.
  • the spring ring 7 also seals an existing gap between the outer circumference of the storey core 6 and the inner circumference of the tubular storey 1.
  • the projectile core 6, with its ogive-shaped head part 10, projects beyond the front end 3 of the tubular storey 1.
  • the reverse construction is also conceivable here.
  • a small free space 11 is provided between the head part 10 and the front end 3.
  • a rear-side, open end 12 of the tubular storey 1 projects beyond a floor 13 of the storey core 6, so that there is a space 14.
  • the spring ring 7 When leaving the gun barrel, the spring ring 7 widens as a result of the swirl, so that the projectile core 6 is axially free from the tubular projectile 1.
  • the projectile core 6 and the tubular projectile 1 leave due to their different air resistances and their different inertias.
  • the tube storey 1 also shows a stable, swirl-stabilized flight behavior with a low Cd value in internal currents, so that it surely quickly moves away from the weapon barrel or the shooting aircraft.
  • the tubular storey 1 can be designed such that it assumes essentially the same trajectory as the storey core 6. The tubular storey 1 then becomes effective in the target of the storey core 6.
  • the projectile core 6 can be designed as a balancing projectile, as a fragmentary projectile or as a detonator projectile.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Elimination Of Static Electricity (AREA)

Abstract

Bei einer unterkalibrigen Munition, insbesondere für Flugzeugbordkanonen, soll sichergestellt sein, daß ein sich von einem Geschoßkern (6) trennender Treibspiegel (1) abschußseitig nicht zu Gefährdungen führt. Es ist hierfür der Treibspiegel als Röhrengeschoß (1) ausgebildet, in dem der Geschoßkern (6) koaxial angeordnet ist.In the case of sub-caliber ammunition, in particular for aircraft cannons, it should be ensured that a sabot (1) separating from a projectile core (6) does not lead to any dangers on the firing side. For this purpose, the sabot is designed as a tubular storey (1) in which the storey core (6) is arranged coaxially.

Description

Die Erfindung betrifft eine unterkalibrige Munition, insbesondere für Flugzeugbordkanonen, mit einem unterkalibrigen Geschoßkern und einem Treibspiegel.The invention relates to a sub-caliber ammunition, in particular for aircraft cannons, with a sub-caliber projectile core and a sabot.

Eine derartige Munition ist in der DE-PS 31 31 540 beschrieben. Ein als Treibkäfig ausgebildeter Treibspiegel ist mittels eines als Fliehkraft­sicherung vorgesehenen Federrings mit dem unterkalibrigen Geschoßkern verbunden. Unter der Wirkung des Dralls des Geschosses weitet sich der Federring auf, so daß der Geschoßkern den Treibkäfig verläßt. Der Treib­käfig hat einen hohen Strömungswiderstand, so daß er gegenüber dem Geschoß­kern zurückbleibt. Es besteht dabei die Gefahr, daß sowohl der Treib­käfig als auch Kunststoffteile der Haube das abschießende Flugzeug treffen und dieses beschädigen.Such ammunition is described in DE-PS 31 31 540. A sabot designed as a sabot is connected to the sub-caliber projectile core by means of a spring ring provided as a centrifugal force lock. The spring ring expands under the action of the swirl of the projectile, so that the projectile core leaves the sabot. The sabot has a high flow resistance, so that it remains behind the core of the projectile. There is a risk that both the sabot and plastic parts of the hood will hit the shooting aircraft and damage it.

In der DE-OS 35 08 053 ist ein unterkalibriges Geschoß mit einem aus Segmenten bestehenden Treibkäfig beschrieben. Der Treibkäfig wird nach dem Abschuß infolge seines hohen Strömungswiderstandes in seine Segmente zerlegt, so daß der Geschoßkern frei wird. Erfolgt der Abschuß eines solchen Geschosses von einem Flugzeug aus, dann besteht die Gefahr, daß das Flugzeug in die Treibkäfigsegmente hineinfliegt.DE-OS 35 08 053 describes a sub-caliber floor with a segmented sabot. After the launch, the sabot is broken down into its segments due to its high flow resistance, so that the core of the projectile becomes free. If such a projectile is fired from an aircraft, there is a risk that the aircraft will fly into the sabot segments.

Aufgabe der Erfindung ist es, eine Munition der eingangs genannten Art vorzuschlagen, bei der der sich vom Geschoßkern trennende Treibspiegel abschußseitig nicht zu Gefährdungen führt.The object of the invention is to propose ammunition of the type mentioned in the introduction, in which the sabot separating from the projectile core does not lead to any dangers on the firing side.

Erfindungsgemäß ist obige Aufgabe bei einer Munition der eingangs genannten Art dadurch gelöst, daß der Treibspiegel als ein für sich stabil und mit berechenbarer Flugbahn fliegendes Sekundärgeschoß ausgebildet ist.According to the invention, the above object is achieved in the case of ammunition of the type mentioned at the outset in that the sabot is designed as a secondary projectile which is stable in itself and which has a predictable trajectory.

Der Treibspiegel fliegt nach der Trennung vom Geschoßkern wie ein Geschoß weiter. Dadurch ist einerseits erreicht, daß ein abschießen­des Flugzeug nicht auf den Treibspiegel treffen kann. Andererseits ist die Wirkung der Munition erhöht, da neben dem Geschoßkern auch der Treibspiegel Geschoßwirkung haben kann. Als besonderer Vorteil erweist sich dabei, daß die Flugbahn des Treibspiegels berechenbar ist. Ferner werden durch die Unterkalibrigkeit höhere Auftreffenergien und durch kürzere Flugzeiten gleichzeitig höhere Zielwirkungen er­zielt. Der Treibspiegel als Sekundärgeschoß kann in Ausbildung der Erfindung als Röhrengeschoß ausgebildet sein, in dem der Geschoß­körper koaxial angeordnet ist. Andererseits kann der Treibspiegel ein Geschoßkern sein, an dem ein effektives Röhrengeschoß koaxial angeordnet ist.The sabot flies like a bullet after being separated from the core. On the one hand, this ensures that a shooting aircraft cannot hit the sabot. On the other hand, the effect of the ammunition is increased, since in addition to the core of the projectile, the sabot can also have a projectile effect. A particular advantage is that the trajectory of the sabot can be calculated. Furthermore, higher impact energies and shorter target times mean higher target effects are achieved due to the sub-caliber. The sabot as a secondary storey can be designed in the embodiment of the invention as a tubular storey in which the projectile body is arranged coaxially. On the other hand, the sabot can be a projectile core on which an effective tubular projectile is arranged coaxially.

Bei einer Munition mit einer zwischen dem Treibspiegel und dem Ge­schoßkern vorgesehenen Fliehkraftsicherung, die sich unter der Wirkung des Dralls löst, ist in bevorzugter Ausgestaltung der Erfindung die Fliehkraftsicherung als Abdichtung zwischen dem Röhrengeschoß und dem Geschoßkern ausgebildet. Dadurch erübrigen sich zusätzliche Maßnahmen, mit denen der im Röhrengeschoß geführte Geschoßkern gegen­über diesem abzudichten ist, um einen unerwünschten Durchtritt von Treibladungsgas zwischen dem Röhrengeschoß und dem Geschoßkern zu vermeiden.In the case of ammunition with a centrifugal force lock provided between the sabot and the projectile core, which releases under the action of the swirl, in a preferred embodiment of the invention, the centrifugal force safety device is designed as a seal between the tubular projectile and the projectile core. This eliminates the need for additional measures with which the projectile core guided in the tube storey is to be sealed with respect to this, in order to avoid an undesired passage of propellant gas between the tube storey and the storey core.

Weitere vorteilhafte Ausgestaltungen der Erfindung ergeben sich aus den Unteransprüchen und der folgenden Beschreibung von Ausfüh­rungsbeispielen. Es zeigen:

  • Fig. 1 einen Geschoßkern in einem röhrenförmigen Treibspiegel, schematisch im Schnitt
  • Fig. 2 ein Röhrengeschoß auf einem Treibspiegel, schematisch im
  • Schnitt
  • Fig. 3 einen Geschoßkern im Röhrengeschoß im Schnitt.
Further advantageous refinements of the invention result from the subclaims and the following description of exemplary embodiments. Show it:
  • Fig. 1 shows a projectile core in a tubular sabot, schematically in section
  • Fig. 2 shows a tube projectile on a sabot, schematically in
  • cut
  • Fig. 3 shows a floor core in the tube floor in section.

Nach Figur 1 ist eine unterkalibrige Munition mit einem als Röhren­ geschoß 15 ausgebildeten Treibspiegel vorgesehen, in das ein Geschoß­kern 16 eingesetzt ist. Das Röhrengeschoß 15 weist dabei ebenso eine ballistisch geformte Spitze 17 wie der Geschoßkern 16 mit der Spitze 18 auf. Neben dem Geschoßkern 16 ist bei dieser Kombination auch das Röhrengeschoß effektiv.According to Figure 1 is a sub-caliber ammunition with a tube storey 15 trained sabot provided in which a projectile core 16 is inserted. The tube storey 15 also has a ballistically shaped tip 17 as does the projectile core 16 with the tip 18. In addition to the projectile core 16, the tube projectile is also effective with this combination.

In Figur 2 ist der Treibspiegel 19 als Geschoßkern mit einem Sockel­körper 20 und einer daran angeformten ballistischen Spitze 21 ausge­bildet. Auf der Mantelfläche des Sockelkörpers 20 ist in einer ent­sprechenden Ringnut ein Führungsband 22 vorgesehen. Die vom Sockel­körper 20 im Durchmesser etwas abgesetzte Geschoßspitze 21 läßt auf der Stirnfläche 23 des Sockelkörpers 20 eine Ringfläche frei für die Anordnung des Röhrengeschosses 24, welches wiederum eine ballistisch geformte Spitze 25 besitzt.In Figure 2, the sabot 19 is designed as a projectile core with a base body 20 and a ballistic tip 21 formed thereon. A guide band 22 is provided on the lateral surface of the base body 20 in a corresponding annular groove. The projectile tip 21, which is somewhat offset in diameter from the base body 20, leaves an annular surface on the end face 23 of the base body 20 free for the arrangement of the tubular storey 24, which in turn has a ballistically shaped tip 25.

Ein Röhrengeschoß 1 weist ein Führungsband 2 auf. Das frontseitige Ende 3 des Röhrengeschosses 1 ist durch eine Schräge 4 zugespitzt. In den zylindrischen Innenraum 5 des Röhrengeschossses 1 ist ein unterkalibriger Geschoßkern 6 bündig eingeschoben.A tube storey 1 has a guide band 2. The front end 3 of the tubular storey 1 is tapered by a bevel 4. In the cylindrical interior 5 of the tubular storey 1, a sub-caliber projectile core 6 is inserted flush.

Zur Verbindung des Geschoßkernes 6 mit dem Röhrengeschoß 1 ist ein Federring 7 vorgesehen. Dieser liegt teils in einer Ringnut 8 des Geschoßkerns 6 und teils in einer Ringnut 9 des Röhrengeschosses 1. Der Federring 7 dichtet dabei zugleich einen zwischen dem Außenumfang des Geschoßkernes 6 und dem Innenumfang des Röhrenge­schosses 1 bestehenden Spalt ab.A spring ring 7 is provided for connecting the projectile core 6 to the tubular projectile 1. This lies partly in an annular groove 8 of the projectile core 6 and partly in an annular groove 9 of the tubular storey 1. The spring ring 7 also seals an existing gap between the outer circumference of the storey core 6 and the inner circumference of the tubular storey 1.

Der Geschoßkern 6 überragt mit seinem ogivenförmig gestalteten Kopf­teil 10 das frontseitige Ende 3 des Röhrengeschosses 1. Hier ist auch die umgekehrte Bauweise denkbar. Zwischen dem Kopfteil 10 und dem frontseitigen Ende 3 ist ein kleiner Freiraum 11 vorgesehen.The projectile core 6, with its ogive-shaped head part 10, projects beyond the front end 3 of the tubular storey 1. The reverse construction is also conceivable here. A small free space 11 is provided between the head part 10 and the front end 3.

Ein heckseitiges, offenes Ende 12 des Röhrengeschosses 1 überragt einen Boden 13 des Geschoßkerns 6, so daß ein Raum 14 besteht.A rear-side, open end 12 of the tubular storey 1 projects beyond a floor 13 of the storey core 6, so that there is a space 14.

Beim Abschuß der Munition wirkt Treibladungsgas auf den Boden 13 und das heckseitige Ende 12. Der Federring 7 übernimmt dabei die axiale Verbindung zwischen dem Geschoßkern 6 und dem Röhrengeschoß 1. Über das Führungsband 2 wird dem Röhrengeschoß 1 und damit auch dem Geschoßkern 6 ein Drall aufgeprägt.When the ammunition is fired, propellant gas acts on the bottom 13 and the rear end 12. The spring ring 7 takes over the axial connection between the projectile core 6 and the tubular projectile 1. A swirl is impressed on the tubular projectile 1 and thus also on the projectile core 6 .

Beim Verlassen des Waffenrohres weitet sich infolge des Dralls der Federring 7 auf, so daß der Geschoßkern 6 vom Röhrengeschoß 1 axial frei ist. Der Geschoßkern 6 und das Röhrengeschoß 1 verlassen sich infolge ihrer unterschiedlichen Luftwiderstände und ihrer unter­schiedlichen Trägheiten.When leaving the gun barrel, the spring ring 7 widens as a result of the swirl, so that the projectile core 6 is axially free from the tubular projectile 1. The projectile core 6 and the tubular projectile 1 leave due to their different air resistances and their different inertias.

Auch das Röhrengeschoß 1 zeigt ein stabiles, drallstabilisiertes Flugverhalten mit einem bei Innenströmung niedrigen Cw-Wert, so daß es sich mit Sicherheit schnell vom Waffenrohr bzw. dem abschießen­den Flugzeug entfernt.The tube storey 1 also shows a stable, swirl-stabilized flight behavior with a low Cd value in internal currents, so that it surely quickly moves away from the weapon barrel or the shooting aircraft.

Durch eine entsprechende Gestaltung der Abmessungen und der Masse läßt sich das Röhrengeschoß 1 so auslegen, daß es im wesentlichen die gleiche Flugbahn annimmt wie der Geschoßkern 6. Das Röhrengeschoß 1 wird dann im Ziel des Geschoßkerns 6 wirksam.By appropriate design of the dimensions and the mass, the tubular storey 1 can be designed such that it assumes essentially the same trajectory as the storey core 6. The tubular storey 1 then becomes effective in the target of the storey core 6.

Der Geschoßkern 6 kann als Wuchtgeschoß, als Splittergeschoß oder als Zündergeschoß ausgelegt sein.The projectile core 6 can be designed as a balancing projectile, as a fragmentary projectile or as a detonator projectile.

Claims (11)

1. Unterkalibrige Munition, insbesondere für Flugzeugbordkanonen, mit einem unterkalibrigen Geschoßkern und einem Treibspiegel, dadurch gekennzeichnet,
daß der Treibspiegel als ein für sich stabil und mit berechenbarer Flugbahn fliegendes Sekundärgeschoß ausgebildet ist.1. Sub-caliber ammunition, in particular for aircraft cannons, with a sub-caliber projectile core and a sabot, characterized in that
that the sabot is designed as a secondary floor that is stable per se and has a predictable flight path. 2. Munition nach Anspruch 1,
dadurch gekennzeichnet,
daß der Treibspiegel als Röhrengeschoß (1) ausgebildet ist, in dem der Geschoßkern (6) koaxial angeordnet ist.2. Ammunition according to claim 1,
characterized,
that the sabot is designed as a tubular projectile (1) in which the projectile core (6) is arranged coaxially. 3. Munition nach Anspruch 1,
dadurch gekennzeichnet,
daß der Treibspiegel als Geschoßkern (19) ausgebildet ist, an dem koaxial ein effektives Röhrengeschoß (24) angeordnet ist.3. Ammunition according to claim 1,
characterized,
that the sabot is designed as a projectile core (19) on which an effective tubular projectile (24) is arranged coaxially. 4. Munition nach Anspruch 2 mit einer zwischen dem Treibspiegel und dem Geschoßkern vorgesehenen Fliehkraftsicherung, die sich unter der Wirkung des Dralls löst,
dadurch gekennzeichnet,
daß die Fliehkraftsicherung als Abdichtung zwischen dem Röhren­geschoß (1) und dem Geschoßkern (6) ausgebildet ist.4. Ammunition according to claim 2 with a centrifugal force lock provided between the sabot and the projectile core, which releases under the action of the swirl
characterized,
that the centrifugal force device is designed as a seal between the tubular storey (1) and the storey core (6). 5. Munition nach Anspruch 4,
dadurch gekennzeichnet,
daß die Abdichtung von einem Federring (7) gebildet ist.5. Ammunition according to claim 4,
characterized,
that the seal is formed by a spring washer (7). 6. Munition nach einem der vorhergehenden Ansprüche,
dadurch gekennzeichnet,
daß der Kopfteil (10) des Geschoßkerns (6) das frontseitige Ende (3) des Röhrengeschosses (1) überragt.6. Ammunition according to one of the preceding claims,
characterized,
that the head part (10) of the projectile core (6) the front Exceeds end (3) of the tubular storey (1). 7. Munition nach einem der vorhergehenden Ansprüche,
dadurch gekennzeichnet,
daß das offene, heckseitige Ende (12) des Röhrengeschosses (1) den Geschoßkern (6) überragt.7. Ammunition according to one of the preceding claims,
characterized,
that the open, rear end (12) of the tubular storey (1) projects beyond the storey core (6). 8. Munition nach einem der vorhergehenden Ansprüche,
dadurch gekennzeichnet,
daß das frontseitige Ende (3) des Röhrengeschosses (1) durch eine Schräge (4) zugespitzt ist.8. Ammunition according to one of the preceding claims,
characterized,
that the front end (3) of the tubular storey (1) is tapered by a bevel (4). 9. Munition nach einem der vorhergehenden Ansprüche,
dadurch gekennzeichnet,
daß zwischen dem frontseitigen Ende (3) und dem Kopfteil (10) des Geschoßkerns (6) ein Freiraum (11) besteht.9. Ammunition according to one of the preceding claims,
characterized,
that between the front end (3) and the head part (10) of the projectile core (6) there is a free space (11). 10. Munition nach Anspruch 2,
dadurch gekennzeichnet,
daß der Geschoßkern als Pfeilgeschoß ausgebildet ist.10. Ammunition according to claim 2,
characterized,
that the projectile core is designed as an arrow projectile. 11. Munition nach Anspruch 3,
dadurch gekennzeichnet,
daß der als Geschoßkern (19) ausgebildete Treibspiegel eine Ge­schoßspitze (21) aufweist,um welche koaxial das Röhrengeschoß (24) angeordnet ist und auf der Stirnfläche aufsteht.11. Ammunition according to claim 3,
characterized,
that the sabot formed as a projectile core (19) has a projectile tip (21) around which the tubular projectile (24) is arranged coaxially and stands on the end face.
EP19890117800 1988-09-29 1989-09-27 Subcalibre ammunition Withdrawn EP0361412A3 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3833001A DE3833001A1 (en) 1988-09-29 1988-09-29 SUB-CALIBRAL AMMUNITION
DE3833001 1988-09-29

Publications (2)

Publication Number Publication Date
EP0361412A2 true EP0361412A2 (en) 1990-04-04
EP0361412A3 EP0361412A3 (en) 1990-09-26

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Family Applications (1)

Application Number Title Priority Date Filing Date
EP19890117800 Withdrawn EP0361412A3 (en) 1988-09-29 1989-09-27 Subcalibre ammunition

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US (1) US4939997A (en)
EP (1) EP0361412A3 (en)
DE (1) DE3833001A1 (en)

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NO310379B1 (en) * 1999-06-04 2001-06-25 Nammo Raufoss As Deceleration and locking device for use between a projectile and a pilot fin in a missile
US6945088B2 (en) 2002-05-14 2005-09-20 The United States Of America As Represented By The Secretary Of The Navy Multi-fragment impact test specimen
US7201104B2 (en) * 2002-08-21 2007-04-10 Ra Brands, L.L.C. Lead attached sabot slug
FR2867267B1 (en) * 2004-03-08 2006-05-26 Jean Claude Sauvestre HUNTING BALL WITH EXPANSION RING
US7451705B2 (en) * 2004-03-17 2008-11-18 Fry Grant R Non-discarding sabot projectile system
FR2892867B1 (en) * 2005-10-27 2008-01-18 Airbus France Sas MIXED DEVICE FOR MONITORING POWER TRANSFER BETWEEN TWO HEADS OF A CONTINUOUS NETWORK AND SUPPLYING AN ALTERNATING CURRENT MOTOR
US8985026B2 (en) 2011-11-22 2015-03-24 Alliant Techsystems Inc. Penetrator round assembly
US9188417B2 (en) 2013-08-01 2015-11-17 Raytheon Company Separable sabot for launching payload
US9157716B1 (en) * 2014-09-29 2015-10-13 The United States Of America As Represented By The Secretary Of The Army Shot start ring for projectile
RU2601699C1 (en) * 2015-07-30 2016-11-10 Закрытое акционерное общество "Новосибирский патронный завод" (ЗАО "НПЗ") Bullet
US10345086B1 (en) * 2017-12-18 2019-07-09 The United States Of America As Represented By The Secretary Of The Army MOUT projectile with sabot integrated shot start

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EP0095868A2 (en) * 1982-06-01 1983-12-07 The State Of Israel Ministry Of Defence Rafael Armament Development Authority A sub-caliber projectile

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GB1430058A (en) * 1969-06-13 1976-03-31 Heckler & Koch Gmbh Ammunition
US4301736A (en) * 1976-03-26 1981-11-24 The United States Of America As Represented By The Secretary Of The Army Supersonic, low drag tubular projectile
EP0069809A1 (en) * 1981-05-21 1983-01-19 Werkzeugmaschinenfabrik Oerlikon-Bührle AG Tubular projectile
EP0095868A2 (en) * 1982-06-01 1983-12-07 The State Of Israel Ministry Of Defence Rafael Armament Development Authority A sub-caliber projectile

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DE3833001A1 (en) 1990-04-05
US4939997A (en) 1990-07-10
EP0361412A3 (en) 1990-09-26

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