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EP3542121A1 - Projectile firing system - Google Patents

Projectile firing system

Info

Publication number
EP3542121A1
EP3542121A1 EP17811985.5A EP17811985A EP3542121A1 EP 3542121 A1 EP3542121 A1 EP 3542121A1 EP 17811985 A EP17811985 A EP 17811985A EP 3542121 A1 EP3542121 A1 EP 3542121A1
Authority
EP
European Patent Office
Prior art keywords
hatch
firing system
opening
hinge
projectile
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
Application number
EP17811985.5A
Other languages
German (de)
French (fr)
Other versions
EP3542121B1 (en
Inventor
Xavier DESCATOIRE
Aymeric Peloux
Christophe FAES
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
Original Assignee
Nexter Systems SA
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Nexter Systems SA filed Critical Nexter Systems SA
Priority to PL17811985T priority Critical patent/PL3542121T3/en
Publication of EP3542121A1 publication Critical patent/EP3542121A1/en
Application granted granted Critical
Publication of EP3542121B1 publication Critical patent/EP3542121B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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
    • 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
    • F41F3/0413—Means for exhaust gas disposal, e.g. exhaust deflectors, gas evacuation systems

Definitions

  • the technical field of the invention is that of projectile firing systems and in particular missile launcher boxes (or pods) mounted on a platform, for example a vehicle.
  • Projectile firing systems having a housing containing at least one projectile are well known. These systems are mounted on a platform, such as a vehicle, and they allow the pointing and firing of one or more projectiles such as missiles or rockets.
  • the hatch is intended to open by pivoting around a site axis by means of a motorized means to allow firing of the projectile or the replenishment of the box with one or more new projectiles.
  • the motorized opening of the hatch requires powering the firing system to be able to activate the opening of the hatch.
  • the opening in site of the hatch is not always favorable to the accessibility of the end of the box, in particular when it is located in superstructure of a vehicle.
  • the invention aims to simplify replenishment operations of a firing system by not imposing power on the firing system.
  • the invention relates to a projectile firing system, in particular a missile launcher, comprising a caisson which is intended to contain at least one projectile and one end of which is closed by at least one hatch, a hatch which is articulated by one of its sides relative to the casing by means of a first hinge, a firing system characterized in that the hatch comprises an opening which is articulated with respect to the hatch with a second hinge oriented perpendicular to the first hinge.
  • the first hinge allows pivoting of the hatch around a horizontal axis.
  • the firing system comprises a motor means for pivoting the hatch around the first hinge.
  • the hatch comprises an L-shaped frame on which is articulated the opening.
  • the opening comprises a lock intended to prevent the pivoting of the second hinge.
  • the opening comprises a holding means in the open position for locking the opening perpendicular to a plane of the hatch.
  • Figure 1 shows a three-quarter view of a firing system according to the invention fixed on a vehicle turret.
  • Figure 2 shows a detail view of the firing system with a hatch in the closed position and its opening also closed.
  • FIG. 3 shows a detail view of the firing system with a hatch in the open position, the opening integral with the hatch being closed.
  • Figure 4 shows a detailed view of the system shot with a hatch in the closed position and the hatch opening in the open position.
  • a turret 200 of a vehicle 100 is armed with a firing system 1 disposed on one of the side and vertical walls 201 of the turret 200.
  • the firing system 1 is orientable in site with respect to the wall 201 around a site axis 101 by means of electrical pointing means or hydraulic (pointing means not shown).
  • the bearing orientation of the firing system 1 is by pivoting the turret 200 about a bearing axis 201 and relative to the chassis of the vehicle 100.
  • the firing system 1 comprises a caisson 2 which according to the illustrated embodiment has a square profile.
  • the caisson 2 is intended to contain at least one projectile, here a missile 8, and it thus forms a launch tube for this missile.
  • the rear AR of the box 2 ( Figure 1) is closed by a hatch 3 having on its upper side a first hinge 4 whose axis is parallel to the axis of site 101, so here substantially horizontal.
  • the hatch 3 carries an opening 5 which here has a square shape of dimensions slightly smaller than those of the square shape of the hatch 3 and which is fixed to a part of the hatch 3 which forms a frame 3a and which is L-shaped. .
  • the frame 3a thus comprises a horizontal upper bar 3al carrying the first hinge 4 and a lateral bar 3a2 which is vertical and which carries a second hinge 9 on which is fixed the opening 5.
  • a latch 6 allows to make the opening 5 and the frame 3a, thus preventing the opening by pivoting the opening 5 relative to the hatch 3.
  • Sealing means between the frame 3a and the opening 5 will be provided, for example deformable joints.
  • the thickness of the opening 5 will advantageously be the same as that of the frame 3a.
  • a motor means 7, such as an electric or hydraulic jack, can be implemented provided that the energy servitudes of the firing system 1 are activated (power up the firing system).
  • the cylinder 7 allows, during the operating phases of the firing system, the opening in the upward position of the hatch
  • motor means conventionally known to those skilled in the art would be possible.
  • an electric motor associated with a gear train or with pulleys and a belt or sprockets and a chain may be used as a motor means 7 for opening and closing the hatch 3.
  • the hatch 3 is sufficiently open so as to be clear of the trajectory of the propellant jet of the missile 8, which jet is ejected by the nozzle of the latter (propulsion jet not shown).
  • the box 2 can be oriented in situ without risk of interference with vehicle elements located downward, such as the roof for example.
  • the lock 6 may be a manual operation lock conventionally known to those skilled in the art such as the lock described in the patent IT7921144 for example. It may include a key lock to block access to the contents of the box 2. Means for holding in the open position (for example a forestay set up manually) may be added to the opening to block the opening in this last position and prevent its closure during reloading of the tube 2 (holding means in position not shown).
  • the invention allows a replenishment of the caisson 2 without having to start the energy servitudes of the firing system 1 and therefore without the need to actuate any motor means.
  • a servant can simply open the opening and reload the box 2.
  • the opening of the opening 5 being around a vertical axis, the maneuver of this opening is facilitated compared to that of the hatch itself which, once opened, forms an obstacle limiting access to the box.

Landscapes

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

Abstract

The invention relates to a projectile firing system (1), in particular a missile launcher (1), comprising a box (2) which is designed to contain at least one projectile (8) and one end of which is closed by at least one hatch (3), hatch (3) which is hinged on one of its sides relative to the box (2) through a first hinge (4), firing system (1) characterised in that the hatch (3) comprises a leaf (5) which is hinged relative to the hatch (3) through a second hinge (9) oriented perpendicularly to the first hinge (4).

Description

SYSTEME DE TIR DE PROJECTILE  PROJECTILE SHOOTING SYSTEM
Le domaine technique de 1 ' invention est celui des systèmes de tir de projectiles et en particulier des caissons (ou pods) lance-missiles montés sur une plateforme, par exemple un véhicule. The technical field of the invention is that of projectile firing systems and in particular missile launcher boxes (or pods) mounted on a platform, for example a vehicle.
Les systèmes de tir de projectiles comportant un caisson contenant au moins un projectile sont bien connus. Ces systèmes sont montés sur une plateforme, telle qu'un véhicule, et ils permettent le pointage et le tir d'un ou de plusieurs projectiles tels que des missiles ou des roquettes.  Projectile firing systems having a housing containing at least one projectile are well known. These systems are mounted on a platform, such as a vehicle, and they allow the pointing and firing of one or more projectiles such as missiles or rockets.
Afin d'empêcher l'entrée de corps étrangers dans le caisson du système de tir, il est classiquement connu d'obturer ce caisson avec une trappe articulée comme on peut le voir dans le brevet FR3026479.  In order to prevent the entry of foreign bodies into the box of the firing system, it is conventionally known to close this box with a hinged door as can be seen in the patent FR3026479.
La trappe est destinée à s'ouvrir par pivotement autour d'un axe de site grâce à un moyen motorisé pour permettre le tir du projectile ou bien le réapprovisionnement du caisson avec un ou plusieurs nouveaux projectiles.  The hatch is intended to open by pivoting around a site axis by means of a motorized means to allow firing of the projectile or the replenishment of the box with one or more new projectiles.
Lors des opérations de réapprovisionnement du système de tir, l'ouverture motorisée de la trappe impose de mettre sous tension électrique le système de tir pour pouvoir activer l'ouverture de la trappe.  When replenishing the firing system, the motorized opening of the hatch requires powering the firing system to be able to activate the opening of the hatch.
En outre, l'ouverture en site de la trappe n'est pas toujours favorable à l'accessibilité de l'extrémité du caisson, en particulier lorsque celui-ci est situé en superstructure d'un véhicule.  In addition, the opening in site of the hatch is not always favorable to the accessibility of the end of the box, in particular when it is located in superstructure of a vehicle.
L'invention vise à simplifier les opérations de réapprovisionnement d'un système de tir en n'imposant pas la mise sous tension du système de tir.  The invention aims to simplify replenishment operations of a firing system by not imposing power on the firing system.
Ainsi , l'invention porte sur un système de tir de projectile, en particulier un lance missile, comportant un caisson qui est destiné à contenir au moins un projectile et dont une extrémité est obturée par au moins une trappe, trappe qui est articulée par l'un de ses cotés relativement au caisson grâce à une première charnière, système de tir caractérisé en ce que la trappe comporte un ouvrant qui est articulé par rapport à la trappe grâce à une seconde charnière orientée perpendiculairement à la première charnière . Thus, the invention relates to a projectile firing system, in particular a missile launcher, comprising a caisson which is intended to contain at least one projectile and one end of which is closed by at least one hatch, a hatch which is articulated by one of its sides relative to the casing by means of a first hinge, a firing system characterized in that the hatch comprises an opening which is articulated with respect to the hatch with a second hinge oriented perpendicular to the first hinge.
Avantageusement, la première charnière permet un pivotement de la trappe autour d'un axe horizontal.  Advantageously, the first hinge allows pivoting of the hatch around a horizontal axis.
Avantageusement, le système de tir comporte un moyen moteur permettant le pivotement de la trappe autour de la première charnière.  Advantageously, the firing system comprises a motor means for pivoting the hatch around the first hinge.
Avantageusement, la trappe comporte un dormant en forme de L sur lequel est articulé l'ouvrant.  Advantageously, the hatch comprises an L-shaped frame on which is articulated the opening.
Avantageusement, l'ouvrant comporte un verrou destiné à interdire le pivotement de la seconde charnière.  Advantageously, the opening comprises a lock intended to prevent the pivoting of the second hinge.
Avantageusement, l'ouvrant comporte une moyen de maintien en position ouverte destiné à bloquer l'ouvrant à la perpendiculaire d'un plan de la trappe.  Advantageously, the opening comprises a holding means in the open position for locking the opening perpendicular to a plane of the hatch.
L'invention sera mieux comprise à la lecture de la description suivante, description faite en référence aux dessins en annexe, dessins dans lesquels : The invention will be better understood on reading the following description, description made with reference to the appended drawings, drawings in which:
La figure 1 représente une vue de trois quarts d'un système de tir selon l'invention fixé sur une tourelle de véhicule .  Figure 1 shows a three-quarter view of a firing system according to the invention fixed on a vehicle turret.
La figure 2 représente une vue de détail du système de tir avec une trappe en position fermée et son ouvrant également fermé.  Figure 2 shows a detail view of the firing system with a hatch in the closed position and its opening also closed.
La figure 3 représente une vue de détail du système de tir avec une trappe en position ouverte, l'ouvrant solidaire de la trappe étant fermé. La figure 4 représente une vue de détail du système tir avec une trappe en position fermée et l'ouvrant de trappe en position ouverte. Selon la figure 1, une tourelle 200 d'un véhicule 100 est armée d'un système de tir 1 disposé sur l'une des parois 201 latérale et verticale de la tourelle 200. Le système de tir 1 est orientable en site par rapport à la paroi 201 autour d'un axe de site 101 grâce à des moyens de pointage électrique ou hydrauliques (moyens de pointage non représentés) . 3 shows a detail view of the firing system with a hatch in the open position, the opening integral with the hatch being closed. Figure 4 shows a detailed view of the system shot with a hatch in the closed position and the hatch opening in the open position. According to FIG. 1, a turret 200 of a vehicle 100 is armed with a firing system 1 disposed on one of the side and vertical walls 201 of the turret 200. The firing system 1 is orientable in site with respect to the wall 201 around a site axis 101 by means of electrical pointing means or hydraulic (pointing means not shown).
L'orientation en gisement du système de tir 1 se fait par le pivotement de la tourelle 200 autour d'un axe de gisement 201 et relativement au châssis du véhicule 100.  The bearing orientation of the firing system 1 is by pivoting the turret 200 about a bearing axis 201 and relative to the chassis of the vehicle 100.
Selon la figure 2, le système de tir 1 comporte un caisson 2 qui selon le mode de réalisation illustré présente un profil carré. Le caisson 2 est destiné à contenir au moins un projectile, ici un missile 8, et il forme ainsi un tube de lancement pour ce missile.  According to FIG. 2, the firing system 1 comprises a caisson 2 which according to the illustrated embodiment has a square profile. The caisson 2 is intended to contain at least one projectile, here a missile 8, and it thus forms a launch tube for this missile.
L'arrière AR du caisson 2 (figure 1) est obturé par une trappe 3 comportant sur son coté supérieur une première charnière 4 dont l'axe est parallèle à l'axe de site 101, donc ici sensiblement horizontal.  The rear AR of the box 2 (Figure 1) is closed by a hatch 3 having on its upper side a first hinge 4 whose axis is parallel to the axis of site 101, so here substantially horizontal.
La trappe 3 porte un ouvrant 5 qui a ici une forme carrée de dimensions légèrement inférieures à celles de la forme carrée de la trappe 3 et qui est fixé à une partie de la trappe 3 qui forme un dormant 3a et qui est en forme de L.  The hatch 3 carries an opening 5 which here has a square shape of dimensions slightly smaller than those of the square shape of the hatch 3 and which is fixed to a part of the hatch 3 which forms a frame 3a and which is L-shaped. .
Comme on le voit à la figure 2, le dormant 3a comporte ainsi une barre supérieure horizontale 3al portant la première charnière 4 et une barre latérale 3a2 qui est verticale et qui porte une deuxième charnière 9 sur laquelle est fixé l'ouvrant 5.  As seen in Figure 2, the frame 3a thus comprises a horizontal upper bar 3al carrying the first hinge 4 and a lateral bar 3a2 which is vertical and which carries a second hinge 9 on which is fixed the opening 5.
L'essentiel de l'obturation du caisson 2 est donc assuré par l'ouvrant 5. Un verrou 6 permet de rendre solidaires l'ouvrant 5 et le dormant 3a, interdisant ainsi l'ouverture par pivotement de l'ouvrant 5 par rapport à la trappe 3. Des moyens d'étanchéité entre le dormant 3a et l'ouvrant 5 seront prévus, par exemple des joints déformables. L'épaisseur de l'ouvrant 5 sera avantageusement la même que celle du dormant 3a . Most of the closure of the box 2 is thus provided by the opening 5. A latch 6 allows to make the opening 5 and the frame 3a, thus preventing the opening by pivoting the opening 5 relative to the hatch 3. Sealing means between the frame 3a and the opening 5 will be provided, for example deformable joints. The thickness of the opening 5 will advantageously be the same as that of the frame 3a.
Selon la figure 3, un moyen moteur 7, tel qu'un vérin électrique ou hydraulique, peut être mis en œuvre à condition d'activer les servitudes énergétiques du système de tir 1 (mettre sous tension le système de tir) .  According to FIG. 3, a motor means 7, such as an electric or hydraulic jack, can be implemented provided that the energy servitudes of the firing system 1 are activated (power up the firing system).
Le vérin 7 permet, lors des phases de fonctionnement du système de tir, l'ouverture en site vers le haut de la trappe The cylinder 7 allows, during the operating phases of the firing system, the opening in the upward position of the hatch
3 par pivotement de celle-ci autour de la première charnière3 by pivoting it around the first hinge
4. 4.
D'autres moyens moteurs classiquement connus de l'Homme du Métier seraient possibles. Par exemple un moteur électrique associé à un train d'engrenage ou bien à des poulies et une courroie ou des pignons et une chaîne pourront être employés en tant que moyen moteur 7 pour ouvrir et fermer la trappe 3.  Other motor means conventionally known to those skilled in the art would be possible. For example, an electric motor associated with a gear train or with pulleys and a belt or sprockets and a chain may be used as a motor means 7 for opening and closing the hatch 3.
On note que la trappe 3 est suffisamment ouverte de manière à être dégagée de la trajectoire du jet propulsif du missile 8, jet qui est éjecté par la tuyère de ce dernier (jet propulsif non représenté) .  It is noted that the hatch 3 is sufficiently open so as to be clear of the trajectory of the propellant jet of the missile 8, which jet is ejected by the nozzle of the latter (propulsion jet not shown).
En outre, en ouvrant la trappe 3 vers le haut tel que sur le présent mode de réalisation, le caisson 2 pourra être orienté en site sans risque d'interférence avec des éléments du véhicule situés vers le bas, tels que le toit par exemple.  In addition, by opening the hatch 3 upwardly as in the present embodiment, the box 2 can be oriented in situ without risk of interference with vehicle elements located downward, such as the roof for example.
Selon la figure 4, la trappe 4 est fermée mais l'ouvrant According to Figure 4, the hatch 4 is closed but the opening
5 est ouvert par pivotement autour de la seconde charnière 9, qui est solidaire de la barre latérale 3a2 de la trappe 3 et disposée perpendiculairement à la première charnière 4. 5 is pivotally open around the second hinge 9, which is integral with the side bar 3a2 of the hatch 3 and disposed perpendicularly to the first hinge 4.
Le verrou 6 pourra être un verrou à fonctionnement manuel classiquement connu de l'Homme du Métier tel que le verrou décrit dans le brevet IT7921144par exemple. Il pourra comporter une fermeture à clé pour bloquer l'accès au contenu du caisson 2. Un moyen de maintien en position ouverte (par exemple un étai mis en place manuellement) pourra être adjoint à l'ouvrant afin de bloquer l'ouvrant dans cette dernière position et empêcher sa fermeture durant le rechargement du tube 2 (moyen de maintien en position non représenté) . The lock 6 may be a manual operation lock conventionally known to those skilled in the art such as the lock described in the patent IT7921144 for example. It may include a key lock to block access to the contents of the box 2. Means for holding in the open position (for example a forestay set up manually) may be added to the opening to block the opening in this last position and prevent its closure during reloading of the tube 2 (holding means in position not shown).
On constate donc que l'invention permet un réapprovisionnement du caisson 2 sans devoir procéder à un démarrage des servitudes énergétiques du système de tir 1 et donc sans nécessiter d'actionner un quelconque moyen moteur. Un servant peut simplement ouvrir l'ouvrant et recharger le caisson 2.  It can therefore be seen that the invention allows a replenishment of the caisson 2 without having to start the energy servitudes of the firing system 1 and therefore without the need to actuate any motor means. A servant can simply open the opening and reload the box 2.
L'ouverture de l'ouvrant 5 se faisant autour d'un axe vertical, la manœuvre de cet ouvrant est facilitée par rapport à celle de la trappe elle-même qui, une fois ouverte, forme un obstacle limitant l'accès au caisson.  The opening of the opening 5 being around a vertical axis, the maneuver of this opening is facilitated compared to that of the hatch itself which, once opened, forms an obstacle limiting access to the box.

Claims

REVENDICATIONS
1- Système de tir de projectile (1) , en particulier lance missile (1) , comportant un caisson (2)qui est destiné à contenir au moins un projectile (8) et dont une extrémité est obturée par au moins une trappe (3) , trappe (3) qui est articulée par l'un de ses cotés relativement au caisson (2) grâce à une première charnière (4) , système de tir (1) caractérisé en ce que la trappe (3) comporte un ouvrant (5) qui est articulé par rapport à la trappe (3) grâce à une seconde charnière (9) orientée perpendiculairement à la première charnière (4) . 1- projectile firing system (1), in particular missile launcher (1), comprising a housing (2) which is intended to contain at least one projectile (8) and one end of which is closed by at least one hatch (3). ), hatch (3) which is articulated by one of its sides relative to the box (2) with a first hinge (4), firing system (1) characterized in that the hatch (3) comprises an opening ( 5) which is articulated relative to the hatch (3) by a second hinge (9) oriented perpendicularly to the first hinge (4).
2- Système de tir (1) selon la revendication 1, caractérisé en ce que la première charnière (4) permet un pivotement de la trappe (3) autour d'un axe horizontal.  2- firing system (1) according to claim 1, characterized in that the first hinge (4) allows pivoting of the hatch (3) about a horizontal axis.
3- Système de tir (1) selon une des revendications 1 ou 2, caractérisé en ce qu'il comporte un moyen moteur (7) permettant le pivotement de la trappe (3) autour de la première charnière (4) .  3- firing system (1) according to one of claims 1 or 2, characterized in that it comprises a motor means (7) for pivoting of the hatch (3) around the first hinge (4).
4- Système de tir (1) selon une des revendications 1 à 4- firing system (1) according to one of claims 1 to
3, caractérisé en ce que la trappe (3) comporte un dormant (3a) en forme de L sur lequel est articulé l'ouvrant (5) . 3, characterized in that the hatch (3) comprises a frame (3a) L-shaped on which is articulated the opening (5).
5- Système de tir (1) selon une des revendications 1 à 5- firing system (1) according to one of claims 1 to
4, caractérisé en ce que l'ouvrant (5) comporte un verrou (6) destiné à interdire le pivotement de la seconde charnière4, characterized in that the opening (5) comprises a latch (6) intended to prevent the pivoting of the second hinge
(9) . (9).
6- Système de tir (1) selon une des revendications 1 à 6- firing system (1) according to one of claims 1 to
5, caractérisé en ce que l'ouvrant (5) comporte une moyen de maintien en position ouverte destiné à bloquer l'ouvrant (5) à la perpendiculaire d'un plan de la trappe (3) . 5, characterized in that the opening (5) comprises a holding means in the open position for locking the opening (5) perpendicular to a plane of the hatch (3).
EP17811985.5A 2016-11-15 2017-11-10 Projectile firing system Active EP3542121B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL17811985T PL3542121T3 (en) 2016-11-15 2017-11-10 Projectile firing system

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1601619A FR3058789B1 (en) 2016-11-15 2016-11-15 PROJECTILE SHOOTING SYSTEM
PCT/FR2017/053075 WO2018091804A1 (en) 2016-11-15 2017-11-10 Projectile firing system

Publications (2)

Publication Number Publication Date
EP3542121A1 true EP3542121A1 (en) 2019-09-25
EP3542121B1 EP3542121B1 (en) 2020-09-02

Family

ID=58314295

Family Applications (1)

Application Number Title Priority Date Filing Date
EP17811985.5A Active EP3542121B1 (en) 2016-11-15 2017-11-10 Projectile firing system

Country Status (4)

Country Link
EP (1) EP3542121B1 (en)
FR (1) FR3058789B1 (en)
PL (1) PL3542121T3 (en)
WO (1) WO2018091804A1 (en)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4444087A (en) * 1982-01-28 1984-04-24 The Boeing Company Missile container and extraction mechanism
GB2140898B (en) * 1983-06-01 1987-01-21 Short Brothers Ltd Weather proof canister
DE3523443C1 (en) * 1985-06-29 1987-02-05 Messerschmitt Boelkow Blohm Cover for ammunition and firing containers for aircraft
FR3026479B1 (en) * 2014-09-26 2016-09-02 Nexter Systems LANCE MISSILE

Also Published As

Publication number Publication date
FR3058789A1 (en) 2018-05-18
PL3542121T3 (en) 2020-11-16
WO2018091804A1 (en) 2018-05-24
EP3542121B1 (en) 2020-09-02
FR3058789B1 (en) 2018-11-02

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