WO2009025570A1 - Ensemble de fusées 'straj' - Google Patents

Ensemble de fusées 'straj' Download PDF

Info

Publication number
WO2009025570A1
WO2009025570A1 PCT/RU2007/000443 RU2007000443W WO2009025570A1 WO 2009025570 A1 WO2009025570 A1 WO 2009025570A1 RU 2007000443 W RU2007000443 W RU 2007000443W WO 2009025570 A1 WO2009025570 A1 WO 2009025570A1
Authority
WO
WIPO (PCT)
Prior art keywords
missile
self
launcher
sea
sonar
Prior art date
Application number
PCT/RU2007/000443
Other languages
English (en)
Russian (ru)
Inventor
Vladimir Anatolevich Matveev
Original Assignee
Vladimir Anatolevich Matveev
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Vladimir Anatolevich Matveev filed Critical Vladimir Anatolevich Matveev
Priority to PCT/RU2007/000443 priority Critical patent/WO2009025570A1/fr
Priority to RU2009109389/11A priority patent/RU2423659C2/ru
Publication of WO2009025570A1 publication Critical patent/WO2009025570A1/fr

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00—Rocket or torpedo launchers
    • F41F3/04—Rocket or torpedo launchers for rockets
    • F41F3/07—Underwater launching-apparatus
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/20—Missiles having a trajectory beginning below water surface

Definitions

  • 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.
  • 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.
  • 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.
  • 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.
  • 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.
  • 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?
  • 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.
  • anti-sabotage self-defense equipment contains at least one multi-barrel rocket-propelled grenade launcher with a sonar.
  • 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.
  • 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.
  • the sonar 4 receives sound signals from sea targets 19, 20 and determines the direction to the nearest sea target.
  • 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).
  • 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.
  • the launcher turns in the direction of the next target 19 and the attack process is repeated.
  • 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.

Landscapes

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

Abstract

L'ensemble de fusées de l'invention appartient au domaine de la défense côtière et peut s'utiliser pour effectuer une frappe avec des fusées (isolée ou en salve) contre les navires (groupes de navires), sous-marins et aéronefs lors de la défense de la côte. Par temps de guerre il s'utilise pour protéger d'un carré désiré de l'océan, pour bloquer le déplacement dans les détroits maritimes, sur des isthmes et/ou pour organiser le blocus maritime de la côte ennemie. L'ensemble a été réalisé de manière à pouvoir être basé sur le fond marin et possède une plus grande viabilité grâce à une moindre visibilité optique du lieu de positionnement et à l'utilisation de moyens passifs de détection et de guidage de missiles. Les moyens passifs sont montés dans une bouée à élévation autonome dans un boîtier hermétique transparent aux sons et aux ondes radio. A des fins de protection contre les incursions ennemies, l'ensemble est muni de lance-roquettes sous-marins multitubes dotés d'un sonar.
PCT/RU2007/000443 2007-08-13 2007-08-13 Ensemble de fusées 'straj' WO2009025570A1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
PCT/RU2007/000443 WO2009025570A1 (fr) 2007-08-13 2007-08-13 Ensemble de fusées 'straj'
RU2009109389/11A RU2423659C2 (ru) 2007-08-13 2007-08-13 Ракетный комплекс "страж"

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/RU2007/000443 WO2009025570A1 (fr) 2007-08-13 2007-08-13 Ensemble de fusées 'straj'

Publications (1)

Publication Number Publication Date
WO2009025570A1 true WO2009025570A1 (fr) 2009-02-26

Family

ID=40378360

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/RU2007/000443 WO2009025570A1 (fr) 2007-08-13 2007-08-13 Ensemble de fusées 'straj'

Country Status (2)

Country Link
RU (1) RU2423659C2 (fr)
WO (1) WO2009025570A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2726580C1 (ru) * 2019-09-04 2020-07-14 Акционерное общество "Научно-производственное предприятие "Калужский приборостроительный завод "Тайфун" Береговой ракетный комплекс

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2726377C1 (ru) * 2020-02-04 2020-07-13 Акционерное общество "Научно-производственное объединение "СПЛАВ" имени А.Н. Ганичева" Мобильный комплекс для поражения подводных целей

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU95111720A (ru) * 1995-07-06 1997-06-27 Государственный ракетный центр "КБ им.акад.В.П.Макеева" Пусковая система для старта ракеты носителя с водной поверхности
RU2093783C1 (ru) * 1995-06-09 1997-10-20 Карягин Николай Васильевич Способ стрельбы с палубной пусковой установки противолодочного ракетного комплекса
RU2151995C1 (ru) * 1999-06-29 2000-06-27 Балтийский государственный технический университет "Военмех" им. Д.Ф. Устинова Комплекс для запуска ракеты с акватории
GB2380244A (en) * 2001-08-13 2003-04-02 Michael Joseph Zabrana Automated defence system
RU2285889C1 (ru) * 2005-09-20 2006-10-20 ОАО "Конструкторское бюро машиностроения" Береговой ракетный противокорабельный комплекс
RU2303762C1 (ru) * 2005-11-03 2007-07-27 Эдуард Дмитриевич Житников Надводное транспортно-пусковое устройство "касатка"

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2093783C1 (ru) * 1995-06-09 1997-10-20 Карягин Николай Васильевич Способ стрельбы с палубной пусковой установки противолодочного ракетного комплекса
RU95111720A (ru) * 1995-07-06 1997-06-27 Государственный ракетный центр "КБ им.акад.В.П.Макеева" Пусковая система для старта ракеты носителя с водной поверхности
RU2151995C1 (ru) * 1999-06-29 2000-06-27 Балтийский государственный технический университет "Военмех" им. Д.Ф. Устинова Комплекс для запуска ракеты с акватории
GB2380244A (en) * 2001-08-13 2003-04-02 Michael Joseph Zabrana Automated defence system
RU2285889C1 (ru) * 2005-09-20 2006-10-20 ОАО "Конструкторское бюро машиностроения" Береговой ракетный противокорабельный комплекс
RU2303762C1 (ru) * 2005-11-03 2007-07-27 Эдуард Дмитриевич Житников Надводное транспортно-пусковое устройство "касатка"

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2726580C1 (ru) * 2019-09-04 2020-07-14 Акционерное общество "Научно-производственное предприятие "Калужский приборостроительный завод "Тайфун" Береговой ракетный комплекс

Also Published As

Publication number Publication date
RU2009109389A (ru) 2010-10-27
RU2423659C2 (ru) 2011-07-10

Similar Documents

Publication Publication Date Title
US5677506A (en) Submarine extendible turret system
Lautenschläger Technology and the evolution of naval warfare
EP1336814B1 (fr) Utilisation d' un leurre contre menaces
KR20060118454A (ko) 엔드 스테이지 유도미사일로부터 선박을 보호하기 위한방법 및 장치
RU2554640C2 (ru) Способ обнаружения морских целей
RU2658517C2 (ru) Разведывательно-огневой комплекс вооружения БМОП
US20090308236A1 (en) Missile system
US7779772B2 (en) Submarine short-range defense system
RU2423659C2 (ru) Ракетный комплекс "страж"
RU2413156C1 (ru) Противовоздушный (противокорабельный) автономный универсальный комплекс позиционный подводный управляемый ("паук" ппу) и способ его применения
RU2382313C2 (ru) Противовоздушный автономный универсальный комплекс самообороны подводных лодок ("паук" со пл) и способ его применения
RU2714274C2 (ru) Крылатая ракета с автономным необитаемым подводным аппаратом-миной
RU2333450C1 (ru) Самоходная огневая установка обнаружения, сопровождения и подсвета целей, наведения и пуска ракет зенитного ракетного комплекса средней дальности
RU2733600C1 (ru) Термобарический способ борьбы с роем малогабаритных беспилотных летательных аппаратов
RU2733732C1 (ru) Способ защиты надводного корабля и судна от поражения торпедой
RU2680919C1 (ru) Мобильное активное устройство для защиты различных объектов от беспилотных управляемых самодвижущихся средств поражения
Walker Smart weapons in naval warfare
Arkin et al. The Nuclearisation of the Oceans: Roles, Missions and Capabilities
RU208980U1 (ru) Устройство для борьбы с роем малогабаритных беспилотных летательных аппаратов путем создания осколочного поля
GB2232748A (en) Remotely controllable aircraft
RU2762137C2 (ru) Защита объектов военной техники от высокоточного оружия
RU2746085C1 (ru) Способ защиты надводного корабля от торпеды
Egozi The Israeli unmanned killer boat-Fire power on the high seas
Dobrzyński et al. Capabilities to combat helicopters by warships of Polish Navy in the light of the development of active systems to counteract sets manpads
Feigl The impact of new maritime technologies

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 07870604

Country of ref document: EP

Kind code of ref document: A1

ENP Entry into the national phase

Ref document number: 2009109389

Country of ref document: RU

Kind code of ref document: A

NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 07870604

Country of ref document: EP

Kind code of ref document: A1