ES2107921T3 - Sistema de lanzamiento y de orientacion de ingenios volantes. - Google Patents

Sistema de lanzamiento y de orientacion de ingenios volantes.

Info

Publication number
ES2107921T3
ES2107921T3 ES95936617T ES95936617T ES2107921T3 ES 2107921 T3 ES2107921 T3 ES 2107921T3 ES 95936617 T ES95936617 T ES 95936617T ES 95936617 T ES95936617 T ES 95936617T ES 2107921 T3 ES2107921 T3 ES 2107921T3
Authority
ES
Spain
Prior art keywords
launching
missile
orientation
missiles
annular body
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Lifetime
Application number
ES95936617T
Other languages
English (en)
Inventor
Ivan Ivanovitch Arkhangelsky
Eugene Gueorguevitch Bolotov
Vladimir Sergueevitc Philippov
Vladimir Yakovlevitch Mizrokhi
Vladimir Grigorievitch Svetlov
Gregory Andreevitch Stanevsky
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
LE BUREAU DE CONSTUCTIONS MECA
Thales SA
Original Assignee
LE BUREAU DE CONSTUCTIONS MECA
Thomson CSF SA
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
Priority claimed from RU95110350A external-priority patent/RU2082946C1/ru
Application filed by LE BUREAU DE CONSTUCTIONS MECA, Thomson CSF SA filed Critical LE BUREAU DE CONSTUCTIONS MECA
Application granted granted Critical
Publication of ES2107921T3 publication Critical patent/ES2107921T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/60—Steering arrangements
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F42B10/663—Steering by varying intensity or direction of thrust using a plurality of transversally acting auxiliary nozzles, which are opened or closed by valves
    • 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
    • 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
    • F41F3/077—Doors or covers for launching tubes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/60—Steering arrangements
    • F42B10/66—Steering by varying intensity or direction of thrust

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Tires In General (AREA)
  • Moulding By Coating Moulds (AREA)

Abstract

LA INVENCION SE REFIERE A UN SISTEMA DE LANZAMIENTO, Y PARTICULARMENTE UN SISTEMA DE LANZAMIENTO Y DE ORIENTACION DE MISIL. PERMITE MODERNIZAR LOS MISILES DE SALIDA INCLINADA TRANSFORMANDOLOS EN MISILES DIRIGIDOS PARA LA DEFENSA CIRCULAR, Y EVITA LA EYECCION DE LA MASA PASIVA SOBRE EL AREA DE LANZAMIENTO. PARA ESTO, EL SISTEMA DE LANZAMIENTO COMPRENDE MEDIOS DE LANZAMIENTO (10) DE LOS TIMONES AERODINAMICOS (2) CON ARRASTRE Y MEDIOS DE ORIENTACION, COMPRENDIENDO AL MENOS UN GENERADOR DE GAS (4), Y TOBERAS (5) CONECTADAS A ESTE ULTIMO. LOS MEDIOS DE ORIENTACION ESTAN SITUADOS EN UN CUERPO ANULAR (3), CONECTADO RIGIDAMENTE A LA PARTE TRASERA DEL CUERPO DEL MISIL. LA SUPERFICIE INTERNA DEL CUERPO ANULAR ESTA REALIZADA EN FORMA CONICA Y RECUBIERTA POR MATERIAL TERMOAISLANTE, QUE FORMA UNA CONDUCCION DE GAS, (7) CUYO PERFIL ES LA CONTINUACION DEL PERFIL DE LA TOBERA (6) DEL MOTOR DE CRUCERO DEL MISIL.
ES95936617T 1994-10-27 1995-10-27 Sistema de lanzamiento y de orientacion de ingenios volantes. Expired - Lifetime ES2107921T3 (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
RU94040077 1994-10-27
RU95110350A RU2082946C1 (ru) 1995-07-03 1995-07-03 Исполнительная система старта и ориентации ракеты

Publications (1)

Publication Number Publication Date
ES2107921T3 true ES2107921T3 (es) 1997-12-01

Family

ID=26653804

Family Applications (1)

Application Number Title Priority Date Filing Date
ES95936617T Expired - Lifetime ES2107921T3 (es) 1994-10-27 1995-10-27 Sistema de lanzamiento y de orientacion de ingenios volantes.

Country Status (14)

Country Link
US (1) US5823469A (es)
EP (1) EP0737297B1 (es)
JP (1) JP3692537B2 (es)
KR (1) KR100404037B1 (es)
AU (1) AU708097B2 (es)
DE (1) DE69500842T2 (es)
DK (1) DK0737297T3 (es)
ES (1) ES2107921T3 (es)
FI (1) FI111032B (es)
IL (1) IL115749A (es)
NO (1) NO310637B1 (es)
TW (1) TW319825B (es)
UA (1) UA27153C2 (es)
WO (1) WO1996013694A1 (es)

Families Citing this family (28)

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US6584907B2 (en) * 2000-03-17 2003-07-01 Ensign-Bickford Aerospace & Defense Company Ordnance firing system
US6779462B2 (en) 2001-06-04 2004-08-24 Raytheon Company Kinetic energy rod warhead with optimal penetrators
US6598534B2 (en) * 2001-06-04 2003-07-29 Raytheon Company Warhead with aligned projectiles
US7624682B2 (en) * 2001-08-23 2009-12-01 Raytheon Company Kinetic energy rod warhead with lower deployment angles
US7624683B2 (en) 2001-08-23 2009-12-01 Raytheon Company Kinetic energy rod warhead with projectile spacing
US8127686B2 (en) 2001-08-23 2012-03-06 Raytheon Company Kinetic energy rod warhead with aiming mechanism
US7621222B2 (en) * 2001-08-23 2009-11-24 Raytheon Company Kinetic energy rod warhead with lower deployment angles
US6910423B2 (en) * 2001-08-23 2005-06-28 Raytheon Company Kinetic energy rod warhead with lower deployment angles
US7017496B2 (en) 2002-08-29 2006-03-28 Raytheon Company Kinetic energy rod warhead with imploding charge for isotropic firing of the penetrators
US7415917B2 (en) * 2002-08-29 2008-08-26 Raytheon Company Fixed deployed net for hit-to-kill vehicle
US20060021538A1 (en) * 2002-08-29 2006-02-02 Lloyd Richard M Kinetic energy rod warhead deployment system
US6931994B2 (en) * 2002-08-29 2005-08-23 Raytheon Company Tandem warhead
CA2541786C (en) 2003-10-14 2008-12-30 Raytheon Company Mine counter measure system
US6920827B2 (en) * 2003-10-31 2005-07-26 Raytheon Company Vehicle-borne system and method for countering an incoming threat
US20090320711A1 (en) 2004-11-29 2009-12-31 Lloyd Richard M Munition
FR2891618B1 (fr) * 2005-10-05 2010-06-11 Giat Ind Sa Dispositif d'entrainement de gouvernes de projectile.
US8418623B2 (en) 2010-04-02 2013-04-16 Raytheon Company Multi-point time spacing kinetic energy rod warhead and system
FR2980265B1 (fr) 2011-09-21 2017-02-24 Mbda France Systeme pour le pilotage d'un engin volant a l'aide de paires de tuyeres laterales
US9372055B2 (en) * 2014-01-31 2016-06-21 The Boeing Company Passive control fin stops for air launched boosted (two stage) high speed vehicles
CN105224778A (zh) * 2014-06-09 2016-01-06 上海机电工程研究所 通用杀伤区计算方法及通用发射区计算方法
RU2563302C1 (ru) * 2014-09-03 2015-09-20 Открытое акционерное общество "Научно-производственное объединение "СПЛАВ" Хвостовой блок управляемого реактивного снаряда, запускаемого из трубчатой направляющей
CN106481482B (zh) * 2015-08-26 2018-07-06 上海宇航系统工程研究所 一种小型液体发动机防热导流结构
RU2639839C1 (ru) * 2016-12-07 2017-12-22 Акционерное общество "Государственное машиностроительное конструкторское бюро "Вымпел" имени И.И. Торопова" Устройство для пуска управляемого снаряда
CN108007280B (zh) * 2017-12-28 2023-08-15 北京威标至远科技发展有限公司 一种舵机防热结构
RU183575U1 (ru) * 2018-05-18 2018-09-26 Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка Летательный аппарат со стартовой двигательной установкой в транспортно-пусковом контейнере
IL269920B1 (en) * 2019-10-10 2024-06-01 Israel Aerospace Ind Ltd missile direction
KR102125947B1 (ko) 2020-03-30 2020-06-23 정종만 용기 운반용 홀더
KR102502552B1 (ko) * 2020-12-07 2023-02-21 이병준 터빈장치

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US2995319A (en) * 1958-10-09 1961-08-08 Richard B Kershner A pre-boost control device for aerial missiles
US3499364A (en) * 1959-11-19 1970-03-10 Us Navy Apparatus for submerged launching of missiles
US3084600A (en) * 1961-02-01 1963-04-09 Atlantic Res Corp Rocket launchers
US3251267A (en) * 1963-06-18 1966-05-17 Emerson Electric Co Spin rocket and launcher
US3218974A (en) * 1964-03-24 1965-11-23 Samms Adolphus Air breathing booster
US3329089A (en) * 1964-12-24 1967-07-04 Herbert L Harrison Retention-release mechanism for reaction motors and rocket interstages
US3340691A (en) * 1965-10-14 1967-09-12 Thiokol Chemical Corp Command controllable self-pressurizing liquid injection system
US3495408A (en) * 1967-11-08 1970-02-17 United Aircraft Corp Self-actuating nozzle plug
US3855789A (en) * 1968-04-05 1974-12-24 Us Navy Explosive coupling assembly
US3914935A (en) * 1969-03-17 1975-10-28 Rockwell International Corp Dual area nozzle
US3568448A (en) * 1969-04-01 1971-03-09 Thiokol Chemical Corp Ignition system for igniting a gas generator by the use of combustion gases from a solid propellant rocket motor having selective zoning capabilities
US3752425A (en) * 1970-10-28 1973-08-14 Europ Propulsion Self-propelled non-guided missiles
GB1537469A (en) * 1975-12-23 1978-12-29 Imi Kynoch Ltd Disintegrable member for controlling flow between pressure chambers
US4050351A (en) * 1976-05-04 1977-09-27 Societe Anonyme Dite: Societe Europeenne Depropulsion Assembly for launching a projectile
FR2376301A1 (fr) * 1976-12-28 1978-07-28 Luchaire Sa Engin autopropulse a etages separables
FR2376300A1 (fr) * 1976-12-28 1978-07-28 Luchaire Sa Dispositif pour la liaison entre deux etages d'un engin autopropulse
US4364530A (en) * 1980-09-08 1982-12-21 The United States Of America As Represented By The Secretary Of The Navy Propulsion/control modular booster
FR2544020B1 (fr) * 1983-04-05 1989-04-21 British Aerospace Moyen permettant la separation en vol des etages des moteurs d'un projectile
GB8324899D0 (en) * 1983-09-16 1983-10-19 Secr Defence Rocket motors
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IL79864A (en) * 1985-11-25 1994-05-30 Hughes Aircraft Co Detachable mechanism for creating a directed thrust for an aeronautical vehicle
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US5400713A (en) * 1994-03-09 1995-03-28 Thiokol Corporation Stage separation and thrust reduction apparatus

Also Published As

Publication number Publication date
JPH09507567A (ja) 1997-07-29
AU3848195A (en) 1996-05-23
NO310637B1 (no) 2001-07-30
JP3692537B2 (ja) 2005-09-07
UA27153C2 (uk) 2000-02-28
US5823469A (en) 1998-10-20
KR100404037B1 (ko) 2004-03-24
NO962653L (no) 1996-08-27
DK0737297T3 (da) 1997-12-22
IL115749A0 (en) 1996-01-19
FI962638A (fi) 1996-08-23
WO1996013694A1 (fr) 1996-05-09
TW319825B (es) 1997-11-11
NO962653D0 (no) 1996-06-21
FI962638A0 (fi) 1996-06-26
EP0737297B1 (fr) 1997-10-08
AU708097B2 (en) 1999-07-29
FI111032B (fi) 2003-05-15
EP0737297A1 (fr) 1996-10-16
DE69500842T2 (de) 1998-02-26
IL115749A (en) 2000-02-29
DE69500842D1 (de) 1997-11-13

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