KR20150096837A - Missile defence of using parachute - Google Patents
Missile defence of using parachute Download PDFInfo
- 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
- Authority
- KR
- South Korea
- Prior art keywords
- parachute
- enemy
- missile
- submarine
- deployed
- Prior art date
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H11/00—Defence installations; Defence devices
- F41H11/02—Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H13/00—Means of attack or defence not otherwise provided for
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
Landscapes
- 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
Description
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
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
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
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
6 is a situation in which a
7 is a state in which the
8 shows a situation in which a parachute deployed by a friendly party toward a
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
11 is a situation in which a
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)
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, .
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 .
A submarine (115) for launching a parachute (300) in water toward an enemy submarine (113) in order to sink an enemy submarine (113)
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 |
Publications (1)
Publication Number | Publication Date |
---|---|
KR20150096837A true KR20150096837A (en) | 2015-08-26 |
Family
ID=54058953
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
KR1020140017623A KR20150096837A (en) | 2014-02-17 | 2014-02-17 | Missile defence of using parachute |
Country Status (1)
Country | Link |
---|---|
KR (1) | KR20150096837A (en) |
Cited By (2)
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 |
-
2014
- 2014-02-17 KR KR1020140017623A patent/KR20150096837A/en not_active Application Discontinuation
Cited By (2)
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 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US6293202B1 (en) | Precision, airborne deployed, GPS guided standoff torpedo | |
AU2002318789B2 (en) | Operation of a decoy against threats | |
CN105539788A (en) | Novel underwater aircraft carrier and use method thereof during battling | |
US11293731B2 (en) | Non-lethal naval vessel interdiction weapon | |
Hogg | German Secret Weapons of World War II: The Missiles, Rockets, Weapons, and New Technology of the Third Reich | |
RU2594314C1 (en) | Method of target destruction with anti-submarine cruise missile | |
Hogg | German Secret Weapons of the Second World War: The Missiles, Rockets, Weapons & New Technology of the Third Reich | |
KR20150096837A (en) | Missile defence of using parachute | |
US7503259B2 (en) | Anti-submarine warfare cluster munitions and cluster depth charges | |
RU2546726C1 (en) | Antisubmarine cruise missile and its application method | |
RU2590760C2 (en) | Missile and method for its operating | |
RU2705730C1 (en) | Method of aircraft protection against missile damage in rear hemisphere | |
RU2714274C2 (en) | Cruise missile with self-contained unmanned underwater vehicle-mine | |
RU2697694C1 (en) | Underwater target destruction method | |
Konstam | Taranto 1940: The Fleet Air Arm’s precursor to Pearl Harbor | |
RU2781555C1 (en) | Kosteniuk aerostat salvo launch system (asls) | |
RU2785316C1 (en) | Rocket-glider with gravity underwater projectile | |
Dobrzyński et al. | Flying means of attack of ships, possible to be used by a potential enemy—analysis of the threats for ships the Polish Navy | |
US6923105B1 (en) | Gun-armed countermeasure | |
US3839940A (en) | Automatic pop-up decoy | |
Yeo | Desperate Sunset: Japan’s kamikazes against Allied ships, 1944–45 | |
RU2339900C1 (en) | Towed false air target | |
JP2022087361A (en) | Intercepting device for moving object | |
RU2711409C2 (en) | Submarine destruction method | |
Bana | Armed to the Hilt Indian Navy’s Anti-Ship Missiles |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
E601 | Decision to refuse application |