KR20150096837A - Missile defence of using parachute - Google Patents

Missile defence of using parachute Download PDF

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Publication number
KR20150096837A
KR20150096837A KR1020140017623A KR20140017623A KR20150096837A KR 20150096837 A KR20150096837 A KR 20150096837A KR 1020140017623 A KR1020140017623 A KR 1020140017623A KR 20140017623 A KR20140017623 A KR 20140017623A KR 20150096837 A KR20150096837 A KR 20150096837A
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KR
South Korea
Prior art keywords
parachute
enemy
missile
submarine
deployed
Prior art date
Application number
KR1020140017623A
Other languages
Korean (ko)
Inventor
황창섭
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황창섭
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Publication date
Application filed by 황창섭 filed Critical 황창섭
Priority to KR1020140017623A priority Critical patent/KR20150096837A/en
Publication of KR20150096837A publication Critical patent/KR20150096837A/en

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41HARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H11/00Defence installations; Defence devices
    • F41H11/02Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41HARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H13/00Means of attack or defence not otherwise provided for
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

The present invention relates to a missile defense system devised to explode an enemy missile body in advance and in midair, by spreading parachutes right in front of the already-fired enemy missiles and inducing the missiles to explode by being tangled with the parachutes or to fall down by losing balance. The structure includes a homing body, on one end, mounted with an automatic navigation device, a heat detection device and a range finder, a parachute connected to the homing body, a parachute chamber and a homing missile, on the other end, mounted with a fuel tank and propulsion fuel. According to the present invention, the missile defense system tremendously lowers the production costs and has high probability of hit when compared with traditional methods. The present invention is also devised to be applied to various cases such as ballistic bodies, rocket systems, fighters, high-speed boats, torpedoes and submarines.

Description

[0002] MISSILE DEFENSE OF USING PARACHUTE [0003]

The present invention relates to a missile, a cannon, and a torpedo, which are launched toward a friendly enemy, are detected early before reaching a target point, and are rapidly demolished in the air, ground, water, or water, , Shells, torpedoes, and so on.

It is technically quite tricky and difficult to have the missiles, shells, and torpedoes fired by the enemy against the enemy in the broad air, on the ground, on the surface of the sea or on the sea floor. It is also difficult to blow up enemy fighters deeply penetrating enemy camps, enemy speedboats that run fast on the sea, and enemy tanks that are fast-paced. As shown in FIG. 2, the basic principle of the present invention is to deploy a parachute 203 in front of a missile 201 launched by an enemy, and to launch a missile 201, which is fired by an enemy, ), It is an invention designed to cause the enemy-launched missile 201 to be blown up in the air or to completely fall in the course of its course.

The most basic method of the present missile defense system is as shown in FIG. 1, in which an enemy missile (101) is fired at an enemy missile base or a friendly enemy ship at an intermediate point to detect an enemy missile (101) A missile 102 capable of destroying an enemy missile is shot and the side (side) of the missile 101 fired by the enemy at the point 103 on the anticipated career line is adjusted have. However, this method has become a big problem because the high technology is required and the accuracy rate is considerably low.

Thus, the present invention is designed to cause the enemy missiles to collide with the parachute, or to explode in the air, or to lose direction and fall from the middle (because of the deployment of the parachute in front of the enemy-launched missile).

The greatest effect of the present invention is that the accuracy rate is very high. For example, assuming that the diameter of the parachute is 30 meters when fully deployed, the missile, cannon, torpedo, and other enemy launches are within 30 meters of the target, so the probability of hit is very high. In addition, this parachute can be deployed on the front of the enemy missile, and even if it spreads on the side, the probability of hit is high. Therefore, it can be seen that the utilization rate is much different from the current system which can only attack the side (side) have. The object of the invention is not limited to only enemy missiles, but also to helicopters of enemy fighters, high-speed enemy ships, enemy submarines, enemy submarines, enemy tanks, enemy shells, multi-purpose rocket shells and so on. The effect can be considered to be infinite, and the manufacturing cost is also much cheaper than the current missile defense system.

FIG. 1 is a view of a missile shooting system according to a currently used missile defense system.
FIG. 2 is a view showing a shot of a missile shot by a parachute shot employing a newly designed invention. FIG.
3 is a schematic view of a newly designed parachute shot.
FIG. 4 is a schematic view of a newly developed parachute immediately after deploying the parachute. FIG.
Figure 5 shows a parachute deployed right in front of enemy fighters by launching a newly designed parachute shot against a fighter plane that is being pursued by an enemy fighter.
FIG. 6 shows a parachute being deployed in front of a shell shot by an enemy after launching a newly designed parachute shot toward an enemy-launched shell.
FIG. 7 shows a parachute deployed right in front of a multi-purpose rocket shell fired by an enemy after launching a newly designed parachute gun against an enemy launching multi-launch rocket.
FIG. 8 shows a parachute deployed in front of an enemy helicopter after launching a newly designed parachute shot toward an enemy helicopter.
Figure 9 shows a parachute deployed in front of a torpedo fired from an enemy submarine after launching a newly designed parachute shot against a torpedo fired from an enemy submarine.
Fig. 10 shows a parachute deployed in front of the enemy's highway after launching a newly designed parachute shot toward the enemy's highway running at high speed.
FIG. 11 shows a parachute being deployed in the submarine immediately after launching a newly designed parachute shot in a submarine to sink an enemy submarine infiltrating into a friendly coast.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS Hereinafter, preferred embodiments of the present invention will be described in detail with reference to the accompanying drawings.

First, the basic structure of the parachute in FIG. 3 will be described. (301) is a derivative including a heat detector, an automatic navigation device based on GPS, a distance detection sensor, etc. to guide the direction of the parachute and determine the time And the parachute 303 is actuated to expand the parachute in front of the target, and the parachute 303 stored in the parachute storage room 302 is operated by the instruction of the step 301 as the parachute storage room. The fuel 305 embedded in the fuel cell 304 is ignited by the instruction of the 301 as the propellant fuel that can be propelled forward, and at the same time, the propulsion of the parachute is carried out, The parachute 303 is unfolded and the parachute storage room 301 and the fuel tank 304, which are integrally formed, are automatically separated and freely fall down under the condition shown in FIG.

Now, when this newly designed parachute shot is used in actual combat, the predicted degree expected after launching to various targets is shown in Figs. 5, 6, 7, 8, 9, 10 and 11. Fig.

5 shows a situation in which a friendly fighter 503 being chased by a bandit 501 in the airplane of a fighter aircraft fires a parachute shot 502 toward a bandit 501 to be chased after the enemy fighter 501, It is a picture that anticipates the unfolded condition. In this case, even if the deployed parachute 502 spans a part of the wing of the enemy fighter 501 pursuing from behind, the enemy fighter 501 will soon lose its center and fall down.

6 is a situation in which a parachute 602 is deployed from directly over the enemy shell 601, which is a parachute shot shot by an enemy group toward an enemy-launched shell. One worry is that the enemy shell (601), which is moving at a very fast pace, may just pass through a parachute (602) spreading in front of it. But if you hold the four corners of a handkerchief tightly and pull the handkerchief with the knife, you will surely tear the handkerchief. However, with a handkerchief thrown in the air, the handkerchief will not be torn and will be stuck with the knife even if the handkerchief is hammered with a knife. Likewise, the enemy-launched shell 601 will never pass through the parachute 602 and will fall down while being wrapped in a parachute. In particular, since most of the shells are advanced while rotating at a high speed as shown in FIG. 6, (601) will be crashed by a parachute (602) of a parachute shot by a friendly fighter.

7 is a state in which the parachute 702 is deployed in front of the enemy shell 701, which is a parachute warrior fired by a friendly army, toward a shell 701 which is fired at a time by several enemy multi-launch rocket guns. In this case, it is also possible to collapse a plurality of shells entering into the parachute 702 at once.

8 shows a situation in which a parachute deployed by a friendly party toward a helicopter 801 of an enemy force spreads from the front of the enemy helicopter. In this situation too, even if a part of the parachute 802 deployed just in front of the enemy helicopter is only a small part of the wing of the enemy helicopter 801, the enemy helicopter 801 will be damaged with a fatal damage.

FIG. 9 shows that a submarine (901) penetrating deeply into a friendly coast has launched a torpedo (902) that has been launched toward a friendly ally after a friendly ally has detected the ally, (903). In this case, the torpedo (902) that entered the unfolded parachute (903) would collide with the deployed parachute (903) and immediately fall into the deep sea.

FIG. 10 is a situation in which a parachute 112 is deployed right before the enemy cruise ship 111 after a friendly party fires a newly designed parachute shot toward an enemy cruiser 111 running on the sea at high speed. In this case, even if the enemy cruiser 111 is enclosed by the parachute 112 by the ally of the parachute, the enemy cruiser 111 is not immediately centered or exploded. However, the parachute (112), which is surrounded by a parachute (112) that commands commander or enemy forces in the wheelhouse, can not secure the watch, and the enemy radar Because of the color of the bright and colorful parachute, the enemy vestibule (111) will be able to be spotted to the friendly group continuously, and it will be a clear target of the ally.

11 is a situation in which a parachute 114 is deployed in front of an enemy submarine 113 after a buddy who has captured an enemy submarine 113 that has penetrated deeply into a friendly coast has fired a newly designed parachute shot toward the enemy submarine 113. In this case, the speed of the enemy submarine 113 wrapped in the parachute 114 will drop rapidly, and it becomes difficult to control the submarine so that the submarine can not be adjusted. When a part of the parachute 114 is wrapped around the screw of the submarine 113 Will result in the progress of the submarine itself becoming more difficult.

As described above, the configuration of the newly invented parachute cannon and its application are examined. In comparison with the method used in the existing missile defense system shown in FIG. 1, The missile defense system of the present invention is superior.

DESCRIPTION OF THE REFERENCE SIGNS

301; Paratrothanite derivatives.

302; Parachute storage room.

303; parachute.

304; Fuel tank with parachute.

305; Fuel for propulsion of parachute.

300; (301), (302), (303), (304), (305).

Claims (3)

The deployed missile 201 is fired at an early stage in the air in order to launch and fire the enemy missile 201. The missile 201 is fired by the enemy missile 201 to launch a parachute gun 300 composed of 301, 302, 303, 304, A device for causing the enemy missiles 201 to be deployed by the parachute 303 in the vicinity of the parachute 303 by spreading the parachute 303 directly in front of the parachute 303;
A parachute storage room 302 and a propelling fuel tank 304 integrally formed with the parachute 303 are expanded by a derivative 301 having a built-in thermal tracking device, an automatic navigation device, an automatic distance measuring device, .
In connection with claim 1;
A device for launching the parachute shot 300 toward the rear side where the enemy fighter 501 pursuing by the friendly fighter 503 being pursued for blowing or crashing the enemy fighter 501 pursuing the friendly fighter 503 .
In connection with claim 1;
A submarine (115) for launching a parachute (300) in water toward an enemy submarine (113) in order to sink an enemy submarine (113)
KR1020140017623A 2014-02-17 2014-02-17 Missile defence of using parachute KR20150096837A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
KR1020140017623A KR20150096837A (en) 2014-02-17 2014-02-17 Missile defence of using parachute

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
KR1020140017623A KR20150096837A (en) 2014-02-17 2014-02-17 Missile defence of using parachute

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2651407C1 (en) * 2017-04-17 2018-04-19 Дмитрий Владимирович Григоренко Method of air objects hitting
CN109029159A (en) * 2018-09-29 2018-12-18 中国空空导弹研究院 A kind of flying mesh injures formula missile armament

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2651407C1 (en) * 2017-04-17 2018-04-19 Дмитрий Владимирович Григоренко Method of air objects hitting
CN109029159A (en) * 2018-09-29 2018-12-18 中国空空导弹研究院 A kind of flying mesh injures formula missile armament

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