EP0224154B1 - Missile with multiple submissiles - Google Patents

Missile with multiple submissiles Download PDF

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Publication number
EP0224154B1
EP0224154B1 EP86115870A EP86115870A EP0224154B1 EP 0224154 B1 EP0224154 B1 EP 0224154B1 EP 86115870 A EP86115870 A EP 86115870A EP 86115870 A EP86115870 A EP 86115870A EP 0224154 B1 EP0224154 B1 EP 0224154B1
Authority
EP
European Patent Office
Prior art keywords
projectile
tie rod
region
stop
bores
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.)
Expired - Lifetime
Application number
EP86115870A
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German (de)
French (fr)
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EP0224154A1 (en
Inventor
Gerald Rieger
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 Verwaltungs Stiftung
Original Assignee
Diehl GmbH and Co
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Filing date
Publication date
Application filed by Diehl GmbH and Co filed Critical Diehl GmbH and Co
Publication of EP0224154A1 publication Critical patent/EP0224154A1/en
Application granted granted Critical
Publication of EP0224154B1 publication Critical patent/EP0224154B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F42B30/00—Projectiles or missiles, not otherwise provided for, characterised by the ammunition class or type, e.g. by the launching apparatus or weapon used
    • F42B30/08—Ordnance projectiles or missiles, e.g. shells

Definitions

  • the invention relates to a projectile with active bodies which have a cylindrical casing wall and are held axially stacked between a floor and a projectile head and for the ejection of which an ejection device is arranged on the projectile.
  • DE-GM 82 18 780 describes a projectile in which a large number of active bodies, which are stacked between a floor and a projectile head, are held together by means of a tie rod which breaks during the ejection process.
  • the tie rod extends centrally through the active bodies. This arrangement cannot be used for active bodies with P charges.
  • EP-A2-0 114 602 describes a projectile for transporting several active bodies.
  • the - thin - shell is relieved of the stresses that occur during launch and flight.
  • the intrinsic stability of the active bodies is not used to relieve the projectile.
  • the object of the invention is to propose a projectile of the type mentioned in the introduction, in which a separate projectile casing is omitted and in which the active bodies themselves ensure the necessary strength of the projectile.
  • the above object is achieved in a projectile of the type mentioned at the outset in that the jacket walls of the active bodies themselves form the projectile envelope, the jacket wall of each active body is provided with at least two axially parallel, continuous bores, that tie rods are inserted through the aligned bores of the jacket walls of the active bodies , which are attached at one end to the floor and at the other end to the head of the floor and that each tie rod has predetermined breaking points in the area of the floor, in the area of the joint between two active bodies and in the area of the floor.
  • the jacket walls of the stacked active bodies themselves form the shell.
  • the projectile head and the projectile floor are braced against one another via the jacket walls.
  • the projectile has the necessary firing resistance.
  • the swirl transmission takes place from the floor of the floor via the active bodies to the floor of the floor.
  • the tie rods break at the predetermined breaking points. As a result, the active bodies are free from one another and from the floor and the floor head.
  • a clamping device is formed. This ensures that after breaking the predetermined breaking points, the tie rod parts remain in the holes. There are therefore no significant material mass differences in the jacket walls, which would be unfavorable in the case of shaped charges for producing an explosive-shaped projectile, called P charges.
  • two P-charge active bodies 3 and 4 are stacked on top of one another. Their jacket walls are designated 5 and 6 respectively. The outer diameter of the floor 1, the projectile head 2 and the active body 3, 4 are aligned.
  • Axial parallel, continuous bores 7 and 8 or 9 and 10 are provided in each jacket wall 5, 6.
  • the floor 1 has threaded holes 11 and 12.
  • steps 13, 14 are formed on the floor 1 and the jacket walls.
  • the steps 13, 14 can also be designed as toothing extending over part of the circumference.
  • Tie rods 15, 16 are screwed into the threaded bores 11 and 12 and extend through the bores 7, 9 and 8, 10, respectively.
  • the tie rods 15, 16 project through guide bores 17, 18 of an ejection cylinder 19 mounted in the projectile head 2 and bores 20, 21 of a collar 22 of the projectile head 2. They are clamped to the collar 22 by means of clamping nuts 23, 24.
  • the ejection cylinder 19 is slidably mounted on an igniter 25 of the projectile head 2. There is a gas space 26 between the igniter 25 and the ejection cylinder 19. The ejection cylinder 19 is in contact with the jacket wall 5.
  • a first predetermined breaking point 27 is formed on the tie rod 15 or 16 in the area of the floor 1.
  • a second predetermined breaking point 28 is formed on the tie rods 15, 16.
  • a third predetermined breaking point 29 is close to the projectile head 2.
  • the diameter of the tie rod 15, 16 between the predetermined breaking points 27, 28 is slightly larger than the diameter between the predetermined breaking points 28 and 29.
  • the diameter of the tie rod 15, 16 between the predetermined breaking points 28 and 29 is slightly larger than between the predetermined breaking point 29 and the clamping nut 23 and 24.
  • corresponding stops 30, 31 are formed for the tie rod section with the larger diameter in each case.
  • the distance between the stop 30 and the predetermined breaking point 29 is larger ß than the distance between the stop 31 and the predetermined breaking point 28 (see FIG. 1).
  • the jacket walls 5 and 6 absorb the launch acceleration.
  • the tie rods 15, 16 transmit the swirl acceleration.
  • the ejection cylinder 19 presses on the jacket wall 5 and via the jacket wall 6 on the floor 1.
  • the tie rods 15, 16 initially tear at the predetermined breaking points 27.
  • the floor 1 is thereby released.
  • the jacket walls 5, 6 move on the tie rods 15, 16 so that the stop 31 meets the larger diameter of the tie rod 15, 16 at the predetermined breaking points 28.
  • the predetermined breaking points 28 also tear.
  • the active body 4 is now free.
  • the stop 30 of the active body 3 hits the section of larger diameter at the predetermined breaking point 29.
  • the predetermined breaking points 29 tear, so that the active body 3 is now free of the projectile head 2.
  • a self-locking cone 34 is formed on the tie rod 15, 16 within the bores 7 to 10, to which a corresponding conical surface 35 of the bores 7 to 10 is assigned.
  • the cone 34 and the conical surface 35 replace the stops 30 and 31. If the cone 34 is pulled into the conical surface 35, then the intended breaking point 28, 29 tears. About the self-locking effect of the cone 34, the tie rod part remains in the jacket wall 5 and 6 held.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Seal Device For Vehicle (AREA)

Description

Die Erfindung betrifft ein Geschoß mit Wirkkörpern, die eine zylindrische Mantelwandung aufweisen und zwischen einem Geschoßboden und einem Geschoßkopf axial gestapelt gehalten sind und für deren Ausstoß am Geschoß eine Ausstoßvorrichtung angeordnet ist.The invention relates to a projectile with active bodies which have a cylindrical casing wall and are held axially stacked between a floor and a projectile head and for the ejection of which an ejection device is arranged on the projectile.

Es ist bekannt, Wirkkörper, die starke Mantelwandungen aufweisen, wie beispielsweise P-Ladungswirkkörper, in Geschossen mit dünnwandiger Geschoßhülle unterzubringen. Bei solchen Geschossen treten Festigkeitsprobleme im Hinblick auf die Abschußfestigkeit des Geschosses und der Wirkkörper, der Drallübertragung vom Waffenrohr auf das Geschoß bzw. die Wirkkörper und den Ausstoßvorgang der Wirkkörper auf.It is known to accommodate active bodies which have strong jacket walls, such as, for example, P-charge active bodies, in floors with a thin-walled shell. With such projectiles, strength problems arise with regard to the firing strength of the projectile and the active bodies, the swirl transmission from the weapon barrel to the projectile or the active bodies and the ejection process of the active bodies.

In dem DE-GM 82 18 780 ist ein Geschoß beschrieben, bei dem eine Vielzahl von Wirkkörpern, die zwischen einem Geschoßboden und einem Geschoßkopf gestapelt sind, mittels eines Zugankers zusammengehalten werden, der beim Ausstoßvorgang bricht. Der Zuganker erstreckt sich zentral durch die Wirkkörper. Für Wirkkörper mit P-Ladungen kann diese Anordnung nicht verwendet werden.DE-GM 82 18 780 describes a projectile in which a large number of active bodies, which are stacked between a floor and a projectile head, are held together by means of a tie rod which breaks during the ejection process. The tie rod extends centrally through the active bodies. This arrangement cannot be used for active bodies with P charges.

In der EP-A2-0 114 602 ist ein Geschoß zum Transport mehrerer Wirkkörper beschrieben. Die - dünne - Geschoßhülle ist von beim Abschuß und beim Flug auftretenden Belastungen entlastet. Die Eigenstabilität der Wirkkörper ist nicht zur Geschoßentlastung ausgenutzt.EP-A2-0 114 602 describes a projectile for transporting several active bodies. The - thin - shell is relieved of the stresses that occur during launch and flight. The intrinsic stability of the active bodies is not used to relieve the projectile.

Aufgabe der Erfindung ist es, ein Geschoß der eingangs genannten Art vorzuschlagen, bei dem eine eigene Geschoßhülle entfällt und bei dem die Wirkkörper selbst die nötige Festigkeit des Geschosses gewährleisten.The object of the invention is to propose a projectile of the type mentioned in the introduction, in which a separate projectile casing is omitted and in which the active bodies themselves ensure the necessary strength of the projectile.

Erfindungsgemäß ist obige Aufgabe bei einem Geschoß der eingangs genannten Art dadurch gelöst, daß die Mantelwandungen der Wirkkörper selbst die Geschoßhülle bilden, die Mantelwandung jedes Wirkkörpers mit wenigstens zwei achsparallelen, durchgehenden Bohrungen versehen ist, daß durch die fluchtenden Bohrungen der Mantelwandungen der Wirkkörper Zuganker gesteckt sind, die mit ihrem einen Ende am Geschoßboden und mit ihrem anderen Ende am Geschoßkopf befestigt sind und daß jeder Zuganker im Bereich des Geschoßbodens, im Bereich der Stoßstelle zwischen zwei Wirkkörpern und im Bereich des Geschoßkopfes Sollbruchstellen aufweist.According to the invention, the above object is achieved in a projectile of the type mentioned at the outset in that the jacket walls of the active bodies themselves form the projectile envelope, the jacket wall of each active body is provided with at least two axially parallel, continuous bores, that tie rods are inserted through the aligned bores of the jacket walls of the active bodies , which are attached at one end to the floor and at the other end to the head of the floor and that each tie rod has predetermined breaking points in the area of the floor, in the area of the joint between two active bodies and in the area of the floor.

Die Mantelwandungen der gestapelten Wirkkörper bilden dabei selbst die Geschoßhülle. Mittels der Zuganker sind über die Mantelwandungen der Geschoßkopf und der Geschoßboden gegeneinander verspannt. Das Geschoß weist die notwendige Abschußfestigkeit auf. Die Drallübertragung erfolgt vom Geschoßboden über die Wirkkörper auf den Geschoßkopf. Bei der Auslösung des Ausstoßvorganges brechen die Zuganker an den Sollbruchstellen. Dadurch werden die Wirkkörper voneinander und von dem Geschoßboden und dem Geschoßkopf frei.The jacket walls of the stacked active bodies themselves form the shell. By means of the tie rods, the projectile head and the projectile floor are braced against one another via the jacket walls. The projectile has the necessary firing resistance. The swirl transmission takes place from the floor of the floor via the active bodies to the floor of the floor. When the ejection process is triggered, the tie rods break at the predetermined breaking points. As a result, the active bodies are free from one another and from the floor and the floor head.

In bevorzugter Ausgestaltung der Erfindung ist an dem Zuganker im Bereich jeder MantelwandungIn a preferred embodiment of the invention is on the tie rod in the area of each jacket wall

eine Klemmvorrichtung ausgebildet. Dadurch ist erreicht, daß nach dem Brechen der Sollbruchstellen die Zugankerteile in den Bohrungen verbleiben. Es treten also in den Mantelwandungen keine wesentlichen Materialmassenunterschiede auf, die bei Hohlladungen zur Erzeugung eines sprengstoffgeformten Projektils, P-Ladungen genannt, ungünstig wären.a clamping device is formed. This ensures that after breaking the predetermined breaking points, the tie rod parts remain in the holes. There are therefore no significant material mass differences in the jacket walls, which would be unfavorable in the case of shaped charges for producing an explosive-shaped projectile, called P charges.

Weitere vorteilhafte Ausgestaltungen der Erfindung ergeben sich aus den Unteransprüchen und der folgenden Beschreibung eines Ausführungsbeispiels. In der Zeichnung zeigen:

  • Figur 1 ein Geschoß im Längsschnitt,
  • Figur 2 eine vergrößerte Teilansicht einer Klemmvorrichtung am Zuganker und
  • Figur 3 eine Alternative zu Figur 2.
Further advantageous refinements of the invention result from the subclaims and the following description of an exemplary embodiment. The drawing shows:
  • 1 shows a projectile in longitudinal section,
  • Figure 2 is an enlarged partial view of a clamping device on the tie rod and
  • Figure 3 shows an alternative to Figure 2.

Zwischen einem Geschoßboden 1 und einem Geschoßkopf 2 sind zwei P-Ladungs-Wirkkörper 3 und 4 aufeinandergestapelt. Deren Mantelwandungen sind mit 5 bzw. 6 bezeichnet. Die Außendurchmesser des Geschoßbodens 1, des Geschoßkopfes 2 und der Wirkkörper 3, 4 fluchten miteinander.Between a floor 1 and a floor head 2, two P-charge active bodies 3 and 4 are stacked on top of one another. Their jacket walls are designated 5 and 6 respectively. The outer diameter of the floor 1, the projectile head 2 and the active body 3, 4 are aligned.

In jeder Mantelwandung 5, 6 sind achsparallele, durchgehende Bohrungen 7 und 8 bzw. 9 und 10 vorgesehen. Der Geschoßboden 1 weist Gewindebohrungen 11 und 12 auf. Zur Zentrierung des Geschoßbodens 1 und der Wirkkörper 3 und 4 sind am Boden 1 bzw. den Mantelwandungen 5 und 6 Stufungen 13, 14 ausgebildet. Um das fluchtende Ausrichten der Bohrungen 7, 9, 11 bzw. 8,10,12 zu erleichtern, können die Stufungen 13, 14 auch als sich über einen Teil des Umfangs erstreckende Verzahnung ausgebildet sein.Axial parallel, continuous bores 7 and 8 or 9 and 10 are provided in each jacket wall 5, 6. The floor 1 has threaded holes 11 and 12. To center the floor 1 and the active bodies 3 and 4, 5 and 6 steps 13, 14 are formed on the floor 1 and the jacket walls. In order to facilitate the aligned alignment of the bores 7, 9, 11 and 8, 10, 12, the steps 13, 14 can also be designed as toothing extending over part of the circumference.

In die Gewindebohrungen 11 und 12 sind Zuganker 15, 16 eingeschraubt, die sich durch die Bohrungen 7, 9 bzw. 8, 10 hindurch erstrecken. Die Zuganker 15, 16 ragen durch Führungsbohrungen 17, 18 eines im Geschoßkopf 2 gelagerten Ausstoßzylinders 19 und Bohrungen 20, 21 eines Bundes 22 des Geschoßkopfes 2. Sie sind mittels Spannmuttern 23, 24 am Bund 22 verspannt.Tie rods 15, 16 are screwed into the threaded bores 11 and 12 and extend through the bores 7, 9 and 8, 10, respectively. The tie rods 15, 16 project through guide bores 17, 18 of an ejection cylinder 19 mounted in the projectile head 2 and bores 20, 21 of a collar 22 of the projectile head 2. They are clamped to the collar 22 by means of clamping nuts 23, 24.

Der Ausstoßzylinder 19 ist an einem Zünder 25 des Geschoßkopfes 2 verschieblich gelagert. Zwischen dem Zünder 25 und dem Ausstoßzylinder 19 besteht ein Gasraum 26. Der Ausstoßzylinder 19 steht an der Mantelwandung 5 an.The ejection cylinder 19 is slidably mounted on an igniter 25 of the projectile head 2. There is a gas space 26 between the igniter 25 and the ejection cylinder 19. The ejection cylinder 19 is in contact with the jacket wall 5.

Am Zuganker 15 bzw. 16 ist im Bereich des Geschoßbodens 1 eine erste Sollbruchstelle 27 ausgebildet. Im Bereich der Stoßstelle zwischen den Wirkkörpern 3 und 4 ist an den Zugankern 15, 16 eine zweite Sollbruchstelle 28 ausgebildet. Eine dritte Sollbruchstelle 29 liegt nahe beim Geschoßkopf 2.A first predetermined breaking point 27 is formed on the tie rod 15 or 16 in the area of the floor 1. In the area of the joint between the active bodies 3 and 4, a second predetermined breaking point 28 is formed on the tie rods 15, 16. A third predetermined breaking point 29 is close to the projectile head 2.

Der Durchmesser des Zugankers 15, 16 ist zwischen den Sollbruchstellen 27, 28 geringfügig größer als der Durchmesser zwischen den Sollbruchstellen 28 und 29. Der Durchmesser des Zugankers 15, 16 ist zwischen den Sollbruchstellen 28 und 29 geringfügig größer als zwischen der Sollbruchstelle 29 und der Spannmutter 23 bzw. 24. In den Bohrungen 7 bis 10 sind entsprechende Anschläge 30, 31 für den Zugankerabschnitt mit dem jeweils größeren Durchmesser ausgebildet. Der Abstand zwischen dem Anschlag 30 und der Sollbruchstelle 29 ist größer als der Abstand zwischen dem Anschlag 31 und der Sollbruchstelle 28 (vgl. Figur 1).The diameter of the tie rod 15, 16 between the predetermined breaking points 27, 28 is slightly larger than the diameter between the predetermined breaking points 28 and 29. The diameter of the tie rod 15, 16 between the predetermined breaking points 28 and 29 is slightly larger than between the predetermined breaking point 29 and the clamping nut 23 and 24. In the bores 7 to 10, corresponding stops 30, 31 are formed for the tie rod section with the larger diameter in each case. The distance between the stop 30 and the predetermined breaking point 29 is larger ß than the distance between the stop 31 and the predetermined breaking point 28 (see FIG. 1).

Beim Abschuß des Geschosses nehmen die Mantelwandungen 5 und 6 die Abschußbeschleunigung auf. Die Zuganker 15, 16 übertragen die Drallbeschleunigung.When the projectile is fired, the jacket walls 5 and 6 absorb the launch acceleration. The tie rods 15, 16 transmit the swirl acceleration.

Wird der Zünder 25 gezündet, dann drückt der Ausstoßzylinder 19 auf die Mantelwandung 5 und über die Mantelwandung 6 auf den Geschoßboden 1. Dadurch reißen die Zuganker 15, 16 zunächst an den Sollbruchstellen 27. Der Geschoßboden 1 wird dadurch frei. Anschließend verschieben sich die Mantelwandungen 5, 6 auf den Zugankern 15, 16, so daß der Anschlag 31 auf den größeren Durchmesser des Zugankers 15, 16 bei den Sollbruchstellen 28 trifft. Dadurch reißen auch die Sollbruchstellen 28. Es ist jetzt der Wirkkörper 4 frei. Schließlich trifft der Anschlag 30 des Wirkkörpers 3 auf den Abschnitt größeren Durchmessers bei der Sollbruchstelle 29. Dadurch reißen die Sollbruchstellen 29, so daß nun auch der Wirkkörper 3 vom Geschoßkopf 2 frei ist.If the igniter 25 is ignited, then the ejection cylinder 19 presses on the jacket wall 5 and via the jacket wall 6 on the floor 1. As a result, the tie rods 15, 16 initially tear at the predetermined breaking points 27. The floor 1 is thereby released. Then the jacket walls 5, 6 move on the tie rods 15, 16 so that the stop 31 meets the larger diameter of the tie rod 15, 16 at the predetermined breaking points 28. As a result, the predetermined breaking points 28 also tear. The active body 4 is now free. Finally, the stop 30 of the active body 3 hits the section of larger diameter at the predetermined breaking point 29. As a result, the predetermined breaking points 29 tear, so that the active body 3 is now free of the projectile head 2.

Um zu vermeiden, daß die Teile der abgerissenen Zuganker 15,16 sich aus den Bohrungen 7, 8 bzw. 9, 10 entfernen, ist nach Figur 2 am Zuganker 15, 16 innerhalb der Bohrungen 7, 9 bzw. 8, 10 je ein O-Ring 32 gelagert, der das betreffende Zugankerteil in der Bohrung an einer Kreisringfläche 33 festklemmt, wenn dieses bis zum Anschlag 30 bzw. 31 bewegt ist.In order to prevent the parts of the torn off tie rods 15, 16 from being removed from the bores 7, 8 or 9, 10, an O is shown on the tie rod 15, 16 according to FIG Ring 32 mounted, which clamps the relevant tie rod part in the bore on an annular surface 33 when it is moved up to the stop 30 or 31.

Anstelle des O-Ringes 32 und der Kreisringfläche 33 ist beim Ausführungsbeispiel nach Figur 3 am Zuganker 15, 16 jeweils innerhalb der Bohrungen 7 bis 10 ein selbsthemmender Konus 34 ausgebildet, dem eine entsprechend konische Fläche 35 der Bohrungen 7 bis 10 zugeordnet ist. Der Konus 34 und die konische Fläche 35 ersetzen die Anschläge 30 und 31. Ist der Konus 34 in die konische Fläche 35 gezogen, dann reißt die betreffende Sollbruchstelle 28, 29. Über die selbsthemmende Wirkung des Konusses 34 bleibt das Zugankerteil in der Mantelwandung 5 bzw. 6 gehalten.Instead of the O-ring 32 and the annular surface 33 in the embodiment according to FIG. 3, a self-locking cone 34 is formed on the tie rod 15, 16 within the bores 7 to 10, to which a corresponding conical surface 35 of the bores 7 to 10 is assigned. The cone 34 and the conical surface 35 replace the stops 30 and 31. If the cone 34 is pulled into the conical surface 35, then the intended breaking point 28, 29 tears. About the self-locking effect of the cone 34, the tie rod part remains in the jacket wall 5 and 6 held.

Claims (8)

1.. A projectile having effective bodies (3, 4) which have a cylindrical jacket wall (5, 6) and are held axially stacked between a projectile base (1) and a projectile nose (2) and for the ejection of which an ejection device (19, 25) is arranged on the projectile and having at least one tie rod, characterised in that the jacket walls (5, 6) of the effective bodies themselves form the projectile case, the jacket wall (5, 6) of each effective body (3, 4) is provided with at least two axially-parallel continuous bores (7 to 10), in that fixed through the aligned bores (7, 9; 8, 10) of the jacket walls (5, 6) of the effective bodies (3, 4) are the tie rods (15, 16) which are fastened by their end to the projectile base (1) and by their other end to the projectile nose (2) and each tie rod (15, 16) has predetermined breaking points (27, 28, 29) in the region of the projectile base (1), in the region of the junction point between two effective bodies (3, 4) and in the region of the projectile nose (2).
2. A projectile according to claim 1, characterised in that the jacket walls (5, 6) have a stepping (13, 14) in the region of the junction points.
3. A projectile according to claim 2, characterised in that the stepping (13, 14) is designed as a toothing.
4. A projectile according to one of the preceding claims, characterised in that a stop (30, 31) for the tie rod (15, 16) is provided in the region of the junction points, in which respect upon the ejection the tie rod (15, 16) initially strikes against the stop (31) of the effective body (4) further from the ejection device (19) and then against the stop (30) of the effective body (3) nearer to the ejection device (19).
5. A projectile according to one of the preceding claims, characterised in that a clamping device (32, 33; 34, 35) is fashioned on the tie rod (15, 16) in the region of the junction points.
6. A projectile according to claim 5, characterised in that the clamping device consists of an O-ring (32) which is clamped to the bore (7 to 10) on a circular ring surface (33).
7. A projectile according to one of the preceding claims 1 to 5, characterised in that the clamping device consists of a cone (34) of the tie rod (15, 16) and a conical surface (35) fashioned in the bores (7 to 10).
8. A projectile according to claim 4 and 7, characterised in that the conical surface (35) together with the cone (34) forms the stop.
EP86115870A 1985-11-28 1986-11-14 Missile with multiple submissiles Expired - Lifetime EP0224154B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3542051 1985-11-28
DE19853542051 DE3542051A1 (en) 1985-11-28 1985-11-28 BULLET WITH ACTUATORS

Publications (2)

Publication Number Publication Date
EP0224154A1 EP0224154A1 (en) 1987-06-03
EP0224154B1 true EP0224154B1 (en) 1990-04-11

Family

ID=6287069

Family Applications (1)

Application Number Title Priority Date Filing Date
EP86115870A Expired - Lifetime EP0224154B1 (en) 1985-11-28 1986-11-14 Missile with multiple submissiles

Country Status (4)

Country Link
US (1) US4712482A (en)
EP (1) EP0224154B1 (en)
DE (2) DE3542051A1 (en)
NO (1) NO159750C (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3902761A1 (en) * 1989-01-31 1990-08-09 Diehl Gmbh & Co Transportation device for payloads
IT223260Z2 (en) * 1991-06-28 1995-06-21 Valsella Meccanotecnica Spa PROJECT PROVIDED WITH A PLURALITY OF EXPLOSIVE CHARGES
DE4429292C2 (en) * 1994-08-18 1998-04-09 Rheinmetall Ind Ag Swirl-stabilized carrier floor
US7168368B1 (en) * 2004-05-06 2007-01-30 The United States Of America As Represented By The Secretary Of The Navy Apparatus for expelling a payload from a warhead
DE102007056785A1 (en) * 2007-11-23 2009-05-28 Rheinmetall Waffe Munition Gmbh bullet
DE102007056786A1 (en) * 2007-11-23 2009-05-28 Rheinmetall Waffe Munition Gmbh bullet

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1325706A (en) * 1919-12-23 Projectile
DE123906C (en) *
GB249765A (en) * 1925-10-29 1926-04-01 Jan Karel Engelbert Triebart Improvements in or relating to anti-aircraft or other shells
US2798431A (en) * 1951-01-25 1957-07-09 Howard W Semon Fragmentation warhead
DE977835C (en) * 1964-09-09 Messerschmitt Boelkow Blohm Shaped charge to produce cut-like effects
DE2422142A1 (en) * 1974-05-08 1975-11-20 Dynamit Nobel Ag Projectile body closer with shear connection - has ring with shear shoulders for ensuring correct ejection of projectile content
DE2739299C2 (en) * 1977-09-01 1984-01-19 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Holder for large cluster weapon containers
DE3048206C2 (en) * 1980-12-20 1985-06-13 Diehl GmbH & Co, 8500 Nürnberg Practice floor
US4499830A (en) * 1981-06-29 1985-02-19 The United States Of America As Represented By The Secretary Of The Army High lethality warheads

Also Published As

Publication number Publication date
DE3670368D1 (en) 1990-05-17
NO159750B (en) 1988-10-24
EP0224154A1 (en) 1987-06-03
DE3542051A1 (en) 1987-06-04
US4712482A (en) 1987-12-15
NO159750C (en) 1989-02-01
NO864218D0 (en) 1986-10-22

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