EP1893936A1 - Kit d'aide a la penetration equipant une bombe, notamment anti-infrastructure, projectile penetrant equipe d'un tel kit, et procede de penetration dans une cible - Google Patents
Kit d'aide a la penetration equipant une bombe, notamment anti-infrastructure, projectile penetrant equipe d'un tel kit, et procede de penetration dans une cibleInfo
- Publication number
- EP1893936A1 EP1893936A1 EP06763727A EP06763727A EP1893936A1 EP 1893936 A1 EP1893936 A1 EP 1893936A1 EP 06763727 A EP06763727 A EP 06763727A EP 06763727 A EP06763727 A EP 06763727A EP 1893936 A1 EP1893936 A1 EP 1893936A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- bomb
- projectile
- target
- detonating
- kit
- 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- Withdrawn
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
- F42B12/04—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type
-
- 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
- F42B12/20—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
-
- 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
- F42B12/20—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
- F42B12/201—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type characterised by target class
- F42B12/204—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type characterised by target class for attacking structures, e.g. specific buildings or fortifications, ships or vehicles
-
- 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
- F42B12/62—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected parallel to the longitudinal axis of the projectile
Definitions
- Kit penetration aid equipping a bomb including anti-infrastructure, penetrating projectile equipped with such a kit, and method of penetration into a target.
- the present invention relates to a penetration aid kit equipping a bomb, including anti-infrastructure. It is particularly applicable for traversing very thick walls of non-metallic material such as concrete for example.
- the invention also relates to a penetrating projectile equipped with such a kit and a method of penetrating such a projectile into a target.
- a bomb is carried by a rocket or a guide kit.
- a rocket has essentially three parts. At the front it contains its guidance system and at the rear its engine for propulsion. Between these two elements is the military charge, in other words essentially the bomb.
- the size and weight of the rockets are fixed and their speed. It follows that the volume, weight and speed of the bomb are also frozen, regardless of the performance required. In particular, the kinetic energy can not be increased in order to obtain new performances, even more advanced.
- One solution could be to strengthen the structural integrity of the body of the bomb, for example by tripling its thickness.
- Another solution could still employ a dense material with significant diameter reduction.
- the first solution prevents in particular to make a bomb body versatile with respect to surface threats or buried.
- the second solution leads to a bomb body very expensive and actually a bomb very inefficient because the explosive mass on board is then reduced by more than half compared to a normal body of steel.
- An object of the invention is in particular to allow a bomb of relatively low structural strength to pass through increasingly thick walls or resistant.
- the invention relates to a penetration aid kit equipping a bomb, the kit comprising at least:
- a launcher tube preferably further comprises a counter-mass, the explosive charge being placed between the latter and the detonating projectile, so that the counter-mass is ejected in a direction opposite to that of the detonating projectile.
- the tubes can be attached to the bomb via a first spacer placed in front of the bomb and a second spacer placed at the rear of the bomb.
- a spacer is for example formed of a plate pierced with holes in which the launching tubes are engaged.
- the kit preferably comprises an even number of launching tubes, the detonating projectiles being ejected two by two from two diametrically opposed tubes.
- the kit comprises for example four launcher tubes.
- a launcher tube comprises for example a propellant charge activation system coupled to an external control member.
- This activation system may advantageously comprise a delay, to delay the firing of the explosive charge with respect to a signal provided by the external control member.
- a detonating projectile includes a system that determines its position within the target as a function of time and that triggers the detonation of its pyrotechnic charge at a predetermined time. For example, the system determines the position of the detonating projectile from its characteristics of the deceleration levels in the target material and its velocity at the point of impact on the target.
- the invention also relates to a penetrating projectile comprising a bomb equipped with a penetration aid kit as previously described.
- the invention furthermore relates to a method of penetration into a target of a bomb equipped with a kit as described above where:
- a detonating projectile is ejected from its launcher tube by firing its propellant charge when the bomb is at a given distance from the target;
- the main advantages of the invention are that it can be adapted to existing bombs, that it makes it possible to increase the field of arrival angle of incidence of the body of a bomb on a wall, and that it is economical.
- FIG. 1 an example of rocket structure
- FIG. 2 an exemplary possible embodiment of a projectile according to the invention equipped with a penetration aid kit
- FIG. 3 a partial view an embodiment of a kit according to the invention equipping a penetration bomb;
- FIG. 4 an exemplary embodiment of a device for activating a kit according to the invention;
- FIG. 8 an illustration of the wide field of incidence of a projectile according to the invention on a wall.
- FIG. 1 shows the structure of a rocket 1. As indicated above, it consists essentially of three parts 2, 3, 4. The front of the rocket comprises the guiding means 2 and the rear comprises the propulsion means 3. Between the two is the penetrating projectile 4, for example a military load such as a bomb. The fact that the envelope of the rocket is frozen as well as the overall mass results in the volume and the mass devoted to the penetrating projectile 4 are also fixed, to the extent that it is also not possible to reduce the allocated parts the guide means and the propulsion means. The structural mechanical strength of the penetrating body can not therefore be significantly increased. Likewise the speed of the penetrating body is fixed by the speed of the rocket 1.
- the speed of the penetrating body is fixed by the speed of the rocket 1.
- FIG. 2 shows a penetrating projectile according to the invention, more particularly a bomb 21 equipped with a penetration aid kit.
- the penetrating projectile 4 is for example arranged in a rocket 1 according to FIG. 1.
- the kit comprises launching tubes 22.
- a launching tube comprises a hyper-velocity detonating projectile which is fired near a target, before the penetrating bomb 21 reaches the latter. This detonating projectile hypervelocity is actually intended to reach the target before the arrival of the bomb 21, to penetrate and destroy by detonation within it.
- the launching tubes 22 are mechanically secured to the bomb 21.
- the kit comprises for example spacers 23.
- a spacer is for example formed of a disk, or a plate, pierced with holes in which are engaged the launching tubes. These can be attached to the spacer by means of soldering points.
- a first spacer 23 is disposed at the front of the bomb 21. It can then be screwed or welded on the front of the bomb.
- a second spacer is disposed at the rear of the bomb. It is for example pierced in the middle to engage around the body of the bomb. It can be maintained by welding points.
- the material forming the launching tubes 22 is for example stainless steel.
- the spacers 23 are for example aluminum or plastic.
- the dimensions of the launching tubes 22 and spacers 23 are in particular provided so that the assembly consisting of the bomb and the kit can take place in an operational space, for example the space provided in the rocket 1 to accommodate a penetrating projectile 4.
- the penetration aid kit represented in FIG. 2 comprises four launching tubes. It can obviously include a different number, in particular function of congestion.
- FIG 3 shows an embodiment of a penetration aid kit, more particularly it has the possible content of a launcher tube 22.
- the launcher tube is represented by a partial view in longitudinal section. The elements it contains are symbolized by the location they occupy.
- the launcher tube 22 comprises a high-velocity detonating projectile 31 and a propellant charge 32.
- the detonating projectile 31 is ejected from the tube during the activation of the propellant charge.
- the detonating projectile 31 is then ejected out of the tube 22 with a speed that is clearly greater than the speed of the latter, which is therefore clearly greater than the speed of the penetration bomb 21 which remains integral with the tube.
- a tube 22 comprises a propellant charge activation system 32 coupled to an external control member.
- this external control member can be installed in the bomb 21 or in the rocket 1.
- the launcher 22 also comprises, for example, a counter-mass 33, the propellant charge 32 being disposed between this counter-mass 33 and the detonating projectile 31.
- the detonating projectile 31 will be sent towards the front of the bomb 21 while the counter-mass 33 will be sent towards the rear of the bomb.
- the penetration aid kit comprises, for example, four tubes 22 thus equipped, the arrival of the penetrating bomb 21 on a target will be preceded by four impacts made by the four detonating projectiles 31 ejected from the tubes 22.
- detonating projectiles 31 are ejected substantially at one time but this is not mandatory. If the projectiles 31 are not all triggered at the same time, they are preferably ejected at the same time two by two, the two projectiles then ejected being symmetrical with respect to the axis of the penetrating bomb 21 to avoid imbalances. It is therefore necessary to transmit an order of release of the ejection towards the tubes 22.
- FIG. 4 is a partial sectional view of an exemplary embodiment of a device for transmitting an activation signal to a launcher tube 22.
- This activation signal comes from outside the launcher tube 22. It can be generated by the rocket 1, for example at its guide means 2. It can also be generated by the penetrating bomb 21. It is in fact that the signal is transmitted sufficiently early to activate the propellant charge 32 and eject the detonating projectile 31 before the arrival of the bomb 21 on the target. It is necessary to predict the ejection at a given distance from the target.
- the activation signal is for example transmitted by induction.
- the tube 22 comprises a first coil 41, wound on its outer surface, and a second coil 42, disposed opposite the first coil but inside the tube.
- the signal thus transmitted via the coils 41, 42 is then directed inside the tube to the means for activating the propellant charge. Possibly the signal is transmitted via a timing circuit.
- This can be particularly useful if the signal is transmitted by the rocket.
- the rocket detects a first distance to the target it ejects the penetrating projectile, that is to say the whole composed of the 21 and the kit 22, 23.
- the rocket also sends an activation signal to the launchers.
- the ejection of detonating projectiles 31 is then done after a time ⁇ t 0 defined by the timing circuit.
- the external coil is for example connected by an electric wire to the rocket via, for example, the spacers which may comprise interconnection printed circuits, the signal can then be transmitted from the spacers to the coils 41, 42 by a metal braid fixed on the tube.
- Figure 5 shows the rocket 1 in two places of its trajectory 51 to a concrete wall 52 in an x, y axis system.
- the positions relative to the ground are indicated on an x-axis.
- the y-axis represents the altitude of the rocket.
- the scales of distances and altitudes are reduced compared to the scales of representation of the rocket and the slab.
- the rocket provided with its penetrating projectile 4 is placed for launching.
- the penetrating projectile 4 is composed of the bomb 21 and its penetration aid kit 22, 23.
- the concrete wall is located at a distance xi from the starting position.
- the rocket is propelled by its propulsion means 3 located at the rear.
- the position of the rocket relative to the wall 52 is for example determined by a proximity sensor located at the front of the rocket with the guide means.
- this proximity sensor detects the distance xi-Xo, it also sends an activation signal to the launching tubes 22 which will trigger the ejection of detonating projectiles after the time ⁇ to defined above.
- FIGS. 6a to 6f illustrate the method according to the invention by presenting different phases of a penetrating projectile according to the invention in approach and through phase of the wall 52.
- These figures notably illustrate the penetration aid provided by a kit according to the invention.
- the kit comprises a system for controlling the firing of each propellant charge before the impact of the bomb 21 on a target, the wall 52 in the case of Figures 6a to 6f.
- This system can be centralized, placed for example in the safety device or firing, on a spacer 23 or decentralized in the tubes.
- FIG. 6a shows the instant of firing of the propellant charges 32 at the immediate approach of the target, in this case the wall 52.
- each detonating projectile 31 is ejected from its tube 22 with a very high speed relative to this tube. For example, if the bomb 21 moves at a speed of the order of 300 m / s, each detonating projectile 31 can exit with a relative speed of this order.
- a timer placed for example in an electronic circuit connected to the tube 22 may for example calculate a delay between the instant of ejection of the bomb body 21 of the rocket 1 and the moment of initiation of the propellant charge 32 inside the tube, l ejection moment of the bomb body being determined for example by the guide means 2 located at the front of the rocket 1.
- FIG. 6b shows the flight of the detonating projectiles 31 to the wall 52, followed by the bomb body 21.
- the detonating projectiles 31 then move towards the target with a speed much higher than the speed of the bomb 21.
- the counter-masses 33 are ejected towards the rear.
- Counterweight 33 is dimensioned so that the amount of rearward movement is substantially the same as the amount of forward motion.
- a counter-mass 33 may have a mass equivalent to that of the detonating projectile 31.
- Figure 6c shows the penetration of the detonating projectiles 31 in the wall 52, before the arrival of the bomb 21 on the wall.
- FIG. 6d shows the detonation of the detonating projectiles 31 inside the wall, preferably in the middle, creating an orifice 61 crossing, if possible, the wall 52.
- each detonating projectile comprises, for example, a system which determines its position. within the wall as a function of time and which triggers the detonation of its pyrotechnic charge at a predetermined time.
- the invention advantageously uses the fact that the concretes do not hold the tensile stress. This allows them to destructure relatively easily by a detonation of a projectile 31 inside the wall, the inner detonation creating high tensile stresses.
- An internal processor located for example in the projectile 31 can determine its moment of detonation corresponding to its most effective position inside the wall, for example in the middle thereof.
- a table is for example stored in the processor.
- This table contains the characteristics of the deceleration levels of an object penetrating into a material. It can take into account several types of materials including of course concrete and even different types of concrete. Thus knowing the initial velocity of the projectile 31 at the entrance to the wall, at the point of impact, and the deceleration curve of the material of the latter, it is possible to know the distance of penetration inside the wall. function of time and therefore its position.
- An impact intelligence module of the "caimam" type is for example used.
- FIG. 6e shows the penetration of the bomb body 21 into the orifice 61 created by the projectiles 31.
- the kit disengages itself, for example, from the bomb.
- the amount of charge carried by the projectiles 31 may be calculated to obtain an orifice adapted to the caliber of the bomb body 21, that is, to say in practice close to the caliber of the body of bomb.
- the invention thus makes it possible to considerably reduce the stresses seen by the body of the bomb during its phase of penetration into the wall, and therefore even allows a bomb of relatively low resistance. Structural mechanics to cross more and more thick or resistant walls.
- Figure 6f shows the bomb body 21 after crossing the wall 52. At this time the bomb body can for example detonate by firing of its pyrotechnic charge.
- FIG. 7 illustrates the impacts created by the detonating projectiles 31 inside the wall 52 in a case where the penetration aid kit comprises four launching tubes 22 each equipped with a detonating projectile 31.
- a first impact 71 is created by a first detonation produced by two projectiles from two diametrically opposed launchers.
- a second impact 72 is created by a second detonation produced by the projectiles from the two other launchers diametrically opposed.
- the axes of symmetry of these two impacts 71, 72 are substantially perpendicular.
- the combination of these two impacts results in a substantially circular impact 73 creating an orifice that allows the bomb 21 to pass through the wall.
- the diameter of the circular impact 73 can reach a diameter of the order of one meter.
- Figure 8 illustrates another advantage of the invention.
- the invention makes it possible to increase the angle of arrival angle range of the bomb body 21 on a wall 52.
- the orifice 81 created by the projectiles 31 in the wall 52 creates there also an input face 73 normal to the speed vector V of the body of the bomb.
- This inlet face 73 in particular avoids the ricochets of the bomb body on the wall when the angle of incidence ⁇ of its velocity vector on the wall is too low. If this angle ⁇ is nevertheless much too weak, there will nevertheless be an incidence.
- a projectile 31 which is thinner and faster than the bomb body can penetrate the wall including for low angles of incidence, the body of a bomb benefiting from the orifice created by the detonating projectiles and thereby having an enlarged incidence range.
- the invention has been described for the realization of a penetration bomb inside an infrastructure. It can, however, apply to other types of projectiles intended to penetrate into infrastructure through a thick wall.
- the invention makes it possible in particular to pass through concrete walls with a high modulus of rupture to compression, which can reach for example 50 or even 60 MPa.
- the invention has particular advantages that it adapts to any type of existing bombs, it is sufficient to equip them with the penetration aid kit to increase the penetrating power thereof.
- the invention is also economical because of the ease of adaptation of the kit without the need to develop a new type of bomb.
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)
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0506016A FR2887021B1 (fr) | 2005-06-14 | 2005-06-14 | Kit d'aide a la penetration equipant une bombe, notamment anti-infrastructure, projectile penetrant equipe d'un tel kit, et procede de penetration dans une cible |
PCT/EP2006/063233 WO2006134139A1 (fr) | 2005-06-14 | 2006-06-14 | Kit d'aide a la penetration equipant une bombe, notamment anti-infrastructure, projectile penetrant equipe d'un tel kit, et procede de penetration dans une cible |
Publications (1)
Publication Number | Publication Date |
---|---|
EP1893936A1 true EP1893936A1 (fr) | 2008-03-05 |
Family
ID=36263761
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP06763727A Withdrawn EP1893936A1 (fr) | 2005-06-14 | 2006-06-14 | Kit d'aide a la penetration equipant une bombe, notamment anti-infrastructure, projectile penetrant equipe d'un tel kit, et procede de penetration dans une cible |
Country Status (6)
Country | Link |
---|---|
US (1) | US7878121B2 (fr) |
EP (1) | EP1893936A1 (fr) |
CA (1) | CA2612155A1 (fr) |
FR (1) | FR2887021B1 (fr) |
IL (1) | IL188090A (fr) |
WO (1) | WO2006134139A1 (fr) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2917130B1 (fr) * | 2007-06-08 | 2012-11-16 | Thales Sa | Propulseur a performance amelioree |
EP2496908B1 (fr) * | 2009-11-04 | 2013-09-11 | Diehl BGT Defence GmbH & Co.KG | Bombe aérienne |
US8651066B2 (en) * | 2010-09-28 | 2014-02-18 | Bha Altair, Llc | Pulse detonation cleaning system |
Family Cites Families (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1385120A (en) * | 1918-12-12 | 1921-07-19 | Gunner A Ekman | Multiple-gun-firing apparatus or bomb |
US1417299A (en) * | 1920-05-08 | 1922-05-23 | Thomas J Cahill | Aerial bomb |
US2264906A (en) * | 1940-08-04 | 1941-12-02 | David H Roby | Aerial bomb |
US2359192A (en) * | 1942-02-17 | 1944-09-26 | Beblo John | Bomb |
US2428744A (en) * | 1945-01-24 | 1947-10-07 | Sonnenschein Louis Carl | Bomb |
FR1176966A (fr) * | 1957-05-14 | 1959-04-17 | Chimie Et Propulsion Soc | Engin auto-propulsé composite à étages de propulsion et projectiles multiples |
GB1458809A (en) * | 1957-10-24 | 1976-12-15 | Mini Defence | Missile warheads |
US3107616A (en) * | 1961-03-14 | 1963-10-22 | Charles W Boaz | Sliding door opening mechanism |
US4072107A (en) * | 1967-06-07 | 1978-02-07 | The United States Of America As Represented By The Secretary Of The Army | Missile control means |
US3948175A (en) * | 1970-02-03 | 1976-04-06 | Dynamit Nobel Aktiengesellschaft | Warhead |
US4172407A (en) * | 1978-08-25 | 1979-10-30 | General Dynamics Corporation | Submunition dispenser system |
FR2470358A1 (fr) * | 1979-11-22 | 1981-05-29 | Serat | Perfectionnements apportes aux armes lancant des projectiles |
US4372216A (en) * | 1979-12-26 | 1983-02-08 | The Boeing Company | Dispensing system for use on a carrier missile for rearward ejection of submissiles |
DE3004047C2 (de) * | 1980-02-05 | 1984-10-31 | Rheinmetall GmbH, 4000 Düsseldorf | Panzerbrechendes Geschoß |
GB2226624B (en) * | 1987-12-12 | 1991-07-03 | Thorn Emi Electronics Ltd | Projectile |
DE29507361U1 (de) * | 1995-05-08 | 1996-09-26 | Diehl GmbH & Co, 90478 Nürnberg | Submunition |
DE19534215A1 (de) * | 1995-09-15 | 1997-03-20 | Diehl Gmbh & Co | Splitterhülle eines Sekundärgeschosses eines Tandemgefechtskopfes |
AUPQ776300A0 (en) * | 2000-05-25 | 2000-08-10 | Metal Storm Limited | Missile control |
IL148919A0 (en) * | 2002-03-26 | 2003-07-31 | Rafael Armament Dev Authority | System and method for low signature launch of projectile |
AU2002950846A0 (en) * | 2002-08-16 | 2002-09-12 | Metal Storm Limited | Interception missile and method of interception |
US7017496B2 (en) * | 2002-08-29 | 2006-03-28 | Raytheon Company | Kinetic energy rod warhead with imploding charge for isotropic firing of the penetrators |
US6843179B2 (en) * | 2002-09-20 | 2005-01-18 | Lockheed Martin Corporation | Penetrator and method for using same |
-
2005
- 2005-06-14 FR FR0506016A patent/FR2887021B1/fr not_active Expired - Fee Related
-
2006
- 2006-06-14 CA CA002612155A patent/CA2612155A1/fr not_active Abandoned
- 2006-06-14 US US11/917,738 patent/US7878121B2/en not_active Expired - Fee Related
- 2006-06-14 EP EP06763727A patent/EP1893936A1/fr not_active Withdrawn
- 2006-06-14 WO PCT/EP2006/063233 patent/WO2006134139A1/fr active Application Filing
-
2007
- 2007-12-12 IL IL188090A patent/IL188090A/en not_active IP Right Cessation
Non-Patent Citations (1)
Title |
---|
See references of WO2006134139A1 * |
Also Published As
Publication number | Publication date |
---|---|
FR2887021A1 (fr) | 2006-12-15 |
WO2006134139A1 (fr) | 2006-12-21 |
FR2887021B1 (fr) | 2007-08-31 |
US20080314278A1 (en) | 2008-12-25 |
US7878121B2 (en) | 2011-02-01 |
IL188090A (en) | 2012-10-31 |
CA2612155A1 (fr) | 2006-12-21 |
IL188090A0 (en) | 2008-03-20 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP3102906B1 (fr) | Charge creuse et application pour la séparation de deux étages d'un engin aéronautique ou sa neutralisation | |
EP1766323B1 (fr) | Projectile, notamment bombe de penetration anti-infrastructure et procede de penetration d'un tel projectile a travers une paroi | |
EP0438343B1 (fr) | Munition perforante pour des cibles à haute résistance mécanique | |
FR2545923A1 (fr) | Projectile assurant le percage des blindages | |
EP0084007B1 (fr) | Bombe de pénétration à corps étagé | |
WO2006134139A1 (fr) | Kit d'aide a la penetration equipant une bombe, notamment anti-infrastructure, projectile penetrant equipe d'un tel kit, et procede de penetration dans une cible | |
FR2844348A1 (fr) | Munitions a bombe d'emploi universel et a cone de charge | |
FR2661465A1 (fr) | Dispositif d'assemblage mecanique temporaire et de separation rapide d'un objet a ejecter lie a un support. | |
FR3022619A1 (fr) | Dispositif de transfert d'impulsion et de quantite de mouvement | |
FR2771499A1 (fr) | Dispositif de declenchement de l'allumage d'un projectile anti-abri | |
FR2691794A1 (fr) | Projectile combiné contre buts blindés. | |
FR2865537A1 (fr) | Fusee pour munitions | |
EP1000312B1 (fr) | Munition de contre mesure | |
FR2673462A1 (fr) | Projectile anti-blindage. | |
FR2769975A1 (fr) | Dispositif de retenue notamment de l'allumeur arriere d'un missile | |
FR2833341A1 (fr) | Systeme d'arme d'attaque de cibles sous-marines | |
FR2775770A1 (fr) | Obus explosif, canon de projection de l'obus et procede de destruction d'un objet predetermine | |
FR2975482A1 (fr) | Tete militaire anti-infrastructure et projectile equipe d'une telle tete militaire | |
EP3136043A1 (fr) | Fusée d'ogive à percuteur | |
FR2727512A1 (fr) | Projectile anti-blindage | |
FR2817955A1 (fr) | Dispositif d'amorcage pour charge explosive et charge formee incorporant un tel dispositif d'amorcage | |
FR2859275A1 (fr) | Obus anti structures betonnees | |
FR2807156A1 (fr) | Charge pyrotechnique a fonctionnement dual | |
FR2523713A1 (fr) | Charge creuse | |
FR2657158A1 (fr) | Munition perforante pour cible a haute resistance mecanique. |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
17P | Request for examination filed |
Effective date: 20080110 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): DE ES GB IT SE |
|
DAX | Request for extension of the european patent (deleted) | ||
17Q | First examination report despatched |
Effective date: 20080403 |
|
RBV | Designated contracting states (corrected) |
Designated state(s): DE ES GB IT SE |
|
DAX | Request for extension of the european patent (deleted) | ||
APAF | Appeal reference modified |
Free format text: ORIGINAL CODE: EPIDOSCREFNE |
|
APBK | Appeal reference recorded |
Free format text: ORIGINAL CODE: EPIDOSNREFNE |
|
APBN | Date of receipt of notice of appeal recorded |
Free format text: ORIGINAL CODE: EPIDOSNNOA2E |
|
APBR | Date of receipt of statement of grounds of appeal recorded |
Free format text: ORIGINAL CODE: EPIDOSNNOA3E |
|
APBT | Appeal procedure closed |
Free format text: ORIGINAL CODE: EPIDOSNNOA9E |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION HAS BEEN WITHDRAWN |
|
18W | Application withdrawn |
Effective date: 20100805 |