Abstract: A steering section for guided munition comprises a steering body having n control surfaces folded inside or deployed protruding from the external surface. The steering section comprises a locking mechanism for the n control surfaces folded inside the steering body having a lock support secured thereto, a fixed sleeve secured to the lock support comprising a locking barrel, a mobile sleeve surrounding the fixed sleeve and slideable longitudinally along the locking barrel, the mobile sleeve comprising, on the outside of the fixed sleeve, a free end collaborating with the n control surfaces to keep them folded inside the steering body, a translational-locking device locking the translational movement along the mobile sleeve along the locking barrel deactivatable by unlocking force to trigger translational sliding movement of the mobile sleeve along the locking barrel and release the n control surfaces which can then move from their folded position into their deployed position.

Abstract: An ejectable protective cap for controlled munition comprises a munition body of cylindrical form, having a front end comprising a central part directed toward a target. The cap comprises n portions distributed around a longitudinal axis, to cover the front end, n being an integer?2, a cap portion having an edge in contact with an edge of a contiguous cap portion with it in a respective plane of assembly of two contiguous cap portions passing through the longitudinal axis, a pyrotechnic initiator for each cap portion comprising a pyrotechnic initiator body securely attached to the respective cap portion, a piston plunger that can slide in a seal-tight manner by one of its ends, the free other end in contact with the contiguous cap portion to separate, upon simultaneous activation of n pyrotechnic initiators, edges of the contiguous cap portions and release the front end of the munition body.

Abstract: A device for opening and locking a tail unit is provided. The tail unit includes a body and at least one fin, pivotable relative to the body along a first axis, that has a projection that forms an element. The device comprises a control ring, slidable relative to the body along a second axis, that includes a component, forming an element, that bears against the projection to deploy the fin, the second axis being non-parallel and non-secant to the first axis. A means for shaping one of the elements during translation along the second axis of the control ring towards the projection of the fin is provided on the other element. The body includes a bearing surface to support the fin during shaping, in which the support of the fin on the bearing surface corresponds to the deployed position of the fin.

Abstract: A separable ejectable protective nosecone for a guided munition comprises a munition body of cylindrical shape of longitudinal axis ZZ? having a munition body front end comprising a central part intended to be directed toward a target of the munition. The nosecone comprises, at the munition body front end and covering said front end, n contiguous nosecone portions of the same shape distributed about said longitudinal axis ZZ?, one respective pyrotechnic device per nosecone portion. Each of the pyrotechnic devices comprises a pyrotechnic device body secured to the munition body, a pusher piston in contact with the respective nosecone portion. Simultaneous activation of the n pyrotechnic devices separates the edges of the nosecone portions from their respective plane of assembly in order to free the front end of the munition body. Application: Steered or guided munitions such as those of the rocket or projectile type or missiles.

Abstract: In the field of steered munitions intended to destroy a target after at least one flight phase followed by a target approach phase, a munition comprises a munition body of cylindrical shape of longitudinal axis having, on the same side as a front end of the munition which is the end intended to be directed toward the target, a front body comprising an optic of a guidance device that guides said munition toward the target, a cap for protecting the optic, secured to the munition body, characterized in that the protective cap comprises at least one recess having a pyrotechnic device intended to destroy said protective cap so as to free the optic and make the munition guidance device operational during the target approach phase. Application: steered or guided munitions such as those of the rocket or projectile type, or missiles.

Abstract: Ammunition comprises, along a longitudinal axis, a fuse in the form of a tip, an ammunition body and a skirt, the ammunition body of cylindrical form with axis of revolution merged with the longitudinal axis, having, between a front end and a rear end, a circular cylindrical wall delimiting a loading compartment containing a pyrotechnic charge, the ammunition body being sealed at its front end by the fuse and at its rear end by the skirt attached to the ammunition body. The ammunition body includes, in the loading compartment, between its two ends, a central core having n fins each comprising at least one edge, in the axis of revolution, attached to the skirt, n being greater than or equal to 1, to separate the pyrotechnic charge into at least two portions on either side of a given fin Ei. Applications are to cannon or mortar type ammunition.

Abstract: A self-propelled munition having a munition rear body of circular cylindrical shape of diameter D1, along axis ZZ?. A propulsion system of the munition has a tubular casing of circular cross section, has an axis of revolution coincident with axis ZZ?, has an internal surface of diameter D1 able to slide over said munition rear body, and contains a pyrotechnic propulsion chamber. The munition includes a mechanical connection between the propulsion system and the munition using shear pins evenly distributed about axis ZZ?, a hardened mechanical connection having a ring groove around the munition rear body in a plane perpendicular to axis ZZ?, another ring groove on the internal surface of the propulsion system casing, a retaining ring inserted in the ring groove configured to expand into the other ring groove from diameter D1 to a diameter greater than diameter D1 to secure the propulsion system to the munition.

Abstract: Embodiments of the invention relate to a safety lighter intended to initiate the combustion of a pyrotechnic device, the lighter including a lighter body (10) having a cylindrical void (12) of axis XX?, and a pyrotechnic slide-in module (14) including pyrotechnic means (70, 74, 30) of initiating the combustion of the pyrotechnic device, the pyrotechnic slide-in module (14) being able to be displaced in the cylindrical void, from a so-called safety position (Ps), providing isolation between the pyrotechnic means of the slide-in module and the pyrotechnic device to be initiated, to a so-called initiation position (Pi), intended to provoke the combustion of the pyrotechnic device.

Abstract: A device for opening and locking a tail unit is provided. The tail unit includes a body and at least one fin, pivotable relative to the body along a first axis, that has a projection that forms an element. The device comprises a control ring, slidable relative to the body along a second axis, that includes a component, forming an element, that bears against the projection to deploy the fin, the second axis being non-parallel and non-secant to the first axis. A means for shaping one of the elements during translation along the second axis of the control ring towards the projection of the fin is provided on the other element. The body includes a bearing surface to support the fin during shaping, in which the support of the fin on the bearing surface corresponds to the deployed position of the fin.

Abstract: Embodiments of the invention relate to a safety lighter intended to initiate the combustion of a pyrotechnic device, the lighter including a lighter body (10) having a cylindrical void (12) of axis XX?, and a pyrotechnic slide-in module (14) including pyrotechnic means (70, 74, 30) of initiating the combustion of the pyrotechnic device, the pyrotechnic slide-in module (14) being able to be displaced in the cylindrical void, from a so-called safety position (Ps), providing isolation between the pyrotechnic means of the slide-in module and the pyrotechnic device to be initiated, to a so-called initiation position (Pi), intended to provoke the combustion of the pyrotechnic device.

Abstract: The invention relates to techniques used to transport artillery-type autonomous weapons, such as cannons or mortars. The invention can be used to transport a heavy weapon on the rear deck of a light all-terrain vehicle. The interface (3, 4) between the vehicle (2) and the weapon (1) comprises a retractable structure (3), e.g. a fork crane (30), a cable (32) and an electrical winch (31). When retracted, the retractable structure is designed to form a mechanical connection between the vehicle and the weapon, and, when released, said structure is configured to enable the weapon to move in relation to the vehicle, such that the stresses produced with the launch of a missile are not transmitted to the vehicle. Moreover, when the retractable structure is in the released position, the weapon can be moved away from the vehicle while remaining connected thereto and, in the retracted position, the structure can be used to position the weapon precisely on the vehicle.