DE69500842D1 - Abschlussvorrichtung und mit einer lenkvorrichtung versehene rakete - Google Patents

Abschlussvorrichtung und mit einer lenkvorrichtung versehene rakete

Info

Publication number
DE69500842D1
DE69500842D1 DE69500842T DE69500842T DE69500842D1 DE 69500842 D1 DE69500842 D1 DE 69500842D1 DE 69500842 T DE69500842 T DE 69500842T DE 69500842 T DE69500842 T DE 69500842T DE 69500842 D1 DE69500842 D1 DE 69500842D1
Authority
DE
Germany
Prior art keywords
rocket
steering
locking device
locking
steering device
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
DE69500842T
Other languages
English (en)
Other versions
DE69500842T2 (de
Inventor
Ivan Arkhangelsky
Eugene Bolotov
Vladimir Philippov
Vladimir Mizrokhi
Vladimir Svetlov
Gregory Stanevsky
Serge Khitenkov
Victor Gaidoukevitch
Eugene Chmikov
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.)
Thales SA
LE BUREAU DE CONST MECANIQUES
Original Assignee
Thomson CSF SA
LE BUREAU DE CONST MECANIQUES
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 Thomson CSF SA, LE BUREAU DE CONST MECANIQUES filed Critical Thomson CSF SA
Publication of DE69500842D1 publication Critical patent/DE69500842D1/de
Application granted granted Critical
Publication of DE69500842T2 publication Critical patent/DE69500842T2/de
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)
DE69500842T 1994-10-27 1995-10-27 Abschlussvorrichtung und mit einer lenkvorrichtung versehene rakete Expired - Lifetime DE69500842T2 (de)

Applications Claiming Priority (3)

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
PCT/FR1995/001423 WO1996013694A1 (fr) 1994-10-27 1995-10-27 Systeme de lancement et d'orientation d'engins volants

Publications (2)

Publication Number Publication Date
DE69500842D1 true DE69500842D1 (de) 1997-11-13
DE69500842T2 DE69500842T2 (de) 1998-02-26

Family

ID=26653804

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69500842T Expired - Lifetime DE69500842T2 (de) 1994-10-27 1995-10-27 Abschlussvorrichtung und mit einer lenkvorrichtung versehene rakete

Country Status (14)

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

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
US6598534B2 (en) * 2001-06-04 2003-07-29 Raytheon Company Warhead with aligned projectiles
US6779462B2 (en) 2001-06-04 2004-08-24 Raytheon Company Kinetic energy rod warhead with optimal penetrators
US7624683B2 (en) 2001-08-23 2009-12-01 Raytheon Company Kinetic energy rod warhead with projectile spacing
US7624682B2 (en) * 2001-08-23 2009-12-01 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
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
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
GB8417706D0 (en) * 1984-07-11 1994-01-26 British Aerospace Spin rate variation of spinning bodies
DE3686321T2 (de) * 1985-10-31 1992-12-17 British Aerospace Ausstossantrieb fuer flugkoerper.
IL79864A (en) * 1985-11-25 1994-05-30 Hughes Aircraft Co Detachable mechanism for creating a directed thrust for an aeronautical vehicle
GB8611406D0 (en) * 1986-05-09 1986-08-20 Lucas Ind Plc Missile flight control system
DE3789956T2 (de) * 1986-08-15 1994-11-10 Advanced Polymer Systems Inc Polymere trägerzubereitungen, herstellung und verwendung.
GB8803164D0 (en) * 1988-02-11 1988-08-24 British Aerospace Reaction control system
US4853827A (en) * 1988-08-01 1989-08-01 Rogers Corporation High dielectric multilayer capacitor
US5400713A (en) * 1994-03-09 1995-03-28 Thiokol Corporation Stage separation and thrust reduction apparatus

Also Published As

Publication number Publication date
AU3848195A (en) 1996-05-23
FI962638A (fi) 1996-08-23
FI962638A0 (fi) 1996-06-26
NO962653L (no) 1996-08-27
NO310637B1 (no) 2001-07-30
UA27153C2 (uk) 2000-02-28
EP0737297A1 (de) 1996-10-16
DE69500842T2 (de) 1998-02-26
IL115749A0 (en) 1996-01-19
AU708097B2 (en) 1999-07-29
US5823469A (en) 1998-10-20
EP0737297B1 (de) 1997-10-08
WO1996013694A1 (fr) 1996-05-09
ES2107921T3 (es) 1997-12-01
NO962653D0 (no) 1996-06-21
JPH09507567A (ja) 1997-07-29
FI111032B (fi) 2003-05-15
DK0737297T3 (da) 1997-12-22
TW319825B (de) 1997-11-11
IL115749A (en) 2000-02-29
JP3692537B2 (ja) 2005-09-07
KR100404037B1 (ko) 2004-03-24

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition