EP2475952A1 - Charge antimissile a barreaux deployables par restitution d'energie et procede d'activation d'une telle charge - Google Patents
Charge antimissile a barreaux deployables par restitution d'energie et procede d'activation d'une telle chargeInfo
- Publication number
- EP2475952A1 EP2475952A1 EP10771683A EP10771683A EP2475952A1 EP 2475952 A1 EP2475952 A1 EP 2475952A1 EP 10771683 A EP10771683 A EP 10771683A EP 10771683 A EP10771683 A EP 10771683A EP 2475952 A1 EP2475952 A1 EP 2475952A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- sectors
- load
- energy
- bars
- activation
- 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.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/56—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing discrete solid bodies
- F42B12/58—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles
- F42B12/60—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected radially
Definitions
- FIG. 1a shows an example of a state-of-the-art anti-ballistic missile load also designated by the acronym ATBM for "Anti Tactical Ballistic Missile" in the English language.
- the load of Figure 1 has essentially a bundle 10 of bars 12, generally made of tungsten, about a longitudinal axis XX 'of the load.
- the bundle 10 is surrounded by a certain number of explosive sectors E1, E2,... E1, ..
- n is equal to 7.
- FIGS. 1b and 1c show the operation of the ATBM load of FIG. 1a in a so-called directed effect mode of use.
- a target C for example a ballistic missile, moving along the axis ZZ '
- a number of explosive sectors of the ATBM load on the side of the target C are expelled or remote from the bundle 10 so as to facilitate the deployment of the bars 12 in the direction of the target (see Figure 1 b).
- at least one explosive sector of the charge opposite the target C is initiated (shaded area E2 in FIG. 1c) to generate a deployment of the bars around an axis MM 'directed from the load towards the target (see Figure 1c).
- the explosive sectors can be replaced by energetic materials with energy rendering less violent than the detonation (deflagration or combustion).
- FIG. 2a shows another example of ATBM load of the state of the art used in the axisymmetric operating mode shown in FIG. 2b.
- the ATBM load of FIG. 2a essentially comprises a bundle 20 of tungsten bars 12 and, in a central sector of the bundle housed in the middle of the bundle, an energetic material 14 intended to deploy the bars.
- the ATBM load of FIG. 2a is intended to be activated in the so-called axisymmetric mode.
- the activation of the charge consists in initiating the energetic material 14 of the central sector.
- the energy rendering of the central sector during the activation of the energy material 14 has the effect of the axisymmetric deployment of the bars 12 around the axis XX 'of the ATBM load and, consequently, at least a portion of the bars 12 of the fagot 10 is directed towards the target C to be destroyed. It seeks to remove the central energy sector of the bundle of bars while maintaining an axisymmetric mode of operation of the load.
- the directed effect mode is also retained.
- the invention proposes an ATBM load, of longitudinal axis XX ', intended to destroy a target C in motion, the load comprising:
- the bars of the bundle are embedded in an elastic material configured to absorb by compression of said elastic material part of the energy generated by the activation of at least one of the energetic sectors and partially restore to the surrounding environment in part the portion of energy absorbed during compression is relaxed, and in particular in the form of kinetic energy transmitted to the bars by the elastic material.
- the elastic material is chosen from rubber, polyurethane and silicone elastomer materials.
- the invention also relates to a method for activating the ATBM charge according to the invention, with a longitudinal axis XX ', intended to destroy a target C in motion along an axis ZZ', the charge comprising:
- a number of energetic sectors smaller than the number of energetic sectors surrounding the bundle are activated, propelling all the bars towards the target.
- all energy sectors surrounding the bundle are activated in a synchronized manner to provide mechanical energy compression of the bundle restored, at least partially, in the form of kinetic energy transmitted to the bars by the elastic material.
- the energy generated by the simultaneous explosion of the set of energy sectors is absorbed at least partially by the elastic material which is compressed.
- the energy stored in the elastic material is then restored, during its expansion dispersing the bars of the bundle axisymétriquement.
- the invention provides a mode of operation of the ATBM load different modes of the state of the art.
- This new mode of operation allows to obtain the mode of axisymmetric deployment of the bars without the reaction of an energetic material in a central sector of the bundle, but resorting to the synchronized action of all energy sectors surrounding the bundle.
- This configuration and method for activating the ATBM load according to the invention assumes that the definition of the load and in particular of the bundle is adapted by embedding the bars in an energy absorption matrix made of a compressible elastic material. as well as the appropriate choice of energy material (explosive detonating explosive, explosive explosive)
- FIG. 1a shows an example of anti-ballistic load with bars of the state of the art
- FIGS. 1b and 1c already described, show the operation of the ATBM load of FIG. 1a in a so-called directed effect mode of use;
- FIG. 2a shows another example of ATBM load of the state of the art
- FIG. 2b shows the operation of the load of FIG. 2a in the axisymmetric mode
- FIG. 3a shows an example of an ATBM load according to the invention
- FIGS. 3b and 3c show the activation method, according to the invention, of the ATBM load of FIG. 3a according to an axisymmetric mode.
- FIG. 3a shows an example of an ATBM load according to the invention, of longitudinal axis XX ', comprising a bundle 30 of bars 12, for example made of tungsten, embedded in a compressible elastic material 34.
- the bundle 30 is surrounded on its entire periphery with a set of energetic sectors E1, E2, .. Ei, ... En.
- the elastic material 34 may for example be chosen from rubber-type materials, of the polyurethane type, for example a polyurethane of commercial designation Ureflex or Eladip, or a silicone elastomer. These materials ensure their mission thanks to their elastic properties.
- An activation device not shown in the figures, is configured to perform the activation of the ATBM load.
- the target C is mainly a ballistic missile moving at a very high speed along the axis ZZ '.
- the device for activating the ATBM load notably comprises electronic modules configured for the detection of the target and the activation of the ATBM load. It is the on-board electronic intelligence that will determine the operating mode to be activated according to the respective position of the ATBM load relative to its target, either in the directed effect mode or in axisymmetric mode.
- FIG. 3a the ATBM charge activation method of FIG. 3a is described in detail using FIGS. 3b and 3c in an axisymmetric mode.
- a ground station detects a ballistic missile
- the ATBM load is carried by its self-steering module to the ballistic missile to be destroyed (target C).
- an onboard activation device for example a proximity fuse, starts the process of activating the ATBM charge which consists of synchronously initiating the explosion of all the energy sectors E1, E2, .. Ei, ... En, around the fagot 30.
- the simultaneous explosion of all energy sectors surrounding the bundle 30 produces, in a first phase, the compression of the elastic material 30 by compression acoustic waves F exerted on the periphery of the bundle 30.
- the bars are reproach each other but remain protected by the elastic material in which they are embedded.
- the elastic material 34 In a second phase, when the acoustic compression waves on the bundle produced by the synchronized explosion of the energy sectors together disappear, the elastic material 34, while suddenly relaxing, partially restores to the surrounding medium this energy absorbed during compression and in particular in the form of kinetic energy transmitted to the bars by the elastic material.
- the bars unfold sharply axisymmetrically away from the longitudinal axis XX '.
- the ATBM charge according to the invention, can also be activated in a so-called directed mode of use whose principle is represented in FIGS. 1a, 1b and 1c.
- the presence of the absorption matrix is also beneficial by the protection it provides on the bars with respect to the effect the reaction of the activated energy sector or sectors.
- the presence of the absorption matrix improves the deployment of the bars.
- the advantage of the ATBM load according to the invention is that it no longer carries a central energy sector 14, while fully ensuring its objective of axisymmetric deployment on demand.
- Another advantage of the ATMB load according to the invention is that, with the same charge architecture, the two modes of activation can be used, namely the effect mode directed by the activation of a limited number of energy sectors. or the axisymmetric mode, by the activation of all the energy sectors associated with the presence of an absorber / energy recovery material.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Vibration Dampers (AREA)
- Processes Of Treating Macromolecular Substances (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0904344A FR2950137B1 (fr) | 2009-09-11 | 2009-09-11 | Charge antimissile a barreaux deployables par restitution d'energie et procede d'activation d'une telle charge |
PCT/EP2010/063317 WO2011029905A1 (fr) | 2009-09-11 | 2010-09-10 | Charge antimissile a barreaux deployables par restitution d'energie et procede d'activation d'une telle charge |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2475952A1 true EP2475952A1 (fr) | 2012-07-18 |
EP2475952B1 EP2475952B1 (fr) | 2013-07-17 |
Family
ID=42102301
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP10771683.9A Not-in-force EP2475952B1 (fr) | 2009-09-11 | 2010-09-10 | Charge antimissile a barreaux deployables par restitution d'energie et procede d'activation d'une telle charge |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP2475952B1 (fr) |
ES (1) | ES2435767T3 (fr) |
FR (1) | FR2950137B1 (fr) |
WO (1) | WO2011029905A1 (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2017046792A1 (fr) * | 2015-09-17 | 2017-03-23 | Israel Aerospace Industries Ltd. | Système, procédé et programme informatique pour la synchronisation de l'amorçage de l'ogive d'un missile d'interception |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6910423B2 (en) * | 2001-08-23 | 2005-06-28 | Raytheon Company | Kinetic energy rod warhead with lower deployment angles |
US7017496B2 (en) * | 2002-08-29 | 2006-03-28 | Raytheon Company | Kinetic energy rod warhead with imploding charge for isotropic firing of the penetrators |
-
2009
- 2009-09-11 FR FR0904344A patent/FR2950137B1/fr not_active Expired - Fee Related
-
2010
- 2010-09-10 ES ES10771683T patent/ES2435767T3/es active Active
- 2010-09-10 WO PCT/EP2010/063317 patent/WO2011029905A1/fr active Application Filing
- 2010-09-10 EP EP10771683.9A patent/EP2475952B1/fr not_active Not-in-force
Non-Patent Citations (1)
Title |
---|
See references of WO2011029905A1 * |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2017046792A1 (fr) * | 2015-09-17 | 2017-03-23 | Israel Aerospace Industries Ltd. | Système, procédé et programme informatique pour la synchronisation de l'amorçage de l'ogive d'un missile d'interception |
Also Published As
Publication number | Publication date |
---|---|
FR2950137B1 (fr) | 2016-08-19 |
EP2475952B1 (fr) | 2013-07-17 |
FR2950137A1 (fr) | 2011-03-18 |
WO2011029905A1 (fr) | 2011-03-17 |
ES2435767T3 (es) | 2013-12-23 |
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