Electromagnetic mobile active system

1. An electromagnetic mobile active system for fitting in a missile, the system comprising:

a detonation-operated magnetic field compressor comprising:

at least one stator coil;

at least one armature casing, which is at least partially surrounded by the stator coil and is spaced a radial distance from it; and

at least one explosive charge, which is embedded in the armature casing;

at least one power source;

a trigger system for detonation of the explosive charge, the trigger system being controllable by a pulse of current from the power source, depending on a distance signal corresponding to a distance between the missile and a target; and

at least one directional antenna for directional radiation of electrical energy generated within the stator coil due to a rapid change of a magnetic field build up in the stator coil caused by the detonation of the explosive charge,

wherein the stator coil has a high ductility to maintain mechanical integrity of the stator coil for as long as possible during the detonation of the explosive charge and subsequent expansion.

2. The active system according to claim 1 , wherein:

the stator coil comprises at least one winding;

the stator coil comprises copper, gold, aluminum, or another material that has a high electrical conductivity and mechanical properties to preserve current conduction between the stator coil and the armature casing for as long as possible during the detonation; and/or

the armature casing comprises depressions, notches, or other structure for controlled disintegration of the armature casing.

3. The active system according to claim 1 , wherein the stator coil comprises a single-layer or multi-layer winding and a spacing of the windings of the stator coil increases at least partially in a direction of a front of the active system.

4. The active system according to claim 1 , wherein the power source comprises a Marx generator, capacitor banks, a dielectric generator, and/or a ferroelectric generator.

5. The active system according to claim 1 , wherein the explosive charge comprises a detonator and has an explosive mixture on a basis of HMX, TKX-50, CL-20, RDX, FOX-7, TATB, PETN, and/or TNT with a high detonation velocity.

6. The active system according to claim 1 , comprising at least one switching device designed to transmit electrical energy generated by the detonation in the stator coil to the directional antenna.

7. The active system according to claim 1 , wherein the distance signal can be activated based on a predetermined distance of the active system from the target.

8. The active system according to claim 7 , wherein the predetermined distance between the active system and the target is between 5 and 100 meters.

9. The active system according to claim 1 , comprising at least one deployment device designed to deliver an electromagnetic pulse generated by the detonation of the explosive charge into a target directly or over distances of up to 5 meters by conducting contact or spark discharge.

10. The active system according to claim 1 :

wherein the explosive charge is arranged in a form of a hollow charge and/or configured to generate a blasting effect and/or a fragmenting effect; and/or

the active system comprising an electrically insulated casing comprising a magnetized and/or magnetizable material.

11. An active system arrangement having at least two active systems according to claim 1 , wherein effects of the at least two active systems can be instigated simultaneously for a cumulative effect or can be triggered shortly one after another for a multiple effect.

12. A missile having at least one active system according to claim 1 .

13. A method for generating a scalable electromagnetic effect at a target, the method comprising:

providing an electromagnetic mobile active system for fitting in a missile, the electromagnetic mobile active system comprising:

a detonation-operated magnetic field compressor comprising:

at least one stator coil;

at least one armature casing, which is at least partially surrounded by the stator coil and is spaced a radial distance from it; and

at least one explosive charge, which is embedded in the armature casing;

at least one power source;

a trigger system for detonation of the explosive charge, the trigger system being controllable by a pulse of current from the power source, depending on a distance signal corresponding to a distance between the missile and the target; and

at least one directional antenna for directional radiation of electrical energy generated within the stator coil due to a rapid change of a magnetic field build up in the stator coil caused by the detonation of the explosive charge,

wherein the stator coil has a high ductility to maintain mechanical integrity of the stator coil for as long as possible during the detonation of the explosive charge; and

triggering the trigger system using the power source;

detonating the at least one explosive charge based on a predetermined distance of the active system from the target; and

generating an electromagnetic effect from detonating the at least one explosive charge;

wherein an amount of the at least one explosive charge detonated is preselected based on the target to be hit.

14. The method according to claim 13 , comprising subsequently firing a volley of shots by at least one anti-tank missile and/or multi-role missile.

15. An electromagnetic mobile active system for fitting in a missile, the system comprising:

a detonation-operated magnetic field compressor comprising:

at least one stator coil;

at least one armature casing, which is at least partially surrounded by the stator coil and is spaced a radial distance from it; and

at least one explosive charge, which is embedded in the armature casing, wherein the explosive charge is arranged in a form of a hollow charge and/or configured to generate a blasting effect and/or a fragmenting effect;

at least one power source;

a trigger system for detonation of the explosive charge, the trigger system being controllable by a pulse of current from the power source, depending on a distance signal corresponding to a distance between the missile and a target;

at least one directional antenna for directional radiation of electrical energy generated by the detonation of the explosive charge; and

an electrically insulated casing comprising a magnetized and/or magnetizable material.

16. The active system according to claim 15 , wherein the stator coil has a high ductility to maintain mechanical integrity of the stator coil for as long as possible during the detonation of the explosive charge and subsequent expansion.

17. The active system according to claim 15 , wherein the distance signal is activated based on a predetermined distance of the active system from a target.

18. The active system according to claim 15 , wherein:

the stator coil comprises at least one winding;

the stator coil comprises copper, gold, aluminum or another material that has a high electrical conductivity and mechanical properties to preserve current conduction between the stator coil and the armature casing for as long as possible during the detonation; and/or

the armature casing comprises depressions, notches, or other structure for controlled disintegration of the armature casing.

19. The active system according to claim 15 , wherein the stator coil comprises a single-layer or multi-layer winding and a spacing of the windings of the stator coil increases at least partially in a direction of a front of the active system.

20. The active system according to claim 15 , comprising at least one switching device designed to transmit electrical energy generated by the detonation in the stator coil to the directional antenna.