EP3001135B1 - Missile launcher - Google Patents

Missile launcher Download PDF

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Publication number
EP3001135B1
EP3001135B1 EP15186723.1A EP15186723A EP3001135B1 EP 3001135 B1 EP3001135 B1 EP 3001135B1 EP 15186723 A EP15186723 A EP 15186723A EP 3001135 B1 EP3001135 B1 EP 3001135B1
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EP
European Patent Office
Prior art keywords
tube
lever
missile
missile launcher
frame
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Active
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EP15186723.1A
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German (de)
French (fr)
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EP3001135A1 (en
Inventor
Jean Luc Duinat
Joris BLANCHET
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.)
Nexter Systems SA
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Nexter Systems SA
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Priority to PL15186723T priority Critical patent/PL3001135T3/en
Publication of EP3001135A1 publication Critical patent/EP3001135A1/en
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Publication of EP3001135B1 publication Critical patent/EP3001135B1/en
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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00—Rocket or torpedo launchers
    • F41F3/04—Rocket or torpedo launchers for rockets
    • F41F3/077—Doors or covers for launching tubes

Definitions

  • the technical field of the invention is that of missile launchers.
  • the missile lances have at least one tube for receiving a missile and to guide it during the initial launch phase of the missile.
  • the tube is oriented at an angle of elevation for which the opening of the tube is no longer closed by the wall.
  • the minimum pointing site is therefore dictated by the height of the wall, which can not be less than the size of the opening of the tube, which can be very restrictive for certain firing distances for which the elevation angle is reduced, for example. example short-range shooting.
  • the object of the invention is to solve this problem of situobturation of the tube for a reduced angle of elevation.
  • the invention also simplifies the mechanism for opening and closing the tube, in particular by not using motor means dedicated to the opening of the tube.
  • the invention relates to a missile launcher comprising a frame and a tube for launching a missile, the tube being orientable about a site axis with respect to the frame, tube comprising at least one of its ends. at least one articulation parallel to the axis of site, articulation intended to allow the tilting relative to the tube of at least one flap at least partially closing the tube, the missile lance comprises at least one lever comprising two branches forming an angle, a pivot connection secured to the frame and parallel to the axis of the site being positioned at the intersection of the branches, a first end of the lever being intended to slide along one face of the shutter facing the outside of the tube when the latter is closed by the shutter and a second end of the lever being intended to slide longitudinally on one side of the tube.
  • the lever comprises means for adjusting the distance separating its ends.
  • the missile lance comprises an elastic means having the effect of promoting the tilting of the flap in the direction of opening of the tube.
  • the first end of the lever comprises a first wheel intended to traverse a first ramp secured to a slice of the flap.
  • the second end of the lever comprises a second wheel intended to traverse a second ramp secured to a side face of the tube.
  • the missile lance comprises an orientation means interposed between the lever and the frame, orientation means having the effect of pivoting the lever so as to bring the first end of the frame.
  • the orientation means comprises at least one spring.
  • a missile lance 1 intended to be installed on a vehicle comprises a frame 2 and a tube 3 intended to receive a missile 4.
  • the tube 3 is orientable in site around a site axis 5 by elevating motor means (raising means 15 visible to the figure 4 ) and is substantially parallel to the horizontal 6 when no target pointing is envisaged.
  • the rear portion AR of the tube includes a blast baffle of the type described in FR2934041 designed to deflect the missile fire gases upwards.
  • the front part AV of the tube through which the missile fires when fired, is closed by a flap 7 which can swing forward around a hinge 11 secured to the lower part of the tube 3 and parallel to the axis of site 5.
  • the flap 7 has on one of its slices, oriented vertically when the tube is closed, a first ramp 7a. On the face of this ramp 7a facing the outside of the tube, can roll a first caster 16a fixed to a first end 8a of a lever 8.
  • a second end 8b of the lever 8 comprises a second caster 16b which is intended to roll along a second ramp 3a integral with the tube 3 and oriented longitudinally with respect to the tube 3.
  • the ends 8a and 8b of the lever 8 could slide without a roller on the outer face 7a of the flap 7 and on the tube 3.
  • the lever 8 has between its two ends 8a and 8b a pivot connection 9 secured to the frame 2 and parallel to the site axis 5.
  • the V-shaped lever 8 comprising two branches 8c and 8d forming an angle between them and at the intersection of which the pivot connection 9 is located.
  • an adjusting means 10 makes it possible to adjust the distance D separating the two ends 8a and 8b of the lever 8.
  • the branches 8a and 8b are therefore independent of each other and articulated each at the level of pivot 9 to allow the angular approximation of these two branches by the adjusting means 10.
  • This adjustment means 10 may comprise means conventionally known to those skilled in the art such as threaded rods extending from each leg with steps inverted relative to each other and interconnected by a threaded tube.
  • the distance D will be chosen so that each of the ends 8a and 8b of the lever 8 is in contact with the ramps 3a and 7a when the tube is horizontal with the flap 7 closing the front of the tube 3.
  • the tube 3 begins to pivot about its axis of site 5 bringing the front part AV of the tube above the horizontal axis 6 passing through the axis of site 5.
  • the support of the tube 3 at the level of the second 8b end of the lever 8 is gradually relieved.
  • the second end 8b of the lever 8 moves longitudinally towards the front of the tube 3 along the second ramp 3a as the angle of elevation of the tube increases, which also decreases the support of the first end 8a of the lever 8 on the flap 7 (the two branches 8c and 8d being integral with each other).
  • a resilient means 11a such as a spring the flap 7 then opens by swinging downwardly as the first end 8a of the lever pivots downwardly rolling along the first ramp 7a which limits the opening stroke of the flap.
  • the skilled person can overcome the use of an elastic means at the flap. In this case the tilting of the flap 7 will be due simply to the effect of gravity.
  • Dashed is represented at the figure 2 a wall 77 representing the position occupied by a front wall of a trunk according to the prior art. It will be noted that for the elevation angle according to figure 2 which is of the order of 8 °, so relatively low, the opening of the tube is completely clear while for the same angle the wall 77 still significantly hinders the opening of the tube.
  • the tube 3 continues to rise in elevation by means of elevation 15 comprising a jack.
  • the ends 8a and 8b lever 8 are no longer in contact with the tube 3 or with the flap 7.
  • the invention thus also allows missile fire at high elevation angles.
  • an orientation means 12 the lever such as a tension spring, can be placed between the lever 8 and the frame 2. This orientation means will rotate the lever 8 so as to bring its first end 8a of the chassis 2.
  • lever 8 ensures both the complete opening and low site of a closure flap of a missile launcher and closing said shutter. No specific motorization is necessary to open or close the shutter 7. It is the pointing movement in site of the tube 3 which will control the opening or closing of the shutter 7.

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

Description

Le domaine technique de l'invention est celui des lance-missiles.The technical field of the invention is that of missile launchers.

Les lances missiles comportent au moins un tube destiné à recevoir un missile et à le guider durant la phase initiale de lancement du missile.The missile lances have at least one tube for receiving a missile and to guide it during the initial launch phase of the missile.

Afin d'éviter l'intrusion volontaire ou accidentelle dans le tube d'éléments susceptibles de provoquer un disfonctionnement du lance missile, celui-ci est souvent contenu dans un coffre dont au moins une paroi située à l'avant du lance missile obstrue le tube comme en témoigne le brevet FR2934041 .In order to avoid accidental or accidental intrusion into the tube of elements likely to cause malfunction of the missile lance, it is often contained in a trunk with at least one wall located at the front of the missile lance obstructing the tube as evidenced by the patent FR2934041 .

Ainsi, sur un tel lance missile, lors d'un tir, il convient d'orienter le tube selon un angle de site pour lequel l'ouverture du tube n'est plus obturée par la paroi. Le site de pointage minimum est donc dicté par la hauteur de la paroi qui ne peut être inférieure à la dimension de l'ouverture du tube ce qui peut être très contraignant pour certaines distances de tir pour lesquelles l'angle de site est réduit, par exemple les tirs à courte distance.Thus, on such a missile lance, during a shot, it is advisable to orient the tube at an angle of elevation for which the opening of the tube is no longer closed by the wall. The minimum pointing site is therefore dictated by the height of the wall, which can not be less than the size of the opening of the tube, which can be very restrictive for certain firing distances for which the elevation angle is reduced, for example. example short-range shooting.

L'invention a pour objet de résoudre ce problème de désobturation du tube pour un angle de site réduit.The object of the invention is to solve this problem of désobturation of the tube for a reduced angle of elevation.

L'invention permet également de simplifier le mécanisme d'ouverture et de fermeture du tube, en permettant en particulier de ne pas utiliser de moyens moteurs dédiés à l'ouverture du tube.The invention also simplifies the mechanism for opening and closing the tube, in particular by not using motor means dedicated to the opening of the tube.

Ainsi, l'invention a pour objet un lance missile comportant un châssis et un tube destiné à lancer un missile, le tube étant orientable autour d'un axe de site par rapport au châssis, tube comportant au moins à l'une de ses extrémités au moins une articulation parallèle à l'axe de site, articulation destinée à permettre le basculement par rapport au tube d'au moins un volet obturant au moins partiellement le tube, le lance missile comporte au moins un levier comportant deux branches formant un angle, une liaison pivot solidaire du châssis et parallèle à l'axe de site étant positionnée à l'intersection des branches, une première extrémité du levier étant destinée à coulisser le long d'une face du volet orientée vers l'extérieur du tube quand celui-ci est fermé par le volet et une seconde extrémité du levier étant destinée à coulisser longitudinalement sur une face du tube.Thus, the invention relates to a missile launcher comprising a frame and a tube for launching a missile, the tube being orientable about a site axis with respect to the frame, tube comprising at least one of its ends. at least one articulation parallel to the axis of site, articulation intended to allow the tilting relative to the tube of at least one flap at least partially closing the tube, the missile lance comprises at least one lever comprising two branches forming an angle, a pivot connection secured to the frame and parallel to the axis of the site being positioned at the intersection of the branches, a first end of the lever being intended to slide along one face of the shutter facing the outside of the tube when the latter is closed by the shutter and a second end of the lever being intended to slide longitudinally on one side of the tube.

Avantageusement, le levier comporte un moyen de réglage de la distance séparant ses extrémités.Advantageously, the lever comprises means for adjusting the distance separating its ends.

Avantageusement, le lance missile comporte un moyen élastique ayant pour effet de favoriser le basculement du volet dans le sens de l'ouverture du tube.Advantageously, the missile lance comprises an elastic means having the effect of promoting the tilting of the flap in the direction of opening of the tube.

Avantageusement, la première extrémité du levier comporte une première roulette destinée à parcourir une première rampe solidaire d'une tranche du volet.Advantageously, the first end of the lever comprises a first wheel intended to traverse a first ramp secured to a slice of the flap.

Avantageusement, la seconde extrémité du levier comporte une seconde roulette destinée à parcourir une seconde rampe solidaire d'une face latérale du tube.Advantageously, the second end of the lever comprises a second wheel intended to traverse a second ramp secured to a side face of the tube.

Avantageusement, le lance missile comprend un moyen d'orientation interposé entre le levier et le châssis, moyen d'orientation ayant pour effet de faire pivoter le levier de façon à rapprocher la première extrémité du châssis.Advantageously, the missile lance comprises an orientation means interposed between the lever and the frame, orientation means having the effect of pivoting the lever so as to bring the first end of the frame.

Avantageusement, le moyen d'orientation comporte au moins un ressort.Advantageously, the orientation means comprises at least one spring.

L'invention sera mieux comprise à la lecture de la description jointe, description faire en référence aux dessins annexés, dessins dans lesquels :

  • La figure 1 représente un lance missile selon l'invention tube fermé.
  • La figure 2 représente un lance missile selon l'invention tube ouvert au site le plus bas.
  • La figure 3 représente un lance missile selon l'invention tube ouvert à un site élevé.
  • La figure 4 représente une vue de trois quarts d'un lance missile selon l'invention tube ouvert.
The invention will be better understood on reading the attached description, description with reference to the appended drawings, drawings in which:
  • The figure 1 represents a missile launcher according to the invention closed tube.
  • The figure 2 represents a missile launcher according to the invention open tube at the lowest site.
  • The figure 3 represents a missile launcher according to the invention open tube at a high site.
  • The figure 4 represents a three-quarter view of a missile launcher according to the invention open tube.

Selon la figure 1, un lance missile 1 destiné à être installé sur un véhicule (véhicule non représenté) comporte un châssis 2 ainsi qu'un tube 3 destiné à recevoir un missile 4. Le tube 3 est orientable en site autour d'un axe de site 5 par un moyen moteur d'élévation (moyen d'élévation 15 visible à la figure 4) et il est sensiblement parallèle à l'horizontale 6 lorsqu'aucun pointage de cible n'est envisagé.According to figure 1 , a missile lance 1 intended to be installed on a vehicle (vehicle not shown) comprises a frame 2 and a tube 3 intended to receive a missile 4. The tube 3 is orientable in site around a site axis 5 by elevating motor means (raising means 15 visible to the figure 4 ) and is substantially parallel to the horizontal 6 when no target pointing is envisaged.

La partie arrière AR du tube comporte un déflecteur 20 de souffle du type décrit dans FR2934041 destiné à dévier les gaz de tir du missile vers le haut.The rear portion AR of the tube includes a blast baffle of the type described in FR2934041 designed to deflect the missile fire gases upwards.

La partie avant AV du tube par laquelle le missile sort en cas de tir, est obturée par un volet 7 pouvant basculer vers l'avant autour d'une articulation 11 solidaire de la partie inférieure du tube 3 et parallèle à l'axe de site 5.The front part AV of the tube through which the missile fires when fired, is closed by a flap 7 which can swing forward around a hinge 11 secured to the lower part of the tube 3 and parallel to the axis of site 5.

Le volet 7 comporte sur une de ses tranches, orientée verticalement quand le tube est fermé, une première rampe de roulement 7a. Sur la face de cette rampe 7a orientée vers l'extérieur du tube, peut rouler une première roulette 16a fixée à une première extrémité 8a d'un levier 8. Une seconde extrémité 8b du levier 8 comporte une seconde roulette 16b qui est destinée à rouler le long d'une seconde rampe 3a solidaire du tube 3 et orientée longitudinalement par rapport au tube 3.The flap 7 has on one of its slices, oriented vertically when the tube is closed, a first ramp 7a. On the face of this ramp 7a facing the outside of the tube, can roll a first caster 16a fixed to a first end 8a of a lever 8. A second end 8b of the lever 8 comprises a second caster 16b which is intended to roll along a second ramp 3a integral with the tube 3 and oriented longitudinally with respect to the tube 3.

Selon un autre mode de réalisation non représenté, les extrémités 8a et 8b du levier 8 pourraient coulisser sans roulette sur la face externe 7a du volet 7 et sur le tube 3.According to another embodiment not shown, the ends 8a and 8b of the lever 8 could slide without a roller on the outer face 7a of the flap 7 and on the tube 3.

Le levier 8 comporte entre ses deux extrémités 8a et 8b une liaison pivot 9 solidaire du châssis 2 et parallèle à l'axe de site 5.The lever 8 has between its two ends 8a and 8b a pivot connection 9 secured to the frame 2 and parallel to the site axis 5.

Selon le mode de réalisation représenté, le levier 8 à une forme de V comportant deux branches 8c et 8d formant un angle entre elles et à l'intersection desquelles se situe la liaison pivot 9.According to the embodiment shown, the V-shaped lever 8 comprising two branches 8c and 8d forming an angle between them and at the intersection of which the pivot connection 9 is located.

Suivant le mode de réalisation décrit, un moyen de réglage 10 permet de régler la distance D séparant les deux extrémités 8a et 8b du levier 8. Les branches 8a et 8b sont donc indépendantes l'une de l'autre et articulées chacune au niveau du pivot 9 pour permettre le rapprochement angulaire de ces deux branches par le moyen de réglage 10.According to the embodiment described, an adjusting means 10 makes it possible to adjust the distance D separating the two ends 8a and 8b of the lever 8. The branches 8a and 8b are therefore independent of each other and articulated each at the level of pivot 9 to allow the angular approximation of these two branches by the adjusting means 10.

Ce moyen de réglage 10 pourra comporter des moyens classiquement connus de l'Homme du Métier tels que des tiges filetées partant de chaque branche avec des pas inversés l'un par rapport à l'autre et reliées entre elles par un tube taraudé.This adjustment means 10 may comprise means conventionally known to those skilled in the art such as threaded rods extending from each leg with steps inverted relative to each other and interconnected by a threaded tube.

La distance D sera choisie de manière à ce que chacune des extrémités 8a et 8b du levier 8 soit en appui avec les rampes 3a et 7a lorsque le tube est à l'horizontale avec le volet 7 fermant l'avant du tube 3.The distance D will be chosen so that each of the ends 8a and 8b of the lever 8 is in contact with the ramps 3a and 7a when the tube is horizontal with the flap 7 closing the front of the tube 3.

On note ainsi que l'action d'appui du tube 3 sur la seconde extrémité 8b du levier provoque, par effet de bascule au niveau de la liaison pivot 9, l'appui de la première extrémité 8a du levier sur la face externe du volet 7 condamnant celui-ci à demeurer en position fermée.It is thus noted that the action of bearing the tube 3 on the second end 8b of the lever causes, by the effect of rocking at the pivot connection 9, the support of the first end 8a of the lever on the outer face of the flap 7 condemning it to remain in the closed position.

Selon la figure 2, le tube 3 entame un pivotement autour de son axe de site 5 amenant la partie avant AV du tube au-dessus de l'axe horizontal 6 passant par l'axe de site 5. L'appui du tube 3 au niveau de la seconde extrémité 8b du levier 8 est progressivement soulagé.According to figure 2 , the tube 3 begins to pivot about its axis of site 5 bringing the front part AV of the tube above the horizontal axis 6 passing through the axis of site 5. The support of the tube 3 at the level of the second 8b end of the lever 8 is gradually relieved.

La seconde extrémité 8b du levier 8 se déplace longitudinalement vers l'avant du tube 3 le long de la seconde rampe 3a au fur et à mesure de l'augmentation de l'angle de site du tube, ce qui diminue aussi l'appui de la première extrémité 8a du levier 8 sur le volet 7 (les deux branches 8c et 8d étant solidaires l'une de l'autre).The second end 8b of the lever 8 moves longitudinally towards the front of the tube 3 along the second ramp 3a as the angle of elevation of the tube increases, which also decreases the support of the first end 8a of the lever 8 on the flap 7 (the two branches 8c and 8d being integral with each other).

Sous l'action d'un moyen élastique 11a tel qu'un ressort le volet 7 s'ouvre alors en basculant vers le bas au fur et à mesure que la première extrémité 8a du levier pivote vers le bas en roulant le long de la première rampe 7a qui limite la course d'ouverture du volet.Under the action of a resilient means 11a such as a spring the flap 7 then opens by swinging downwardly as the first end 8a of the lever pivots downwardly rolling along the first ramp 7a which limits the opening stroke of the flap.

Selon un autre mode de réalisation, l'Homme du Métier pourra s'affranchir de l'usage d'un moyen élastique au niveau du volet. Dans ce cas le basculement du volet 7 sera dû simplement à l'effet de la gravité.According to another embodiment, the skilled person can overcome the use of an elastic means at the flap. In this case the tilting of the flap 7 will be due simply to the effect of gravity.

En pointillés est représentée à la figure 2 une paroi 77 représentant la position occupée par une paroi avant d'un coffre selon l'art antérieur. On notera que pour l'angle de site selon la figure 2 qui est de l'ordre de 8°, donc relativement faible, l'ouverture du tube est totalement dégagée alors que pour le même angle la paroi 77 entrave encore significativement l'ouverture du tube.Dashed is represented at the figure 2 a wall 77 representing the position occupied by a front wall of a trunk according to the prior art. It will be noted that for the elevation angle according to figure 2 which is of the order of 8 °, so relatively low, the opening of the tube is completely clear while for the same angle the wall 77 still significantly hinders the opening of the tube.

On voit donc que l'invention permet le tir d'un missile avec un pointage faible. Selon les figures 3 et 4, le tube 3 poursuit son élévation en site grâce au moyen d'élévation 15 comportant un vérin. Les extrémités 8a et 8b du levier 8 ne sont plus en contact ni avec le tube 3 ni avec le volet 7.So we see that the invention allows the firing of a missile with a low score. According to figures 3 and 4 the tube 3 continues to rise in elevation by means of elevation 15 comprising a jack. The ends 8a and 8b lever 8 are no longer in contact with the tube 3 or with the flap 7.

L'invention permet donc également le tir de missile à des angles d'élévation importants.The invention thus also allows missile fire at high elevation angles.

On notera à la figure 3 qu'un moyen d'orientation 12, du levier tel qu'un ressort de traction, pourra être placé entre le levier 8 et le châssis 2. Ce moyen d'orientation fera pivoter le levier 8 de façon à rapprocher sa première extrémité 8a du châssis 2.We will note in figure 3 that an orientation means 12, the lever such as a tension spring, can be placed between the lever 8 and the frame 2. This orientation means will rotate the lever 8 so as to bring its first end 8a of the chassis 2.

Ceci permet, lorsque le tube 3 redescend à site horizontal, que la seconde extrémité 8b roule d'abord sur la seconde rampe 3a, fixée sur une face latérale du tube 3, pour ensuite permettre la remontée du volet 7 par roulement de la première extrémité 8a du levier sur la première rampe 7a jusqu'à fermeture complète du tube 3.This allows, when the tube 3 descends to horizontal site, the second end 8b rolls first on the second ramp 3a, fixed on a side face of the tube 3, to then allow the raising of the flap 7 by rolling the first end 8a of the lever on the first ramp 7a until complete closure of the tube 3.

Ainsi le levier 8 permet d'assurer à la fois l'ouverture complète et à site faible d'un volet de fermeture d'un tube lance-missile et la fermeture dudit volet. Aucune motorisation spécifique n'est nécessaire pour ouvrir ou fermer le volet 7. C'est le mouvement de pointage en site du tube 3 qui va commander l'ouverture ou la fermeture du volet 7.Thus the lever 8 ensures both the complete opening and low site of a closure flap of a missile launcher and closing said shutter. No specific motorization is necessary to open or close the shutter 7. It is the pointing movement in site of the tube 3 which will control the opening or closing of the shutter 7.

Claims (7)

  1. A missile launcher (1) comprising a frame (2) and a tube (3) for launching a missile (4), the tube (3) being pointable around an elevation axis (5) with respect to the frame (2), the tube (3) comprising, at least at one of its ends, at least one hinge (11) parallel to the elevation axis (5), the hinge (11) allowing at least one shutter (7), at least partially blocking the tube (3), to be tilted with respect to the tube (3), the missile launcher (1) being characterized in that it comprises at least one lever (8) comprising two legs (8c and 8d) forming an angle, a pivot link (9) integral with the frame (2) and parallel to the elevation axis (5) being arranged at the intersection of the legs (8c and 8d), a first end (8a) of the lever (8) being intended to slide along a face (7a) of the shutter (7) directed to the outside of the tube (3) when closed by the shutter (7), and a second end of the lever (8) being intended to longitudinally slide on a face (3a) of the tube (3).
  2. The missile launcher (1) according to claim 1, characterized in that the lever (8) comprises a means (10) for adjusting the distance separating its ends (8a and 8b).
  3. The missile launcher (1) according to one of claims 1 or 2, characterized in that it comprises an elastic means (11a) having the effect of causing the shutter (7) to be tilted in the direction of opening the tube (3).
  4. The missile launcher (1) according to one of claims 1 to 3, characterized in that the first end (8a) of the lever (8) comprises a first wheel (16a) for moving on a first ramp (7a) integral with an edge of the shutter (7).
  5. The missile launcher (1) according to one of claims 1 to 4, characterized in that the second end (8b) of the lever (8) comprises a second wheel (16b) for moving on a second ramp (3a) integral with a side face of the tube (3).
  6. The missile launcher (1) according to one of claims 1 to 5, characterized in that it comprises an orientation means (12) arranged between the lever (8) and the frame (2), the orientation means (12) having the effect of pivoting the lever (8) so as to move the first end (8a) closer to the frame (2).
  7. The missile launcher (1) according to claim 6, characterized in that the orientation means (12) comprises at least one spring (12).
EP15186723.1A 2014-09-26 2015-09-24 Missile launcher Active EP3001135B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL15186723T PL3001135T3 (en) 2014-09-26 2015-09-24 Missile launcher

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1402191A FR3026479B1 (en) 2014-09-26 2014-09-26 LANCE MISSILE

Publications (2)

Publication Number Publication Date
EP3001135A1 EP3001135A1 (en) 2016-03-30
EP3001135B1 true EP3001135B1 (en) 2016-12-07

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EP (1) EP3001135B1 (en)
DK (1) DK3001135T3 (en)
ES (1) ES2612437T3 (en)
FR (1) FR3026479B1 (en)
IL (1) IL241805B (en)
PL (1) PL3001135T3 (en)

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FR3058789B1 (en) * 2016-11-15 2018-11-02 Nexter Systems PROJECTILE SHOOTING SYSTEM
FR3062717B1 (en) 2017-02-07 2021-01-01 Nexter Systems BOX INTENDED TO BE DISPOSED OF ON A VEHICLE AND WEAPON SYSTEM INCLUDING SUCH A BOX.

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GB256741A (en) * 1925-06-11 1926-08-19 Whitehead Torpedo Company Ltd Improvements in or relating to launching or ejecting tubes for automobile torpedoes
JPH0561689U (en) * 1992-01-16 1993-08-13 三菱電機株式会社 Canister lid opening mechanism device
RU2182305C2 (en) * 1995-11-08 2002-05-10 Военно-морская академия имени Адмирала Флота Советского Союза Н.Г.Кузнецова Underwater torpedo tube
FR2934041B1 (en) * 2008-07-17 2011-07-01 Dcns ARMS SYSTEM, IN PARTICULAR FOR MISSILES, INTENDED TO BE INTEGRATED INTO A COMBAT PLATFORM AND CORRESPONDING COMBAT PLATFORM

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PL3001135T3 (en) 2017-05-31
FR3026479A1 (en) 2016-04-01
DK3001135T3 (en) 2017-01-23
EP3001135A1 (en) 2016-03-30
FR3026479B1 (en) 2016-09-02
ES2612437T3 (en) 2017-05-16
IL241805B (en) 2018-12-31

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