EP3882563A1 - Projectile, weapon assembly and method - Google Patents

Abstract

Projectile 1 with an active agent arrangement, the active agent arrangement having a pre-charge 6 and a main charge 7, the pre-charge 6 and the main charge 7 being spaced apart along a flight direction 3 and the pre-charge 6 being arranged in the flight direction 3 in front of the main charge 7, the main charge 7 is designed as a shaped charge and the Vorladdung 6 is designed as a projectile-forming charge.

Description

The invention relates to a projectile with the features of the preamble of claim 1. The invention also relates to an active agent arrangement, in particular for the projectile, and a method for bombarding a target.

The bombardment of hardened targets, especially targets with reactive armor, is often carried out with multi-stage charges, for example with tandem shaped charges. ATGM missiles, for example, are known in the prior art.

In the case of tandem hollow charges, the time interval between the initiation of the two charges is fixed by the geometric distance, since a hollow charge (HL) needs a firmly defined distance from the target (stand-off). For an optimal effect, the time interval for this is less than 1 millisecond. During this time, protective plates of enemy reactive armor cannot leave the bullet's trajectory quickly enough, so that there is an interaction with the main hollow charge and a loss of performance.

It is an object of the present invention to provide a projectile which has an improved effect against hardened targets and / or reactive armored targets.

The object is achieved by a projectile with the features of claim 1, by an active agent arrangement with the features of claim 14 and a method for firing a reactive armored target with the features of claim 15. Preferred or advantageous embodiments of the invention emerge from the subclaims, the following description and the accompanying figures.

A projectile with an active agent arrangement is proposed. The projectile is especially designed for guns. For example, the projectile can be designed to be fired by means of a machine gun or a tank gun. In particular, the projectile forms battle tank ammunition, for example 120 mm, 130 mm or 140 mm ammunition. The projectile is designed in particular for use against heavily armored targets, targets with reactive armor and / or targets with an active protection system. The active agent arrangement is designed in particular as a tandem charge.

The active agent arrangement comprises a pre-charge and a main charge. The main charge and the subpoena are arranged spaced apart from one another in a flight direction of the projectile. The summons is arranged in the direction of flight in front of the skin charge so that when the projectile is used and / or when the projectile is fired, the summons faces the target. For example, the projectile has a point and a tail, the point being arranged in the direction of flight at the front and the tail in the direction of flight being arranged at the rear, the summons being arranged in particular in the region of the point and the main charge being arranged in the region of the stern. In particular, the pre-charge and the main charge each comprise a high-explosive, wherein the high-explosive can be chemically and / or physically identical or different.

The main charge is designed as a shaped charge. In particular, the shaped charge has a conical or hemispherical metal insert, the explosive material being arranged around the metal insert. The metal insert is also referred to in particular as a liner. The skin charge is designed, for example, to penetrate armor. The metal insert is preferably made of a malleable, high density material such as copper or uranium. The main charge is designed in particular to emit a spike from the metal insert in the event of a detonation, the main charge being arranged such that a direction of flight of the spike is aligned in the same direction as the direction of flight of the projectile. For example, the tip of the conical or hemispherical metal insert points against the direction of flight of the projectile. The main charge is specifically designed as a high-performance main charge. A special design provides that a projectile-forming main charge is used as the main charge instead of a shaped charge.

The subpoena is designed as a projectile-forming charge. A projectile-forming charge is also known as a P charge or EEP (Explosively Formed Projectile). In particular, a projectile-forming charge constitutes armor-piercing ammunition. The pre-charge designed as a projectile-forming charge is designed to send out a projectile upon and / or through a detonation of the pre-charge. The projectile is emitted in particular in the direction of flight of the projectile. The projectile emitted by the projectile-forming charge is designed, for example, as an elongated but nevertheless compact projectile, in particular like a rifle projectile. The projectile-forming charge has in particular a metal insert, the metal insert preferably being parabolic or spherical. The metal algae is specifically composed of a high-density metal, for example copper, tantalum or steel.

The shaped charge is preferably designed for ignition at a distance of less than 4 caliber lengths from the target, the projectile-forming charge preferably being designed for ignition at a distance of at least 50 caliber lengths from the target. In particular, the projectile is designed to detonate the pre-charge before the main charge, or the main charge and the pre-charge, at different times.

The invention provides a projectile with which it is possible to combat heavily armored targets effectively, for example targets that are protected by reactive armor. The proposed projectile can be fired as a tandem charge, with the reactive armor of the target being activated and neutralized by means of the projectile-forming summons and the main charge being used to penetrate the main armor. The use of a projectile-forming charge as a subpoena has the advantage that the standoff to the target can be increased. This makes it possible to place the projectile of the projectile-forming charge before an active protection system of the target can take effect. The attack with two very quickly successive threats, a fast projectile of the projectile-forming summons and the remaining ballistic projectile with the main charge, is difficult for an active protection system to fend off.

In particular, the invention is based on the idea of using a projectile-forming pre-charge and a hollow charge instead of two shaped charges as tandem charges in one projectile. This has the advantage that the pre-charge can trigger possible reactive armor independent of the vehicle, so that when Later impact of the main charge, protective bursts of the reactive armor cannot reduce the penetration performance.

Optionally, the storey has a support structure. The support structure is arranged in particular in the direction of flight between the main cargo and the summons. The support structure is designed, for example, to be screwed into and / or pinned to a housing of the projectile. The support structure can be designed as a support structure made of metal and / or plastic. The pre-charge preferably adjoins a front end of the support structure, with the main charge preferably adjoining a rear end of the support structure. In particular, one or more detonators can be arranged in the support structure and / or in the region of the support structure. The task of the support structure is, for example, to shield the main charge from a blast and / or splinter effect of the subpoena. Furthermore, the task of the support structure is to partially absorb loads and / or acceleration forces of the front projectile part that occur when the projectile is fired and to relieve the outer shell.

For example, the support structure has a cone that is open to the precharge, one tip of the cone being directed in the direction of the main charge. An elongated tube in the direction of the main charge preferably adjoins the tip of the cone. The tube is also referred to as a tubular section. In particular, another open cone can be connected to a rear end of the elongated tube, this cone being open to the main charge. In particular, the structures for forming the cone, the tube and / or the further cone are part of the support structure.

It is particularly preferred that the support structure has passage openings. The passage openings are arranged in particular on the side of the support structure facing the precharge. In particular, the passage openings are in the area of the cone that is open for the pre-charge. For example, the cone has a cone envelope, the passage openings being arranged in the cone envelope. The passage openings are preferably arranged in the circumferential direction in the surface of the cone. The passage openings are, for example, breakthroughs, through bores and / or holes. The passage openings are designed and / or arranged to divert and / or allow a detonation pressure that occurs when the precharge is detonated. In particular, the passage openings are arranged for the radial discharge of the detonation pressure. This configuration lies the consideration to protect the main charge by diverting the detonation pressure of the summons.

In particular, the projectile has a housing. The active agent arrangement is preferably arranged in the housing. For example, the support structure is screwed or pinned into the housing. The housing preferably has openings for the detonation pressure to escape in the event of a detonation of the pre-charge. In particular, the openings are arranged in the area of the support structure, especially in the area of the passage openings in the support structure. The openings are preferably arranged in the direction of rotation around the direction of flight. The openings are, for example, bores, holes and / or openings in the housing. The openings are preferably designed to be slit-shaped in the direction of flight.

In particular, the housing comprises closure elements. The closure elements are designed in particular to close the openings in the housing provided for the escape of the detonation pressure in a first state. The first state is the state before the detonation and / or the ignition of the summons. The closure elements can for example be designed as a layer of plastic, in particular fiber-reinforced plastic, over the openings. A predetermined breaking point is preferably provided between the closure elements and the housing, for example a connection between the closure elements and the housing has perforations. The closure elements are designed, fastened and / or arranged in such a way that the closure elements release the openings in the housing and / or are thrown out by the detonation pressure when the precharge detonates.

The projectile preferably has at least one detonation waveguide. The detonation wave guide is arranged, for example, in and / or in the area, also called the front section, of the pre-charge, the detonation wave guide being designed and / or arranged to shape, influence and / or a projectile shape and / or projectile speed of the projectile ejected by the pre-charge to adjust. In particular, the main charge can also have a detonation wave guide.

The projectile preferably has a target detection device. The target detection device is preferably arranged in a front region of the projectile, in particular in front of the summons, for example in the tip.

In particular, the target detection device is designed to determine a point in time of the ignition of the main charge and / or precharge and / or the target detection device is designed to ignite the main charge and / or the precharge and / or initiate their ignition, for example together with an ignition device. In particular, the target detection device is designed to initiate the precharge for ignition at a distance of at least 50 caliber lengths.

In particular, the target detection device is designed to initiate the main charge for ignition at a distance of less than four caliber lengths. The target detection device comprises, for example, a radar-based sensor system and / or a radar-based sensor system.

The projectile comprises in particular an ignition device, the ignition device being designed as a central ignition device. The central ignition device is arranged between the main charge and the pre-charge. The central ignition device is designed, for example, as a mechanical, electromechanical or electrical igniter. The central ignition device is designed to ignite the pre-charge and the main charge, in particular to ignite them with a time delay, in particular to ignite the main charge with a delay compared to the pre-charge. For example, the central ignition device has a flyer which is designed to trigger a rear booster of the skin charge for ignition.

One embodiment of the invention provides that the projectile has an ignition device, the ignition device having a first and a second igniter. The first igniter is designed to ignite the pre-charge, the second igniter being designed to ignite the main charge. The first and second detonators are connected by means of a communication line, the communication line forming, for example, a wire or an electrical line. An ignition signal can be transmitted between the first and second and / or vice versa by means of the communication line. The ignition signal is, for example, a current and / or voltage pulse.

Another embodiment of the invention provides that the projectile has an ignition device, the ignition device having an ignition controller, a first and a second igniter. The first igniter is designed to ignite the pre-charge, the second igniter being designed to ignite the main charge.

The first and the second igniter are each connected to the ignition device. The ignition device is designed to ignite the first igniter and the second igniter. The ignition control is designed in particular as an electronic control and comprises, for example, a processor and / or microchip. The ignition control is preferably coupled in terms of data technology and / or connected to the target detection device, the ignition control being designed to determine an ignition time for the first and / or second igniter.

The projectile preferably comprises a pyrotechnic separation system. The pyrotechnic separation system is arranged in particular between the main charge and the pre-charge, especially in the area of the support structure. The separation system is designed to separate the projectile into at least, preferably exactly, two parts based on a pyrotechnic detonation, one part comprising the pre-charge and one part the main charge.

The separation system is, for example, designed in the shape of a ring. In particular, the separation system forms a ring, in particular a ring section of the housing and / or around the housing. The separation system has a plurality of ignition points, the ignition points being designed in particular for pyrotechnic separation of the projectile into at least two parts. The ignition points are arranged in particular in a direction of rotation around the direction of flight of the projectile.

The projectile particularly preferably has an ogive head, the target detection device, the summons and / or the main charge being arranged entirely or partially in the ogive head.

Another subject matter of the invention is an active agent arrangement. The active agent arrangement is designed in particular for and / or as in the previously described projectile. The active agent arrangement specifically forms a tandem charge. The active agent arrangement comprises a pre-charge and a main charge. The subpoena is designed as a projectile-forming charge. The main charge is designed as a shaped charge. Alternatively, the main charge can be designed as a projectile-forming charge.

Another object of the invention is a method for bombarding a target, in particular an actively and / or reactively armored target. In particular, the method envisages bombarding the target with the one previously described Projectile and / or with the previously described active agent arrangement. The projectile is fired at and / or in the direction of the target. The projectile has a direction of flight. The method provides that a pre-charge designed as a projectile-forming charge is triggered and / or ignited, a projectile emerging therefrom triggering and / or neutralizing reactive armor of the target. The triggering and / or ignition takes place in particular in a standoff of at least 50 caliber lengths. According to the method, the main charge is triggered, in particular with a time delay, the ignited and / or triggered main charge penetrating a main armor of the target.

Figur 1

eine Schnittansicht eines Geschossausschnitts;

Figur 2

schematische Ansicht eines Ausführungsbeispiels einer Vorladung;

Figur 3

schematische Ansicht eines weiteren Ausführungsbeispiels einer Vorladung;

Figur 4

schematisches Ausführungsbeispiel eines Geschosses;

Figur 5

Detailausschnitt des Geschosses aus Figur 4;

Figur 6

Detailausschnitt eines Geschosses mit Öffnungen;

Figur 7

Detailausschnitt eines Geschosses mit Durchlassöffnungen;

Figur 8

schematisches Ausführungsbeispiels eines 130 mm Geschosses;

Figur 9

Geschoss aus Figur 8 nach einem Abschuss;

Figuren 10, 11 und 12

Ausführungsbeispiele von Zündeinrichtungen;

Further features, effects and advantages of the invention emerge from the following description of a preferred exemplary embodiment of the invention and the attached figures. Show:

Figure 1

a sectional view of a projectile detail;

Figure 2

schematic view of an embodiment of a subpoena;

Figure 3

schematic view of a further embodiment of a subpoena;

Figure 4

schematic embodiment of a projectile;

Figure 5

Detail of the floor Figure 4 ;

Figure 6

Detail of a floor with openings;

Figure 7

Detail of a floor with passage openings;

Figure 8

schematic embodiment of a 130 mm projectile;

Figure 9

Bullet off Figure 8 after a kill;

Figures 10, 11 and 12

Embodiments of ignition devices;

Figure 1 shows schematically an embodiment of a detail of a projectile 1 in a sectional view. The projectile 1 comprises a housing 2, the housing 2 being designed as a continuous casing. In the section shown, the housing 2 is designed as a metallic hollow cylinder. The projectile 1 can be shot at a target by means of a barrel weapon. The projectile 1 follows a flight path, with a tangential vector on the flight path being able to characterize the flight speed. In use, the projectile 1 flies along a flight direction 3. A front section 4 and a rear section, for example rear 5, of the projectile 1 can be defined by means of the flight direction 3.

A pre-charge 6 is arranged in the front section 4 and a main charge 7 is arranged in the rear section 5. A support structure 8 is arranged between the pre-charge 6 and the main charge 7. The pre-charge 6, the support structure 8 and the main charge 7 are arranged within the housing 2.

The summons 6 is designed as a projectile-forming charge. The pre-charge 6 is arranged in such a way that if the pre-charge 6 detonates, the projectile produced is ejected in the direction of flight 3, that is to say forwards. For example, the precharge 6 has a parabolic liner 9 for this purpose, the parabola being open towards the front. By igniting the summons 6, the armored target is first hit by the separate projectile, so that its active armor is triggered. Until the main charge 7 hits and / or is triggered, this active armor can leave the trajectory of the projectile 1.

The main charge 7 is designed as a shaped charge. In particular, the main charge 7 forms a high-power charge. The main charge 7 is arranged in such a way that an ejected sting is ejected when the main charge 7 detonates in the direction of the target, that is to say the direction of flight 3. For example, the main charge 7 has a conical liner, the cone being open in the direction of flight.

The support structure 8 has two cone sections 10a, b, the cone section 10a being open towards the precharge 6 and the cone 10b being open towards the main charge 7. The cones, in particular the cone tips, are connected by means of a tubular section 11. The support structure 8 has the task of supporting the projectile 1, but also the main charge 7 before the detonation and the Detonation pressure of the summons 6 to protect. For this purpose, passage openings 12a are arranged in the lateral surface of the cone 10a, which conduct a detonation pressure during the detonation of the pre-charge 6 into an area between the tubular section 11 and the housing 2, so that the detonation pressure cannot fully affect the main charge. The conical surface of the cone 10b has no passage openings 12a, so that the detonation pressure diverted to the housing cannot penetrate the main charge 7. In the housing 2, in the area of the tubular section 11 of the support structure 8, openings 12b are provided, these being slit-shaped and diverting the detonation pressure of the precharge 6 radially from the projectile 1.

Figure 2 shows a section of an exemplary embodiment of a pre-charge 6. The pre-charge 6 is designed, for example, as a 120 mm P-charge. The summons 6 has a spherical or parabolic liner 9, which is surrounded by an explosive substance. The pre-charge also has a detonation waveguide 13. The detonation waveguide 13 is designed to optimize and / or improve the projectile shape and the projectile speed. The detonation waveguide 13 is designed to generate an elongated but compact projectile at a very high speed, in particular in order to avoid low angles of attack when interacting with the target. For the 120 mm charge, the detonation wave guide 13 is designed as an equally disgraceful trapezoid, the trapezoid expanding in the direction of flight.

Figure 3 shows an embodiment of a pre-charge 6, this pre-charge 6 being designed as a 50 mm P-charge. Contrary to the exemplary embodiment, this subpoena has ended Figure 2 a detonation wave guide 13, which is not cut off like a trapezoid in the direction of the support structure 8, but converges to a point against the direction of flight.

Figure 4 shows a schematic representation of a 120 mm ammunition as a tandem concept 14 with the projectile 1. The dimension and / or geometry is, for example, similar to 120 HE multi-purpose projectiles with an ogive head 15. The projectile 1 can be fired at a target by means of a propellant charge 20. By igniting the propellant charge 20, the projectile 1 is actually fired as a warhead.

The floor 1 from Figure 4 is available as a detail in Figure 5 shown. A target detection device 16 is arranged in the ogive head 15. The target detection device 16 is designed as a radar device in order to detect the target and / or to determine a distance to the target. For example, an ignition controller is designed to determine an ignition time based on the interval and / or to initiate the ignition of the pre-charge 6 and / or main charge 7. Behind the target detection device 16 sits the summons 6, which is designed as a projectile-forming charge. The summons 6 is designed as an 80 mm caliber. The support structure 8 adjoins the precharge 6, an ignition device 17 being arranged in the region of the support structure 8. The ignition device 17 comprises a first igniter 18a and a second igniter 18b. The first igniter 18a forms an ignition chain in the direction of the pre-charge 6 for igniting the pre-charge 6. The second igniter 18b comprises a flyer which is designed to trigger the booster 19 or the main charge 7.

Figure 6 shows a section of a projectile 1 in the area between the main charge 7 and the pre-charge 6. The casing or housing 2 is designed as a hollow cylinder in this area. In the area between the pre-charge 6 and the main charge 7, openings 12b for discharging a detonation pressure of the pre-charge 6 are arranged. The openings 12b are arranged around the hollow cylinder in the direction of rotation and are designed as slots in the direction of flight 3.

Figure 7 shows the same section as in Figure 5 shown, the housing 2 being shown transparent here, so that the support structure 8 and in particular the tubular section 11 and the conical section 10a are visible. In the cone surface of the cone 10a, passage openings 12a are made, which are arranged in the circumferential direction and guide a detonation pressure arising during the detonation of the precharge 6 into an area between the tubular section 11 and the housing 2. The detonation pressure is released from this area via the openings 12b.

Figure 8 shows an example of an ammunition concept in 130 caliber.In contrast to the 120 mm caliber, in which the projectile 1 flies in one piece to the detonation point, the 130 mm variant provides for a separation of the projectile 1 before the detonation of the subpoena 6 by sufficient distance to create between the impact of the projectile of the summons 6 and the main charge 7. The ammunition concept sees one Propellant charge case 19 in which a propellant charge 20 is arranged. By igniting the propellant charge 20, the projectile 1 is ejected and shot at the target.

Figure 9 shows the fired floor 1 Figure 7 . A radar device is arranged as the target detection device 16 in the tip of the projectile 1. For reasons of radiation permeability, this part is made of back-foamed laminate material. Behind it sits the summons 6, here an 80 mm summons, which is secured from behind by a screwed-in support cage 21. A free space between stiffening ribs of the support body 8 is used to position and accommodate the ignition device. The front projectile part 22 is fired or the front projectile part 22 is separated from the rear projectile part 23 by means of a separating unit 24. The separating unit 24 is ring-shaped and comprises four symmetrically distributed ignition points. By igniting the ignition points, the inner ring is pushed out of the device like a piston against the front edge of the rear projectile casing until the outer casing of the front projectile part 22 tears open at a defined separation point behind the connection point of the casing. Subsequently, the projectile parts 22, 23 are guided away from one another and accelerated by the ejection movement of the ring over the circumference of the floor height until the projectile 1 divides.

Figure 10 shows an embodiment of an ignition device 17 for the pre-charge 6 and the main charge 7. In order to save as much installation space as possible, the ignition device 17 is placed between the two charges 6, 7. This essentially corresponds to a basic idea of the projectile design of separating the two charges spatially from one another as far as possible so that there is as little interaction as possible when the charges detonate. This is particularly important in order, on the one hand, not to destroy the stern part of the main charge if the subpoena detonates and, on the other hand, to ensure the flight stability of the remaining floor. To initiate the ignition, the ignition device 17 is designed to initiate ignition via an ignition signal that is generated, for example, by a proximity sensor. In the event of a flyby of the target or a malfunction of the proximity detonator, an impact switch is integrated in the detonator itself, which initiates ignition in the event of a mechanical impact.

The ignition device 17 must ignite with a time delay for the charges 6, 7, the initiation taking place via a single central detonator. In the concept shown here, the pre-charge 6 is ignited via a classic ignition chain 25. The main charge 7 in the rear area is initiated via a booster 26, which is activated by a shock coupling of a flyer element 27. With the help of the flyer 27, the shaped charge can be placed maximally in the rear area, so that no activating element is necessary behind the shaped charge.

Figure 11 shows a further embodiment of an ignition device 17. The ignition device 17 has two independent mechanical igniters 18a and 18b. The igniter 18a is designed to initiate the pre-charge 6 and the igniter 18b is designed to initiate the main charge 7. The two detonators 18a, b are connected by means of a communication line 33, through which an ignition signal can be transmitted. For example, an interest signal for initiating the igniter 18a is forwarded to the igniter 18b via the communication line 28 for ignition.

Figure 12 shows a third exemplary embodiment of an ignition device 17. The ignition device 17 has two igniters 18 a, b and an ignition controller 34. The ignition controller 34 is designed as a fuse intelligence. The two detonators 18a, b can be placed independently of the ignition controller 29. The ignition control 29 is connected to the igniter 18a, b for initiating the ignition. In particular, the ignition control 29 can be designed to ignite the igniters 18a, b with a time delay.

List of reference symbols

1

bullet

2

casing

3

Flight direction

4th

Front section

5

Rear

6th

Subpoena

7th

Main charge

8th

Support structure

9

Liner

10a, b

Cone section

10

Tubular section

12a

Passage opening

12b

opening

13th

Detonation wave guide

14th

Tandem concept ammunition

15th

Ogive head

16

Target detection device

17th

Ignition device

18a, b

Detonator

19th

booster

20th

Propellant charge

21

Support cage

22nd

Front story part

23

Rear floor section

24

Separator

25th

Ignition chain

26th

booster

27

Flyer

28

Communication line

29

Ignition control

Claims (15)

Projectile (1) with an active agent arrangement,
wherein the active agent arrangement has a pre-charge (6) and a main charge (7),
wherein the pre-charge (6) and the main charge (7) are spaced apart along a direction of flight (3) and the pre-charge (6) is arranged in front of the main charge (7) in the direction of flight (3),
characterized,
that the main charge (7) is designed as a shaped charge and the Vorladdung (6) is designed as a projectile-forming charge. Projectile (1) according to claim 1,
characterized by a support structure (9), the support structure (8) spacing the main charge (7) and the pre-charge (6) apart in the direction of flight (3). Projectile (1) according to claim 2,
characterized,
that the support structure (8) has passage openings (12a) at an end facing the pre-charge (6) for the escape of detonation pressure in the event of a detonation of the pre-charge (6). Projectile (1) according to one of the preceding claims,
characterized by a housing (2),
wherein the active agent arrangement is arranged in the housing (2),
wherein the housing (2) in a region between the main charge (7) and the pre-charge (6) has openings (12b) for the radial escape of a detonation pressure in the event of a detonation of the pre-charge (6). Projectile (1) according to claim 4,
characterized,
that the housing (2) has closure elements, the closure elements being designed and / or arranged to close the openings (12b) in a first state before the detonation of the pre-charge (6) and in a second state after the detonation of the pre-charge (6 ) are removed from the openings (12b) by a detonation pressure of the detonation of the pre-charge (6). Projectile (1) according to one of the preceding claims,
characterized,
that the pre-charge has a detonation waveguide (13) for setting a projectile shape and / or a projectile speed. Projectile (1) according to one of the preceding claims,
characterized by a target detection device (16), in particular for communication with an ignition device (17). Projectile (1) according to one of the preceding claims,
characterized by an ignition device (17),
wherein the ignition device (17) is designed as a central ignition device (17) between the main charge (7) and the pre-charge (6). Projectile (1) according to one of Claims 1 to 7,
characterized by an ignition device (17),
wherein the ignition device (17) has a first igniter (18a) for the pre-charge (6) and a second igniter (18b) for the main charge (7), the first igniter (18a) and the second igniter (18b) by means of a communication line (28) are connected to transmit an ignition signal. Projectile (1) according to one of Claims 1 to 7,
characterized by an ignition device (17),
wherein the ignition device (17) has an ignition control (29), a first igniter (18a) for the pre-charge (6) and a second igniter (18b) for the main charge (7),
wherein the ignition control (29) is connected to the first igniter (18a) for igniting the pre-charge (6) and to the second igniter (18b) for igniting the main charge (7). Projectile (1) according to one of the preceding claims,
characterized by a pyrotechnic separation system (24) between the main charge (7) and the pre-charge (6). Projectile (1) according to claim 11,
characterized,
that the pyrotechnic separation system (24) is designed as a ring and has ignition points distributed in the direction of rotation. Projectile (1) according to one of the preceding claims,
characterized by an ogive head (15),
wherein the active agent arrangement is arranged in the ogive head (15). Active agent arrangement for a projectile (1), in particular according to one of the preceding claims,
characterized,
that the active agent arrangement has a projectile-forming precharge (6) and has a shaped charge as the main charge (7). Procedure for bombarding a reactive armored target,
wherein a projectile (1) according to one of claims 1 to 13 is fired in the direction of and / or at the target,
the projectile-forming summons (6) being triggered to activate and / or neutralize reactive armor on the target,
wherein the main charge (7) is triggered to penetrate main armor of the target.

Images