Pod-borne laser weapon

Abstract

The invention relates to a laser weapon (1) comprising a pod (15), means for orienting said pod, and at least one laser effector (2) that emits a laser beam, said laser effector successively comprising, in the direction of propagation of the laser beam, a laser source, first optical deflection means, which are able to deflect the laser beam, and a lens for focusing the laser beam, said lens being supported by the pod. The laser weapon (1) also comprises control means that control the means for orienting the pod and the first optical deflection means of the laser effector. The laser effector comprises second optical deflection means able to deflect the laser beam, said second optical deflection means being supported by the pod (15) and positioned after the lens in the direction of propagation of the laser beam, said second optical deflection means being controlled by the control means.

Description

Laser weapon carried by a pod Field of invention

[0001] The field of invention is that of weaponry, and more precisely weapons emitting a powerful laser beam enabling the destruction of a target. Prior art

[0002] Flying objects, such as drones, can pose numerous security challenges. They can be used by armed forces, in a conflict context, for intelligence purposes, or carry weapons or explosive charges and be used for aggressive purposes. Security forces must therefore have the capacity to destroy such flying objects that could pose threats. Due to the small size, agility, and low cost of such flying objects, allowing their deployment in large numbers, the weapons traditionally used for anti-aircraft warfare often prove inadequate. New weapons systems, specifically adapted to the destruction of such flying objects, have therefore been developed.

[0003] A weapon has been proposed that allows a powerful laser beam to be focused on a flying object. This laser beam, by heating a point on the flying object, can cause its destruction.

[0004] The destruction of a flying object by such a laser beam requires a duration of the order of ten seconds, during which the beam must be focused on the same point of the flying object. An adaptation of the characteristics of the laser beam, and in particular of its power, makes it possible to reduce this duration but it has been found that, beyond a certain power level, it is no longer profitable to obtain a significant reduction in this duration necessary for the destruction of a flying object by an additional increase in the power emitted.

[0005] This relatively long time during which the laser weapon must be focused on a single flying object can lead to difficulties in the event of a simultaneous threat from a plurality of flying objects. In such a case, the weapon will have to destroy each of the flying objects in succession and will, in some cases, be unable to destroy them all.

[0006] To facilitate the successive destruction of several flying objects, it is desirable for the laser weapon to be able to move very quickly from one target to another. The means of directing the laser beam to focus it on a target must therefore be extremely responsive and efficient.

[0007] To further increase the destructive capacity of multiple flying objects, it is possible to multiply the number of deployed laser weapons. However, such a solution involves high costs.

[0008] The present invention aims to overcome these drawbacks of the prior art.

[0009] In particular, an objective of the invention is to provide such a laser weapon whose effectiveness is improved compared to the solutions of the prior art.

[0010] A particular objective, for at least some of the embodiments, is to provide such a laser weapon in which the systems for directing the laser beam to point and focus that laser beam on a target are improved.

[0011] Another objective, for at least some of the embodiments, is to provide such a laser weapon whose effectiveness in simultaneously and / or successively neutralizing several targets is improved.

[0012] Another objective, for at least some of the embodiments, is to provide such a laser weapon whose production, implementation and / or operating cost can be reduced, compared to the solutions of the prior art.

[0013] These objectives, as well as others which will appear more clearly later, are achieved using a laser weapon comprising a nacelle, means for orienting this nacelle, and at least one laser effector capable of emitting a laser beam, the laser effector successively comprising, in the direction of propagation of the laser beam: a laser source, first optical deflection means, capable of deflecting the laser beam, an objective capable of focusing the laser beam, this objective being carried by the nacelle, this laser weapon comprising control means controlling the means for orienting the nacelle and said first optical deflection means of said laser effector.According to the invention, this laser effector comprises second optical deflection means capable of deflecting the laser beam, these second optical deflection means being carried by the nacelle and placed after the objective, in the direction of propagation of the laser beam, these second optical deflection means being controlled by the control means.

[0014] With the second optical deflection means, the output laser beam emitted by the laser effector can be oriented relative to the position of the pod, over significant angular ranges. The laser weapon thus has faster, more efficient and reliable means for pointing the output laser beam towards a target. Furthermore, since the orientation of the laser beam can vary relative to the direction of the pod, this pod can carry other weapons, or other laser effectors, which can be pointed towards different targets.

[0015] Preferably, the second optical deflection means are capable of allowing controlled deflection of the beam over an angular range greater than 3°, and preferably greater than 5°, and even more preferably greater than 10°.

[0016] The angular range is considered, in the present application, as the maximum angle formed between two possible orientations of the beam. This angular range is preferably centered on the optical axis of the beam leaving the objective, which is called, in the present application, "optical axis of the objective". Furthermore, this angular range preferably allows a deflection of the beam in all directions, around the optical axis of the objective. In certain cases, it is even possible to obtain a controlled deflection of the beam of several tens of degrees. Such a significant deviation allows the beam to be oriented towards targets, independently of the position of the nacelle.

[0017] Preferably, the first optical deflection means are capable of allowing controlled deflection of the beam over an angular range of less than 5 milliradians.

[0018] This deviation must be of low amplitude so as not to disturb the passage of the beam in the objective. Such a deviation can however be obtained very quickly and precisely.

[0019] According to an advantageous embodiment, these second optical deflection means comprise several prismatic blades capable of rotating around the optical axis of the objective.

[0020] Such deflection means are known in particular as diasporameter, or Risley prisms. The rotation of the prismatic blades+ can easily be motorized, in order to easily and quickly obtain a controlled deflection of a beam.

[0021] According to another possible embodiment, these second optical deflection means may comprise one or more mobile reflectors.

[0022] Such optical deflection means comprising movable mirrors can allow beam deflections of very large amplitude, for example of several tens of degrees.

[0023] According to an advantageous embodiment, the laser effector comprises an optical fiber capable of conducting the laser beam between the laser source and the first deflection means.

[0024] In this case, advantageously, the first deflection means of the laser effector are carried by the nacelle, and the laser source of the laser effector is placed outside the nacelle.

[0025] Such a solution has the particular advantage of allowing a reduction in the mass and volume of the nacelle.

[0026] According to an advantageous embodiment, the means for orienting the nacelle comprise a turret carrying the nacelle, this turret being capable of pivoting the nacelle around two axes perpendicular to each other.

[0027] Such a turret is commonly used to orient a nacelle quickly and efficiently. This nacelle can carry, in addition to the laser effector, other elements such as, for example, weapons or sensors, which can be oriented by the nacelle. In this case, the beam emitted by the laser effector can be oriented in a direction independent of the orientation of these weapons or sensors, thanks to the second optical deflection means.

[0028] According to a particularly advantageous embodiment, the laser weapon comprises at least two distinct laser effectors, each of these laser effectors comprising at least one objective carried by the nacelle, at least one of these laser effectors comprising the second means of optical deflection of the beam.

[0029] These second optical beam deflection means allow the different laser effectors, carried by the same nacelle, to be able to be pointed in independent directions and aim at distinct targets. Preferably, the distinct laser effectors each have first and second optical beam deflection means as described above. It should be noted, however, that these distinct laser effectors may, in certain configurations, share certain components, for example share the same laser source. They are nevertheless considered distinct to the extent that they allow distinct beams to be emitted.

[0030] Advantageously, the objectives of the separate laser effectors are oriented, on said nacelle, along optical axes which are not parallel to each other.

[0031] The overall angular range in which the different laser effectors carried by the same nacelle can emit laser beams is thus increased. Description of figures

[0032] The invention will be better understood upon reading the following description of preferred embodiments, given as a simple figurative and non-limiting example, and accompanied by the figures among which: La is a schematic representation of a laser weapon according to a possible embodiment of the invention. La is a diagram schematically representing the components of the laser weapon of the. La is a diagram schematically representing the components of the laser effector of the laser weapon of the. La is a schematic representation of a laser weapon according to another possible embodiment of the invention. La is a schematic representation of a laser weapon according to yet another possible embodiment of the invention. Detailed description of embodiments of the invention

[0033] The figure represents in perspective a laser weapon 1 according to an embodiment of the invention, the main components of which are represented schematically by the diagram of the figure.

[0034] This laser weapon 1 comprises an orientable nacelle 15, which carries some of the components of the laser weapon 1. This nacelle is controlled, that is to say that its orientation can be modified in response to instructions from control means. In the embodiment represented by 1a, this nacelle 15 is constituted by a metal housing. In other possible embodiments, a nacelle according to the invention can be constituted by any support which can be oriented in different directions, and capable of carrying at least part of a laser effector.

[0035] This nacelle 15 is advantageously carried by an articulated turret 14 which makes it possible to orient the nacelle 15 in a desired direction, in response to instructions from control means. In the embodiment shown, the turret 14 is articulated along two axes: a substantially vertical axis 141 and a substantially horizontal axis 142. It thus makes it possible to vary the orientation of the nacelle 15 which it carries, relative to the support on which the turret 14 is fixed, in all directions of space.

[0036] The movements of the components of the turret 14 are advantageously controlled by servomotors capable of rapidly modifying the angular position of the nacelle 15, in response to instructions from control means. The turret 14 thus makes it possible to modify the orientation of the nacelle 15 in a fairly reactive and efficient manner with a very large angular amplitude. These movements of the components of the turret 14, of the nacelle 15 and of the components carried by this nacelle 15, however, involve significant inertial forces, due to the masses of these components. These inertial forces impose a limitation on the speed of the movements of the nacelle.

[0037] The nacelle 15 carries, according to the invention, at least part of a laser effector 2, capable of emitting a focused laser beam capable of damaging or destroying a distant target.

[0038] The movements of the components of the turret 14, by modifying the orientation of the nacelle 15, thus make it possible to modify the orientation of the focused laser beam emitted by the laser effector 2, with a very large angular amplitude, in order to orient this focused laser beam in the direction of its target. Thus, for information purposes, the precision of the orientation of the nacelle obtained by the movements of the components of the turret is generally of the order of a few hundredths of a milliradian.

[0039] The precision of the orientation obtained by the movements of the components of the turret 14 is however insufficient to ensure the precise pointing of the beam emitted by the laser effector 2 on a small target located several hundred meters away.

[0040] The laser effector 2 is itself composed of several components which are represented schematically by: a laser source 21 emits an initial laser beam 210, first optical deflection means 22 orient this initial laser beam 210, an objective 23 focuses this initial laser beam 210, to form the focused laser beam 230, second optical deflection means 24 orient the focused laser beam 230 to form the output laser beam 240.

[0041] The laser source 21 which emits the initial laser beam 210 may comprise a laser diode or any laser cavity capable of producing a beam and, where appropriate, one or more amplifiers capable of amplifying this beam. Such a laser source is well known to those skilled in the art. It is advantageously controlled, that is to say it emits a laser beam having desired characteristics in response to instructions from control means.

[0042] Advantageously, the laser source 21 may be configured to emit the initial laser beam 210 into an optical fiber, which can easily transport the initial laser beam 210.

[0043] Thanks to such an optical fiber, the laser source 21 can be moved away from the other components of the laser effector 2. It is thus possible, for example, that the majority of the components of the laser effector 2 are carried by the nacelle 15, while the laser source 21 is placed outside the nacelle 15. In such a case, the laser source 21 is connected to the other components of the laser effector 2 by the optical fiber.

[0044] According to the invention, the initial laser beam 210 passes through first optical deflection means 22 before being focused by the objective 23. These first optical deflection means 22 are advantageously designed to precisely orient the output laser beam 240 within a restricted angular range. They are advantageously controlled, that is to say they make it possible to vary the orientation of the output laser beam 240 in response to instructions from control means.

[0045] These first optical deflection means 22 may for example consist of a diasporameter, or Risley prisms, composed of several prismatic blades which can pivot relative to each other around the optical axis. Such optical deflection means are known, in themselves, for the orientation of laser beams.

[0046] In another possible embodiment, these first optical deflection means 22 may form an optical device for changing the direction of propagation of a light beam which comprises, in the direction of propagation of the light beam, a generally divergent lens group and a generally convergent lens group, the generally divergent lens group containing, in the direction of propagation of the light beam, a fixed lens and an optical module comprising at least one movable optical element capable of modifying the direction of propagation of the light beam emerging from the generally divergent lens group. Such optical devices are known to those skilled in the art and are described, for example, in document FR3064758A1.

[0047] In such a case, the first optical deflection means 22 may have the effect of angularly deflecting the initial laser beam 210 before its introduction into the objective 23, and / or of shifting the initial laser beam 210 from the optical axis of the objective 23. In both cases, the first optical deflection means 22 have the effect of angularly deflecting the focused laser beam 230 exiting the objective 23, and therefore the output laser beam 240.

[0048] Such an angular deviation of the output laser beam 240 can be obtained by the first optical deflection means 22 as a function of a command from the control means, very precisely and with very high responsiveness. Indeed, the initial laser beam 210 is advantageously of small diameter. The mobile optical components of the first optical deflection means 22 can therefore be of small size, and have only very low inertia during their movements. It is thus possible to move them very quickly.

[0049] On the other hand, the angular deviation of the output laser beam 240 obtained by the first optical deflection means 22 can only have a very limited amplitude. Indeed, a deviation of too high an amplitude would not allow the correct passage of the initial laser beam 210 into the objective 23. By way of illustration, such first optical deflection means 22 can allow the output laser beam 240 to be deflected by an angle of the order of a milliradian, with an accuracy of the order of a hundredth of a milliradian.

[0050] The combination of the controlled orientation of the nacelle 15 by the turret 14, of very large amplitude but relatively imprecise and relatively unresponsive, and the controlled deflection, by the first optical deflection means 22, of the focused laser beam 230 relative to the nacelle 15, of small amplitude but very precise and very responsive, allows in practice the laser weapon 1 to point, over a large angular amplitude but in a very precise manner, the output laser beam 240 emitted by the laser effector 2, so that it reaches a distant and small moving target.

[0051] After passing through the first optical deflection means 22, the laser beam passes through an objective 23, which is composed of a succession of lenses capable of focusing the output laser beam 240 at a desired distance. The operation of such an objective is known, in itself, to those skilled in the art. The lenses composing this objective are preferably movable relative to each other in order to allow adjustment of the focal length of the objective as a function of the distance of the target on which the beam is to be focused. This objective is advantageously controlled, that is to say it makes it possible to give the beam variable focusing characteristics in response to instructions from control means.

[0052] In order for this focused laser beam 230 to be able to be focused on a distant point, it preferably has a diameter much greater than the diameter of the initial laser beam 210.

[0053] According to the invention, provision is made to add, at the output of the objective 23, second optical beam deflection means 24 capable of modifying the orientation of the focused laser beam 230. These second optical beam deflection means 24 are advantageously controlled, that is to say they make it possible to vary the orientation of the output laser beam 240 in response to instructions from control means.

[0054] As indicated above, these second optical deflection means 24 are generally not necessary to orient the focused laser beam 230. Indeed, the combination of the movements of the turret 14 and the first optical deflection means 22 is generally sufficient to orient this focused laser beam 230 over a large angular range and with great precision, in order to reach its target.

[0055] These second optical deflection means 24 may for example consist of a diasporameter, or Risley prisms, composed of two prismatic blades which can pivot, one relative to the other around the optical axis. Such deflection means are known, in themselves, to allow the controlled deflection of a beam.

[0056] According to another possible embodiment, these second optical deflection means may consist of a set of reflectors movable relative to each other, for example movable mirrors, the position of which is controlled. It is also possible for these second optical deflection means to comprise a combination of several components of different types, for example pivoting prismatic blades and movable mirrors.

[0057] These second optical deflection means 24 are advantageously designed to allow a deviation amplitude of the output beam 240, relative to the optical axis of the objective, of an angle α greater than 3°, and preferably greater than 5°. It is even possible, in preferred embodiments, for these second optical deflection means to allow a deviation amplitude of the output beam 240 of an angle α greater than 10 or 20°.

[0058] These second optical deflection means 24 being advantageously located after all the optics shaping the laser beam, they can have a significant deflection angle without this inducing any penalizing distortion on the output beam 240.

[0059] The laser weapon 1 advantageously comprises a detection and aiming system 11. Such a detection and aiming system 11, which is known per se, may comprise, for example, one or more radars, one or more LIDARs and one or more cameras. It makes it possible to detect potential targets, to precisely measure their position and to track this position. This detection and aiming system 11 may be associated with a human-machine interface 12 which may, for example, allow an operator to view the potential targets on a screen. The operator can thus choose whether he wishes to destroy one of these targets.

[0060] Furthermore, this detection and pointing system may comprise the control means capable of controlling the laser source 21, the first optical deflection means 22, the objective 23 and the second optical deflection means 24.

[0061] In the embodiment shown, at least some of the sensors of the detection and pointing system 11 are carried by the nacelle 15. It is however possible that other components of this detection and pointing system 11 are not carried by the nacelle 15. In other embodiments, it is also possible that none of the components of the detection and pointing system 11 are carried by the nacelle 15. This detection and pointing system 11 then operates independently of the position of the nacelle 15.

[0062] If the operator so requests, through the human-machine interface, the detection and pointing system 11 can point the laser effector 2 in the direction of a target, in order to allow this laser effector 2 to emit a laser beam focused on this target, with a view to destroying it. For this, the detection and pointing system 11 comprises control means controlling the movements of the turret 14, the first optical deflection means 22, the objective 23 and the second optical deflection means 24, in order to obtain a pointing of the output laser beam 240 focused on the target.

[0063] The combination of the movements of the nacelle 15, thanks to the turret 14, and the beam deflections by the first optical deflection means 22 and the second optical deflection means 24 makes it possible to obtain several advantages.

[0064] Thus, the detection and pointing system 11 which controls these different means of orientation of the output beam, can both modify the direction of the laser beam over a large angular amplitude, in particular using the movements of the nacelle 15, and correct, in particular using the first more precise optical deflection means, the high uncertainties linked to the orientation of the nacelle 15 by the turret 14, in order to ensure the precise pointing of the target.

[0065] Furthermore, the combination of the means for orienting the output laser beam 240 provided by the turret 14 and by the second optical deflection means 24 advantageously makes it possible to improve the time of a significant angular displacement of the output laser beam 240, for example to pass from one target to another, and therefore to optimize the time of successive destruction of several targets by the laser weapon.

[0066] The second optical deflection means 24, which are placed on a focused laser beam 230 of large diameter, are formed by components whose size, and therefore weight, are relatively large. These components thus have, when they are set in motion, a greater inertia than the smaller components of the first optical deflection means 22. Consequently, these second optical deflection means 24 have a longer reaction time than the first optical deflection means 22. This reaction time is however shorter than that of the turret 14, which makes it possible to reduce the overall reaction time of the laser weapon 1, for example to move from one target to another.

[0067] Finally, the combination of these three means of orientation of the output laser beam 240 makes it possible to improve the reliability of the laser weapon, in particular by allowing the orientation of the laser beam even in a degraded situation in which a malfunction of the turret 14 would reduce its precision or its orientation speed, or even prevent any movement of the nacelle 15. The second optical deflection means 24, by allowing an orientation of the output laser beam 240 relative to the position of the nacelle 15, over a relatively large amplitude, would allow the laser weapon 1 to continue to destroy targets.

[0068] Schematically represents a laser weapon 3 according to another possible embodiment of the invention.

[0069] This laser weapon comprises a steerable nacelle 15, which is carried by an articulated turret 14. This nacelle and this turret are advantageously identical or almost identical to those of the laser weapon 1 presented previously. This nacelle 15 carries, in the embodiment shown, two separate laser effectors 201 and 202. At least a first of these laser effectors 201 is of the type represented by 1a, and comprises a laser source, first optical deflection means, a lens, and second optical deflection means. Thus, the output laser beam emitted by this laser effector can be oriented, in particular by the second deflection means, independently of the movements of the nacelle 15.

[0070] The second laser effector 202 may, in certain embodiments, not have second optical deflection means. In such a case, the orientation of the output beam emitted by this second laser effector is solely achieved by the combination of the orientation means provided by the turret, which ensure its orientation over a large angular range, and by the second optical deflection means which ensure its precise orientation over a small angular range.

[0071] However, preferably, the second laser effector 202 is, like the first laser effector 201, of the type represented by 1a, and comprises a laser source, first optical deflection means, a lens, and second optical deflection means. Thus, each of the two laser effectors can emit a laser beam that can be steered relative to its positioning axis on the nacelle, over an angular range of more than 6°, and preferably more than 10°.

[0072] According to a preferred solution, the optical axes of the first laser effector 201 and the second laser effector 202 may not be parallel, but on the contrary form an angle which may, advantageously, be from 10° to 20°. Thanks to the optical deflection means, each of the laser effectors can orient its beam in an angular zone centered on its optical axis, for a given position of the nacelle. Due to the divergences of the beams, the angular zones of the first laser effector 201 and the second laser effector 202 do not overlap, but are neighboring, which makes it possible to simultaneously target several targets distant from each other. It is however advantageous for these angular zones to partially overlap.Thus, if the nacelle 15 is positioned such that a target is placed in the overlapping area of ​​the angular areas of several laser effectors, these laser effectors can simultaneously target the same target, which can facilitate its destruction.

[0073] The laser weapon 3 advantageously comprises a detection and pointing system 31 similar to the detection and pointing system 11 described previously, which makes it possible to detect potential targets, to precisely measure their position and to track this position. In this embodiment, the detection and pointing system 31 comprises control means capable of controlling the orientation means of the nacelle 15 and the laser source, the first optical deflection means, the objective and the second optical deflection means of each of the laser effectors 201 and 202.

[0074] When this detection and pointing system 31 detects several targets simultaneously, it can place the nacelle 15 in a position chosen to allow each of the laser effectors 201 and 202 to be pointed towards one of the targets, taking into account the possible deviation amplitudes of each of these laser effectors. If possible, this position of the nacelle is chosen such that each of the output beams emitted by one of the laser effectors 201 and 202 can be moved around its line of sight, in order to follow its target.

[0075] The detection and pointing system 31 then controls the second optical deflection means of the first laser effector 201, and where appropriate those of the second laser effector 202, to orient their beams towards the distinct targets. The detection and pointing system 31 finally controls the first optical deflection means of each of the laser effectors 201 and 202, to precisely point their beams towards distinct targets.

[0076] Like the detection and pointing system 11, the detection and pointing system 31 can be associated with a human-machine interface to allow an operator to decide on the destruction of each of the targets.

[0077] The independence of the orientation of each of the beams emitted by the first and second laser effectors, thanks to the second optical deflection means with which at least one of these laser effectors is equipped, therefore allows the laser weapon 3 to destroy or damage several targets simultaneously. Such a weapon is therefore significantly more effective, for example, against a coordinated attack by several drones. However, such a weapon involves a lower cost than a combination of two laser weapons of the type represented by the. Indeed, the cost of the turret 14 and of the possible carrier vehicle represents a significant part of the cost price of such a laser weapon.

[0078] In other possible embodiments, it is also possible to have more than two laser effectors carried by the same steerable nacelle, which will make it possible to simultaneously target a greater number of targets, if these laser effectors can be steered independently of each other. The optical axes of the objectives of these laser effectors may advantageously not be parallel to each other.

[0079] In yet another possible embodiment, it is also possible to have one or more laser effectors and one or more conventional weapons carried by the same steerable nacelle.

[0080] Thus, by way of example, the represents a laser weapon 4 comprising an orientable nacelle 15, which is carried by an articulated turret 14. This nacelle and this turret are advantageously identical or almost identical to those of the laser weapon 1 presented previously. This nacelle 15 carries, in the embodiment shown, a laser effector 2, which is advantageously identical to that represented by the. This laser effector 2 thus comprises a laser source, first optical deflection means, a lens, and second optical deflection means. Thus, the laser beam emitted by this laser effector 2 can be oriented, in particular by the second deflection means, independently of the movements of the nacelle 15.

[0081] This nacelle also carries a conventional weapon 5, such as a machine gun. Advantageously, this conventional weapon 5 can be pointed towards its target by the movements of the nacelle 15. The laser beam emitted by the laser effector 2 can be oriented independently of the movements of the nacelle 15, this laser effector 2 and the conventional weapon 5 can be simultaneously pointed towards two separate targets.

Claims

Laser weapon (1, 3, 4) comprising a gondola (15), means for orienting said gondola, and at least one laser effector (2) capable of emitting a laser beam, said laser effector (2) comprising successively, in the direction of propagation of said laser beam: a laser source (21), first optical deflection means (22) capable of deflecting said laser beam, a lens (23) capable of focusing said laser beam, said lens (23) being carried by said gondola (15), said laser weapon (1, 3) comprising control means controlling said means for orienting said gondola and said first optical deflection means (22) of said laser effector (2), characterized in that said laser effector (2) comprises second optical deflection means (24) capable of deflecting said laser beam, said second optical deflection means (24) being carried by said gondola (15) and placed after said objective (23), in the direction of propagation of said laser beam,said second optical deflection means (24) being controlled by said control means. Laser weapon according to the preceding claim, characterized in that said second optical deflection means (24) are capable of allowing a controlled deflection of said laser beam of an angle greater than 3°, and preferably greater than 5°, and even more preferably greater than 10°. Laser weapon according to any one of the preceding claims, characterized in that said first optical deflection means (22) are capable of permitting a controlled deflection of said beam over an angular range of less than 5 milliradians. Laser weapon according to any one of the preceding claims, characterized in that said second optical deflection means (24) comprise several prismatic blades capable of rotating around the optical axis of said objective (23). Laser weapon according to any one of the preceding claims, characterized in that said second optical deflection means (24) comprise one or more movable reflectors. Laser weapon according to any one of the preceding claims, characterized in that said laser effector (2) comprises an optical fiber capable of conducting said laser beam between said laser source (21) and said first optical deflection means (22). Laser weapon according to the preceding claim, characterized in that said first optical means for deflecting said laser effector (2) are carried by said nacelle (15), and in that said laser source (21) of said laser effector (2) is placed outside said nacelle (15). Laser weapon according to any one of the preceding claims, characterized in that said orienting means of said gondola comprise a turret (14) carrying said gondola (15), said turret (14) being capable of rotating said gondola (15) around two axes (141, 142) perpendicular to each other. Laser weapon (3) according to any one of the preceding claims, characterized in that it comprises at least two separate laser effectors (201, 202), each of said laser effectors (201, 202) comprising at least one objective (23) carried by said pod (15), at least one of said laser effectors (201, 202) comprising said second optical means for deflecting the beam (22). Laser weapon according to the preceding claim, characterized in that said objectives of said separate laser effectors (201, 202) are oriented, on said nacelle (15), along optical axes not parallel to each other.

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