WO2009025570A1

WO2009025570A1 - Missile system

Info

Publication number: WO2009025570A1
Application number: PCT/RU2007/000443
Authority: WO
Inventors: Vladimir Anatolevich Matveev
Original assignee: Vladimir Anatolevich Matveev
Priority date: 2007-08-13
Filing date: 2007-08-13
Publication date: 2009-02-26
Also published as: RU2423659C2; RU2009109389A

Abstract

The inventive missile system relates to coastal defense systems and can be used for carrying out a missile strike (single or in volleys) on warships (squadrons), submarines and aeroplanes during a coast defence. In wartime, the system is used for defending a given square of the sea, for blocking traffic in sea channels, in isthmuses and/or for blocking an enemy coast. The system can be positioned at the sea bed and exhibits a high ability to survive due to the reduced optical vision of the site where it is located and to the use of passive missile detection and pointing means. The passive detection means are mounted on a self-lifting buoy ina sealed radioparent and sound-transparent body. For antidiversionary protection, the system is provided with submarine multi-barreled jet grenade launchers.

Description

Missile system "Guard"

The invention relates to coastal defense systems and can be used to launch a missile strike (single or salvo) against ships (ship formations), submarines and aircraft while protecting the coast.

The well-known French missile system "Exoset" ("Militar Defepse" 1995, v.19, JSfe2, p.24-26, 28-31. Massimo Ashiati "Сostal Defefse; issuеs apd solutiops") and the American missile complex "Harpoon" (Japé's Naval Weapon Systems, Sulsdop 2000, ρρ.328-344 RGM-84 / UGM HARPOON (GWS 60), coast-based, consisting of a command radar module and several firing modules for performing single and multiple-launch missiles "Exoset MM 40 and Harpoon, respectively.

The disadvantage of these systems is the lack of survivability due to the vulnerability of stationary radar control centers for anti-radar shells and the difficulty of masking stationary missile systems from spaceborne reconnaissance vehicles. The failure of the control point leads to the inability to use the entire complex.

The well-known Russian missile system Rubezh (Armament of the Navy. Encyclopedia of the XXI century. Arms and technologies of Russia, volume 3, p. 129. Publishing house "Arms and Technologies". M., 2001) coast-based, consisting of self propelled missile launchers

SUBSTITUTE SHEET (RULE 26) installations, including a radar target designation system, a prelaunch and missile launch system, a radio communication system and a vehicle (car) with an energy supply system.

The mobility of the Pybezh missile system, as well as the supply of each self-propelled launcher with its own radar target designation, slightly increases its survivability. However, with a massive plaque, the indicated survivability measures are insufficient.

Known missile system (RU 2285889, class F41H 13/00, F41F 3/04, 2006), containing the main command and control point and communication with the target data formation system and topographic location, data exchange system, as well as self-propelled launchers with missiles, system forming the initial data, the data exchange system, characterized in that it is provided with self-propelled backup command point control and communications, wherein a primary and backup control command propelled connection points and and all propelled launchers introduced ^"information control systems with a control module, a processing module, a control panel, while the control module is connected to the data processing module via the Ethernet network, and the control panel is configured to provide input of the operating mode of the main or backup self-propelled command and control command and communication center, and the processing module the data contains a timer connected to the second system bus, to which the input of the second controller of the serial channel is connected, the output of which is connected to the data exchange system and wherein the first input of the serial controller ^* connected to the first system bus, and the output to the system. the formation of target designation and topographic location information and control systems of the main and backup, self-propelled command and control command and communication center and all self-propelled launchers through data exchange systems are interconnected.

Reservation of command posts and the use of the Ethernet network somewhat increase the survivability of the coast-based complex. However, as in the previous version with massive plaque, these measures to increase the survivability of the complex are insufficient.

Known missile system (GB 2380244, IPC: B63G8 / 28; F41G7 / 22; F41H11 / 02; B63G8 / 00; F41G7 / 20; F41H11 / 00, 2003), containing detection means and means of hitting targets, interconnected by digital communication lines moreover, the detection means contain a sonar and a digital radio receiver of the satellite-based space reconnaissance system, and the means of hitting targets are made in the form of a launcher * rocket with homing heads. Moreover, the missile launcher block contains launchers of air, coastal and sea-based. Launchers of air-based missiles are located on unmanned aerial vehicles, equipped with sonars and are configured to automatically take off according to the early warning system and cyclic barrage in the airspace along the defended coast. The coastal and sea-based missile launchers are equipped with their own passive detection means and are located on Earth and on ships, respectively. Missile launchers are equipped with television homing heads. The use of sonars (passive means of detecting targets) can increase the survivability of the missile system and protect it from anti-radar missiles. However, the high accuracy of modern enemy optical means for space reconnaissance and topographic location, comparable with the size of the zones of destruction of missiles with non-nuclear warheads, does not solve the problem of survivability (self-preservation) of the missile complex before the enemy attacks the objects defended by the missile complex.

The basis of the present invention is the task of increasing the survivability of the missile system. The technical result that provides a solution to this problem is to reduce the optical visibility of the rocket complex from space at its location.

The solution of this problem and the achievement of the claimed technical result is ensured by the fact that a missile system containing detection means and targets, interconnected by digital communication lines, the detection means containing a sonar and a digital radio receiver of the satellite system for space reconnaissance, and means of destroying targets - in the form of a missile launcher block with homing heads, according to the invention it further comprises anti-sabotage means of self-defense, numbers stems link? made of fiber optic, a sonar and a digital radio receiver of the satellite-based space reconnaissance system are mounted on a self-raising buoy in a sealed radio-transparent case, the missile launcher block is made with the possibility of bottom-based and contains at least one self-elevating launcher with a vertical arrangement of trunks and at least one self-elevating launcher with horizontal the location of the trunks. At the same time, anti-sabotage self-defense equipment contains at least one multi-barrel rocket-propelled grenade launcher with a sonar.

The installation of a sonar and a digital radio signal receiver on a self-propelling buoy in a sealed radio-transparent case and the implementation of a launcher block with the possibility of bottom-based elimination of the possibility of optical reconnaissance of the combat order of the missile system from space and, thereby, increase the survivability of the missile system. The introduction of anti-sabotage self-defense means can further increase the survivability of the missile system by counteracting underwater reconnaissance. Supplying the launcher block with self-elevating launchers with vertical and horizontal shafts allows counteracting air and sea attack means and, thus, additionally increasing the survivability of the missile system.

The figure shows a figure explaining the design of the missile system and the method of its use.

The missile system contains means 1 for detecting and means 2 for hitting targets, interconnected by digital lines 3 of communication. The detection means 1 comprise a sonar 4 and a digital receiver 5 of radio signals of the satellite system 6 for space reconnaissance, mounted on a self-raising buoy 7 in a sealed radio-transparent case. Means 2 of target destruction are made in the form of a missile launcher block with homing heads for the infrared or optical range of electromagnetic waves. Launcher block is made with the possibility of bottom-based and contains at least one self-elevating launcher 8 with a vertical arrangement of trunks and at least one self-elevating launcher 9 with a horizontal arrangement of trunks. On the outside of the launchers 8 and 9 (from the sea), self-contained anti-sabotage self-defense devices are installed, including at least one automatic or multi-barrel grenade launcher 10 with a sonar 11. Digital communication lines 3 are made of fiber optic. To enable the lifting and lowering means _w l detection grenades 10 are provided with ballast 12, self launchers 8 and 9, it ballasts 13, minrepami 14, winches 15 and reservoir 16 with air and turntables 17. Ballasts 13 are in the form of hardware containers provided with lead weights, battery electric power sources and digital signal processing and winch control devices 15. Minrepa 14 are graphite fiber cables through the central axis of which conducted fiber-optic communication lines 3.

The missile system works as follows. In the initial position, to ensure the rigidity of the launchers 8 and 9 with their ballasts, 13 minrepecks 14 are wound on the winch 15. In the threatened period, the detection means 1, the destruction means 2 and grenade launchers 10 are secretly taken to the place of deployment of the missile complex by means of a submarine or cargo ship and lowered to the bottom of the sea. After that, connect these elements together with optical communication lines 3 and turn on the winch? 15 to unwind minrepa 14 from the optical communication line 3. In this case, buoy 7 pops up. When the buoy 7 reaches the sea surface, the tension of the minrepa 14 weakens. The device for digital signal processing and control of the winch 15 of buoy 7 responds to a weakening of the cable and issues a command to turn off its winch 15 and to turn on the receiver 5 and sonar 4. The receiver 5 receives satellite navigation signals to determine the exact the location of the missile system and signal information on the coordinates of the air 18 and sea surface 19 and 20 underwater targets of the enemy. At the same time, the sonar 4 receives sound signals from sea targets 19, 20 and determines the direction to the nearest sea target. According to the signals of sonar 4 or satellite, the platform 16 deploys the launcher 9 in the direction of the nearest sea target, for example 20. When the sea target approaches the affected area, a signal is generated to raise the launcher 9. The winches 15 of the platform 17 are turned on and the last one floats horizontally to the surface of the sea or set range of permissible depth of missile launch (missile corridor). After the launcher 9 ascends to the given launch depth and after the homing heads of the missiles of the sea target 20, a signal is issued to detonate the squib of one of the missiles of the launcher 9. The missile flies in the direction of the first target 20. After the departure of the first missile, the launcher turns in the direction of the next target 19 and the attack process is repeated. Similarly, the launcher 8 for air targets works. The difference is its vertical ascent from the bottom of the sea and the launch of missiles mainly according to external target designation from satellite 6.

The invention is not limited to the above example of its implementation. In the framework of this invention, other variants of its implementation are possible. So, depending on the tactical task, the configuration of the missile system (battle order and the number of its launchers 8, 9) may vary. The missile system can both execute external control commands and work autonomously analyzing information from its sonars and independently make decisions on the destruction of objects in its reach. The rotation noise of the turntable 8 and 9 can be masked from the sonar of the complex by the powerful radiation of the cries of birds (gulls) and marine animals (dolphins).

The invention is developed at the level of a technical proposal.

Claims

Formula

1. A missile system containing detection means and means of hitting targets, interconnected by digital communication lines, the means of detection containing a sonar and a digital receiver of radio signals from a satellite-based space reconnaissance system, and means of hitting targets are made in the form of a missile launcher with homing heads, according to the invention additionally contains anti-sabotage means of self-defense, digital communication lines are made of fiber optic, a sonar and a digital radio receiver satellite The new space reconnaissance systems are mounted on a self-propelling buoy in a sealed radio-transparent housing, the missile launcher block is made with the possibility of bottom-based and contains at least one self-elevating launcher with a vertical arrangement of trunks and at least one self-elevating launcher with a horizontal arrangement of trunks.

2. The missile system according to claim 1, characterized in that the anti-sabotage self-defense means contain at least one multi-barrel rocket-propelled grenade launcher with a sonar.