JP2018151125A - Electromagnetic pulse projectile and irradiation method of electromagnetic pulse of electromagnetic pulse projectile - Google Patents

Abstract

PROBLEM TO BE SOLVED: To provide an electromagnetic pulse projectile capable of radiating an electromagnetic pulse over a wide range, and an irradiation method of the electromagnetic pulse of the electromagnetic pulse projectile.SOLUTION: In the electromagnetic pulse projectile, an irradiation axis of an electromagnetic pulse in an electromagnetic pulse irradiation part of a projectile body is tilted relative to a projectile axis of the projectile body and the irradiation axis is spun in a final stage of flying. The electromagnetic pulse projectile spins the irradiation axis by rotating the projectile body. The electromagnetic pulse projectile spins the irradiation axis by rotating the electromagnetic pulse irradiation part. In the irradiation method of the electromagnetic pulse of the electromagnetic pulse projectile, the electromagnetic pulse is radiated while spinning the irradiation axis of the electromagnetic pulse in a final stage of flying of the electromagnetic pulse projectile.SELECTED DRAWING: Figure 1

Description

  The present invention relates to an electromagnetic pulse (EMP) bullet and an electromagnetic pulse irradiation method of an electromagnetic pulse bullet. In more detail, this invention relates to the irradiation method of the electromagnetic pulse of an electromagnetic pulse bullet and the electromagnetic pulse bullet which can expand the effective range of an electromagnetic pulse.

  Conventionally, in an electromagnetic pulse bullet, an antenna for irradiating an electromagnetic pulse is attached in parallel to the bullet axis of the bullet. Therefore, the irradiation axis of the electromagnetic pulse is parallel to the bullet axis of the bullet.

  Here, a conventional electromagnetic pulse bullet will be described with reference to the drawings. FIG. 6 is an explanatory view showing an outline of a conventional electromagnetic pulse bullet. As shown in FIG. 6, a conventional electromagnetic pulse bullet 100 includes a bullet body 10 and an electromagnetic pulse generator 20 that is disposed on the bullet body 10 and has an electromagnetic pulse irradiation unit 21. The electromagnetic pulse irradiation unit 21 such as an antenna is attached so that the irradiation axis Ea of the electromagnetic pulse E in the electromagnetic pulse irradiation unit 21 is parallel to the bullet axis 10 a of the bullet 10. In the figure, an arrow Z indicates the traveling direction of the electromagnetic pulse bullet 100. In the figure, θ represents the irradiation angle range of the electromagnetic pulse E.

Moreover, FIG. 7 is explanatory drawing which shows an example of the effective range of the electromagnetic pulse of the conventional electromagnetic pulse bullet. As shown in FIG. 7, in the conventional electromagnetic pulse bombs, potency range R _E which irradiation effects of electromagnetic pulse can be expected is only the peripheral region of the point of impact P.

  Conventionally, the functions of the electronic devices that make up the nervous system of weapons can be destroyed with a small number of small caliber bullets and without substantially damaging personnel without requiring a very high accuracy. Has been proposed. This bullet (electromagnetic bullet) has a bullet that forms the outer shell of the bullet, a fusible tube, an explosive filled, and is arranged coaxially with the bullet within the bullet and axially between the bullet wall A metal cylinder forming a long ring-shaped space, a power source arranged in the space, a switch that is closed by a pressure generated when the fuse is ignited or ignited, and the metal cylinder surrounding the ring-shaped space Coaxially with the cylinder and in an insulated state with the cylinder and the bullet, the one end is connected to the bullet via the power source and the switch in series, and the other end is directly connected to the bullet And a coiled conductor that forms a closed circuit together with a power source, a switch, and a bullet. The bullet circulates current in the closed circuit by closing the switch when the fuze is ignited or ignited, and the power is supplied to the cylinder by the explosion of the explosive in the metal cylinder following the igniting of the fuze. In addition, the conductor is inflated from the switch side toward the other end, the conductor is pushed outward, the current from the power source side is brought into contact with the wall of the bullet body in order to change the current flowing through the bullet, and electromagnetic waves are radiated from the bullet ( (See Patent Document 1).

JP 63-148097 A

  However, the conventional electromagnetic pulse bullet described in Patent Document 1 has a problem that the electromagnetic pulse irradiation effect can be expected only in a narrow region including the impact point.

  The present invention has been made in view of such problems of the prior art. An object of the present invention is to provide an electromagnetic pulse bullet that can irradiate an electromagnetic pulse over a wide range and an electromagnetic pulse irradiation method of the electromagnetic pulse bullet.

  The inventors of the present invention have made extensive studies in order to achieve the above object. As a result, the irradiation axis of the electromagnetic pulse in the electromagnetic pulse irradiation part of the bullet is tilted with respect to the bullet axis of the bullet, and the above object can be achieved by rotating the irradiation axis at the final stage of flight. As a result, the present invention has been completed.

  That is, in the electromagnetic pulse bullet according to claim 1, the irradiation axis of the electromagnetic pulse in the electromagnetic pulse irradiation part of the bullet is inclined with respect to the bullet axis of the bullet, and the irradiation axis is rotated at the final stage of the flight. It is characterized by.

  The electromagnetic pulse bullet according to claim 2 is characterized in that, in claim 1, the irradiation axis is rotated by rotating the bullet.

  Furthermore, the electromagnetic pulse bullet according to claim 3 is characterized in that the irradiation axis is rotated by rotating the electromagnetic pulse irradiation part in claim 1 or claim 2.

  The electromagnetic pulse irradiation method of the electromagnetic pulse bullet according to claim 4 is characterized in that the electromagnetic pulse is irradiated while rotating the irradiation axis of the electromagnetic pulse at the final stage of the flight of the electromagnetic pulse bullet.

  According to the first aspect of the present invention, the electromagnetic pulse can be irradiated over a wide range in the electromagnetic pulse bullet. In addition, there is a secondary advantage that the effect of electromagnetic pulses can be obtained even if the target impact point deviates.

  According to the second aspect of the present invention, the electromagnetic pulse can be irradiated over a wide range in the electromagnetic pulse bullet by a simple control that the number of components is relatively small and the bullet is rotated. In addition, there is a secondary advantage that the effect of electromagnetic pulses can be obtained even if the target impact point deviates.

  According to the invention of claim 3, the electromagnetic pulse can be irradiated over a wide range in the electromagnetic pulse bullet by a relatively simple control of rotating the electromagnetic pulse irradiation unit. In addition, there is a secondary advantage that the effect of electromagnetic pulses can be obtained even if the target impact point deviates.

  According to the invention according to claim 4, the electromagnetic pulse is irradiated over a wide range by irradiating the electromagnetic pulse while rotating the irradiation axis of the electromagnetic pulse at the final stage of the flight of the electromagnetic pulse bullet. be able to. In addition, there is a secondary advantage that the effect of electromagnetic pulses can be obtained even if the target impact point deviates.

FIG. 1 is an explanatory diagram showing an outline of an electromagnetic pulse bullet according to the first embodiment of the present invention. FIG. 2 is an explanatory diagram showing an example of the effective range of the electromagnetic pulse of the electromagnetic pulse bullet according to the first embodiment of the present invention. FIG. 3 is a flowchart showing an example of rotation control in the electromagnetic pulse bullet according to the first embodiment of the present invention. FIG. 4 is an explanatory diagram showing an outline of an electromagnetic pulse bullet according to the second embodiment of the present invention. FIG. 5 is an explanatory diagram showing an outline of an electromagnetic pulse bullet according to the third embodiment of the present invention. FIG. 6 is an explanatory view showing an outline of a conventional electromagnetic pulse bullet. FIG. 7 is an explanatory diagram showing an example of the effective range of electromagnetic pulses of a conventional electromagnetic pulse bullet.

  Hereinafter, an electromagnetic pulse bullet and an electromagnetic pulse irradiation method according to an embodiment of the present invention will be described in detail.

In the electromagnetic pulse bullet according to one embodiment of the present invention, the irradiation axis of the electromagnetic pulse in the electromagnetic pulse irradiation unit of the bullet is inclined with respect to the bullet axis of the bullet, and the irradiation axis is rotated at the final stage of the flight. It is.
By setting it as such a structure, an electromagnetic pulse can be irradiated over a wide range in an electromagnetic pulse bullet. In addition, there is a secondary advantage that the effect of electromagnetic pulses can be obtained even if the target impact point deviates.

Moreover, the suitable form of an electromagnetic pulse bullet rotates an irradiation axis | shaft by rotating a bullet body (for example, refer 1st or 2nd embodiment mentioned later).
With such a configuration, the electromagnetic pulse can be irradiated over a wide range in the electromagnetic pulse bullet by a simple control in which the number of parts is relatively small and the bullet is rotated. In addition, there is a secondary advantage that the effect of electromagnetic pulses can be obtained even if the target impact point deviates.

Furthermore, the suitable form of an electromagnetic pulse bullet rotates an irradiation axis | shaft by rotating an electromagnetic pulse irradiation part (for example, refer 3rd Embodiment mentioned later).
With such a configuration, the electromagnetic pulse can be irradiated over a wide range in the electromagnetic pulse bullet by relatively simple control of rotating the electromagnetic pulse irradiation unit. In addition, there is a secondary advantage that the effect of electromagnetic pulses can be obtained even if the target impact point deviates.

The electromagnetic pulse irradiation method of the electromagnetic pulse bullet according to the embodiment of the present invention is a method of applying an electromagnetic pulse while rotating the irradiation axis of the electromagnetic pulse at the final stage of the flight of the electromagnetic pulse bullet. Further, it is a method of irradiating an electromagnetic pulse while rotating the irradiation axis of the electromagnetic pulse continuously or intermittently at the final stage of the flight of the electromagnetic pulse bullet.
By setting it as such a structure, an electromagnetic pulse can be irradiated over a wide range in an electromagnetic pulse bullet. In addition, there is a secondary advantage that the effect of electromagnetic pulses can be obtained even if the target impact point deviates.

(First embodiment)
First, the electromagnetic pulse bullet according to the first embodiment will be described in detail with reference to the drawings. FIG. 1 is an explanatory diagram showing an outline of an electromagnetic pulse bullet according to the present embodiment. In addition, the dimension ratio of drawing is exaggerated on account of description, and may differ from an actual ratio.

  As shown in FIG. 1, the electromagnetic pulse bullet 1 of this embodiment includes a bullet body 10 and an electromagnetic pulse generator 20 that is disposed on the bullet body 10 and has an electromagnetic pulse irradiation unit 21. The electromagnetic pulse bullet 1 is arranged on the bullet 10 and is a wing that rotates the bullet 10 in the direction indicated by the arrow Y in the figure with respect to the bullet axis 10a of the bullet 10 at the final stage before the electromagnetic pulse irradiation. The turning means 30 is further provided. Although not shown, it goes without saying that the direction of rotation may be the direction opposite to the direction indicated by arrow Y in the figure. The electromagnetic pulse irradiation unit 21 such as an antenna is attached such that the irradiation axis Ea of the electromagnetic pulse E in the electromagnetic pulse irradiation unit 21 forms an angle with respect to the bullet axis 10 a of the bullet 10. In the figure, the arrow Z indicates the traveling direction of the electromagnetic pulse bullet 1. Although not particularly limited, the angle formed between the irradiation axis Ea of the electromagnetic pulse E and the bullet axis 10a of the bullet 10 is θ / 2 or θ which is half of the irradiation angle range θ of the electromagnetic pulse E. It is preferably less than / 2. Thereby, it can prevent thru | or suppress that the electromagnetic pulse E is not irradiated to the impact point P which is a center part.

  Here, in the present invention, “final stage before electromagnetic pulse irradiation” is a part of “final stage of flight”, for example, a stage prior to irradiation with electromagnetic pulses as in the conventional electromagnetic pulse bullet. Even when rotation control that may cause a deviation of the impact point is performed, the impact point of the electromagnetic pulse bullet is the same as the initially set impact point or the expected error range. Means a stage that can be maintained at a point within. Note that the final stage before the electromagnetic pulse irradiation is appropriately set according to the specifications and usage pattern of the electromagnetic pulse bullet, and can be determined by preliminary experiments or simulations. For example, although depending on the speed of the electromagnetic pulse bullets, the interval between the electromagnetic pulses, and the like, the rotation speed in the rotation control is preferably set to 2 to 3 Hz.

  As described above, it is further provided with a rotating means that is arranged on the bullet and rotates the bullet with respect to the bullet axis of the bullet in the final stage before the electromagnetic pulse irradiation, and the irradiation axis of the electromagnetic pulse in the electromagnetic pulse irradiation unit is The structure has an angle with respect to the bullet axis of the bullet. Therefore, compared with the conventional electromagnetic pulse bullet, the electromagnetic pulse can be irradiated over a wide range. In addition, there is a secondary advantage that the effect of electromagnetic pulses can be obtained even if the target impact point deviates.

  Here, FIG. 2 is an explanatory diagram showing an example of the effective range of the electromagnetic pulse of the electromagnetic pulse bullet of the present embodiment. As shown in FIG. 2, it can be seen that the electromagnetic pulse bullet of the present embodiment can irradiate the electromagnetic pulse over a wide range as compared with the conventional electromagnetic pulse bullet shown in FIG.

  Here, each configuration will be described in more detail.

  A conventionally known bullet can be applied as the bullet 10. Moreover, you may have wings, such as an engine, a stable wing | blade, a steering wing | blade. In addition, since it is an electromagnetic pulse bullet, it is preferable that some countermeasures against electrons are taken.

  As the electromagnetic pulse generator 20, a conventionally known electromagnetic pulse generator can be applied. A conventionally known antenna can also be applied to the electromagnetic pulse irradiation unit 21.

  Further, as the turning means 30, a wing arranged in a bullet as shown in the drawing can be applied. As described above, the bullet may have a wing such as a steering wing and can be used. By using the wings, the turning means can be constructed with a small number of parts. However, the present invention is not limited to this. For example, as described above, the bullet may have an engine, and therefore, it may further have an auxiliary engine and may be used.

  The electromagnetic pulse bullet 1 preferably further includes a control device 40 disposed on the bullet 10. Furthermore, the control device 40 preferably includes a position information acquisition unit 41, a final stage determination unit 42, and a turning means control unit 43.

  Here, each configuration will be described in more detail.

  The position information acquisition unit 41 is not particularly limited as long as it can acquire the position information of a bullet, and various conventionally known sensors and arithmetic devices can be used.

  The final stage determination unit 42 is not particularly limited as long as it can determine whether it is the final stage before electromagnetic pulse irradiation based on a signal from the position information acquisition unit. A known arithmetic unit can be used.

  Further, the turning means control unit 43 is not particularly limited as long as it can control the turning means based on the signal from the final stage determination unit. For example, the signal from the final stage determination unit For example, an electric motor that moves a rotating means such as a wing can be used based on an electric signal.

  FIG. 3 is a flowchart showing an example of rotation control in the electromagnetic pulse bullet of this embodiment. As shown in FIG. 3, in step 1 (hereinafter abbreviated as “S1”, the same applies hereinafter), the position information acquisition unit 41 acquires the position information of the bullet 10 and proceeds to S2.

  In S2, the final stage determination unit 42 determines whether it is the final stage before the electromagnetic pulse irradiation based on the signal from the position information acquisition unit 41, and determines that it is the final stage before the electromagnetic pulse irradiation ( If YES, the process proceeds to S3. If it is not determined that the final stage is before the electromagnetic pulse irradiation (NO), the process returns to S1.

  In S <b> 3, the turning means control unit 43 that has received a signal from the final stage determination unit 42 that it is the final stage before the electromagnetic pulse irradiation rotates to rotate the bullet 10 with respect to the bullet axis 10 a of the bullet 10. The final stage turning control which is the control of the means 30 is executed.

  Here, in the present invention, the “final stage rotation control” means that even if rotation control for the purpose of flight stability is performed as necessary before the final stage before the electromagnetic pulse irradiation, the electromagnetic pulse is controlled. After being judged as the final stage before irradiation, it means the rotation control for the purpose of expanding the effective range of the electromagnetic pulse.

As described above, the electromagnetic pulse bullet is placed on the bullet and is the final stage before the electromagnetic pulse irradiation based on the signal from the positional information acquisition unit and the positional information acquisition unit that acquires the positional information of the bullet. And a control device having a turning means control section for controlling the turning means based on a signal from the final stage judging section, and the turning means control section receives an electromagnetic pulse from the final stage judging section. When receiving a signal indicating that it is the final stage before irradiation, it is preferable to execute a final stage rotation control that is a control of a turning means for rotating the bullet with respect to the bullet axis of the bullet. .
By setting it as such a structure, an electromagnetic pulse can be irradiated over a wide range in an electromagnetic pulse bullet by controlling a rotation means based on the positional information acquired by the simple method. In addition, there is a secondary advantage that the effect of electromagnetic pulses can be obtained even if the target impact point deviates.

  In addition, when the electromagnetic pulse bullets fly at a predetermined landing point at a predetermined flight speed or flight path, the flight time of the bullet may be acquired when acquiring the position information of the bullet. Thereby, it becomes a very simple control device, and the turning means can be controlled with a small number of parts.

That is, it is preferable that the position information acquisition unit acquires the position information of the bullet according to the flight time of the bullet.
By adopting such a configuration, it is possible to irradiate the electromagnetic pulse over a wide range in the electromagnetic pulse bullet by controlling the turning means based on the position information acquired by a simple method such as measuring the flight time. it can. In addition, there is a secondary advantage that the effect of electromagnetic pulses can be obtained even if the target impact point deviates.

(Second Embodiment)
Next, an electromagnetic pulse bullet according to the second embodiment will be described in detail with reference to the drawings. FIG. 4 is an explanatory diagram showing an outline of the electromagnetic pulse bullet of the present embodiment. In addition, the dimension ratio of drawing is exaggerated on account of description, and may differ from an actual ratio. Moreover, about the thing equivalent to what was demonstrated in said embodiment, the code | symbol same as them is attached | subjected and description is abbreviate | omitted.

  As shown in FIG. 4, the electromagnetic pulse bullet 2 of the present embodiment is different from the first embodiment described above in that the control device 40 further includes a storage unit 44. That is, the control device 40 includes a position information acquisition unit 41, a final stage determination unit 42, a turning means control unit 43, and a storage unit 44.

  By having the configuration as described above, it is possible not only to irradiate the electromagnetic pulse over a wide range compared to the conventional electromagnetic pulse bullet, but also the effect of the electromagnetic pulse even if the target landing point is shifted. Is obtained. Note that the electromagnetic pulse bullet of the present embodiment can irradiate the electromagnetic pulse over a wide range as compared with the case of the conventional electromagnetic pulse bullet as in the first embodiment described above.

  Here, the storage unit will be described in more detail. The storage unit 44 is not particularly limited as long as it can store position information at the final stage before the electromagnetic pulse irradiation, and a conventionally known arithmetic unit can be used. In addition, when the target landing point moves, for example, it is preferable to receive a search result regarding position information at the final stage before electromagnetic pulse irradiation or to search automatically.

  In the electromagnetic pulse bullet of this embodiment, for example, the following rotation control is performed. For example, in S1 in FIG. 3, the position information acquisition unit 41 acquires the position information of the bullet 10 and proceeds to S2.

  In S2, the final stage determination unit 42 determines the final stage before the electromagnetic pulse irradiation based on the signal from the position information acquisition unit 41 and the signal from the storage unit 44 that stores the position information of the final stage before the electromagnetic pulse irradiation. If it is determined that it is the final stage before the electromagnetic pulse irradiation (in the case of YES), the process proceeds to S3. If it is not determined that the final stage is before the electromagnetic pulse irradiation (NO), the process returns to S1. In addition, in the “position information at the final stage before the electromagnetic pulse irradiation” here, when the target landing point moves, the storage unit displays the search result regarding the position information at the final stage before the electromagnetic pulse irradiation. Includes received or automatically searched.

  In S <b> 3, the turning means control unit 43 executes final stage turning control that is control of the turning means 30 for turning the bullet 10 with respect to the bullet axis 10 a of the bullet 10.

  In addition, when the target landing point moves or the deviation from the landing point is large, when acquiring the position information of the bullet, the flight time, flight speed, flight distance or flight altitude of the bullet is obtained. Or may be obtained by calculating any combination thereof. Thus, even when the target landing point moves or when the deviation from the landing point is large, a simple control device can be realized, and the turning means can be controlled with a small number of parts.

As described above, the electromagnetic pulse bullet is arranged on the bullet, and the position information acquisition unit that acquires the position information of the bullet, the storage unit that stores the position information of the final stage before the electromagnetic pulse irradiation, the position information acquisition unit A final stage determination unit that determines whether it is the final stage before the electromagnetic pulse irradiation, and a rotation unit that controls the rotation unit based on the signal from the final stage determination unit A control unit having a control unit, and when the turning means control unit receives a signal from the final stage determination unit that it is the final stage before the electromagnetic pulse irradiation, It is preferable to execute final stage rotation control, which is control of the rotation means for rotating.
By setting it as such a structure, an electromagnetic pulse can be irradiated over a wide range in an electromagnetic pulse bullet by controlling a turning means based on position information acquired by various methods. In addition, there is a secondary advantage that the effect of electromagnetic pulses can be obtained even if the target impact point deviates.

In addition, it is preferable that the position information acquisition unit acquires the position information of the bullet from the flight time, the flight speed, the flight distance, or the flight altitude of the bullet or any combination thereof.
By adopting such a configuration, the rotation means is controlled based on position information acquired by various methods such as flight time, flight speed, flight distance, flight altitude, etc. Electromagnetic pulses can be irradiated.

Furthermore, it is preferable that the bullet has wings, and the wings are rotating means.
By adopting such a configuration, it is possible to irradiate the electromagnetic pulse over a wide range in the electromagnetic pulse bullet by controlling a simple structure such as a wing. In addition, there is a secondary advantage that the effect of electromagnetic pulses can be obtained even if the target impact point deviates.

(Third embodiment)
Next, an electromagnetic pulse bullet according to the third embodiment will be described in detail with reference to the drawings. FIG. 5 is an explanatory diagram showing an outline of the electromagnetic pulse bullet of the present embodiment. In addition, the dimension ratio of drawing is exaggerated on account of description, and may differ from an actual ratio. Moreover, about the thing equivalent to what was demonstrated in said embodiment, the code | symbol same as them is attached | subjected and description is abbreviate | omitted.

  As shown in FIG. 5, the electromagnetic pulse bullet 3 of this embodiment includes a bullet body 10 and an electromagnetic pulse generator 20 that is disposed on the bullet body 10 and has an electromagnetic pulse irradiation unit 21. Then, the electromagnetic pulse bullet 3 is arranged on the bullet 10 and rotates to rotate the electromagnetic pulse irradiation unit 21 in the direction indicated by the arrow Y in the figure with respect to the bullet axis 10a of the bullet 10 at the final stage before the electromagnetic pulse irradiation. A means 30 'is further provided. Although not shown, it goes without saying that the direction of rotation may be the direction opposite to the direction indicated by arrow Y in the figure. The electromagnetic pulse bullet 3 preferably further includes a control device 40 disposed on the bullet body 10. Moreover, in the example of illustration, although the control apparatus 40 has the position information acquisition part 41, the last stage determination part 42, the rotation means control part 43, and the memory | storage part 44, it is not limited to this. For example, a configuration without the storage unit 44 may be used.

  Also by having the above-described configuration, it is possible to irradiate electromagnetic pulses over a wide range as compared with conventional electromagnetic pulse bullets. In addition, there is a secondary advantage that the effect of electromagnetic pulses can be obtained even if the target impact point deviates. Note that the electromagnetic pulse bullet of the present embodiment can irradiate the electromagnetic pulse over a wide range as compared with the case of the conventional electromagnetic pulse bullet as in the first embodiment described above.

  Here, the turning means 30 'will be described in more detail. As the turning means 30 ′, for example, the bullet body 10 includes a bullet head 11 and a main body portion 12, and the bullet head 11 is attached to the main body portion 12 so as to be rotatable as necessary. Can be mentioned. Further, as the rotating means 30 ′, not only the main body portion 12 but also the bullet body 10 including the warhead 11 itself is not rotated at all, and only the electromagnetic pulse irradiation unit 21 is rotated. Examples of the rotating means 30 'include an electric motor that rotates an electromagnetic pulse irradiation unit. When constructing such a mechanism, the number of parts is increased as compared with the case of using a wing or an auxiliary rocket as the rotating means, but there is an advantage that the flying posture of the electromagnetic pulse bullet can be easily maintained.

  In addition, the same rotation control as described above may be performed in the electromagnetic pulse bullet of this embodiment.

  As mentioned above, although this invention was demonstrated by some embodiment, this invention is not limited to these, A various deformation | transformation is possible within the range of the summary of this invention.

  For example, the configuration is not limited to the configuration described in the above-described embodiment, and details of the configuration of the rotating means and the control device can be changed.

1, 2, 3, 100 Electromagnetic pulse bullet 10 Bullet 10a Bullet 11 Bullet head 12 Main body 20 Electromagnetic pulse generator 21 Electromagnetic pulse irradiation unit 30, 30 'Turning means 40 Control device 41 Position information acquisition unit 42 Final stage determination part 43 flipping means irradiation axis P point of impact R _E potency range of the control unit 44 storage unit E electromagnetic pulses Ea electromagnetic pulse

Claims (4)

  An electromagnetic pulse bullet characterized in that an irradiation axis of an electromagnetic pulse in an electromagnetic pulse irradiation unit of a bullet is inclined with respect to the bullet axis of the bullet, and the irradiation axis is rotated at the final stage of flight.   The electromagnetic pulse bullet according to claim 1, wherein the irradiation shaft is rotated by rotating the bullet body.   The electromagnetic pulse bullet according to claim 1, wherein the irradiation axis is rotated by rotating the electromagnetic pulse irradiation unit.   An electromagnetic pulse irradiation method for an electromagnetic pulse bullet characterized in that the electromagnetic pulse is irradiated while rotating the irradiation axis of the electromagnetic pulse at the final stage of the flight of the electromagnetic pulse bullet.

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