IL118251A - Missile control system and method for its use - Google Patents

Missile control system and method for its use

Info

Publication number
IL118251A
IL118251A IL118251A IL11825196A IL118251A IL 118251 A IL118251 A IL 118251A IL 118251 A IL118251 A IL 118251A IL 11825196 A IL11825196 A IL 11825196A IL 118251 A IL118251 A IL 118251A
Authority
IL
Israel
Prior art keywords
missile
control system
vanes
gear
detachable
Prior art date
Application number
IL118251A
Other languages
English (en)
Other versions
IL118251A0 (en
Original Assignee
Hughes Missile Systems
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 Hughes Missile Systems filed Critical Hughes Missile Systems
Publication of IL118251A0 publication Critical patent/IL118251A0/xx
Publication of IL118251A publication Critical patent/IL118251A/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/805—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control servo-mechanisms or control devices therefor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/90—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using deflectors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/97—Rocket nozzles
    • F02K9/978—Closures for nozzles; Nozzles comprising ejectable or discardable elements
    • 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
    • F42B10/62—Steering by movement of flight surfaces
    • F42B10/64—Steering by movement of flight surfaces of fins
    • 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
    • F42B10/665—Steering by varying intensity or direction of thrust characterised by using a nozzle provided with at least a deflector mounted within the nozzle

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
IL118251A 1995-05-26 1996-05-14 Missile control system and method for its use IL118251A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/452,211 US5806791A (en) 1995-05-26 1995-05-26 Missile jet vane control system and method

Publications (2)

Publication Number Publication Date
IL118251A0 IL118251A0 (en) 1996-09-12
IL118251A true IL118251A (en) 1998-04-05

Family

ID=23795545

Family Applications (1)

Application Number Title Priority Date Filing Date
IL118251A IL118251A (en) 1995-05-26 1996-05-14 Missile control system and method for its use

Country Status (9)

Country Link
US (1) US5806791A (no)
EP (2) EP0744591A3 (no)
AU (1) AU686050B2 (no)
CA (1) CA2176048C (no)
DE (1) DE69611940T2 (no)
ES (1) ES2154487T3 (no)
IL (1) IL118251A (no)
NO (1) NO309668B1 (no)
TR (1) TR961035A2 (no)

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US5631830A (en) 1995-02-03 1997-05-20 Loral Vought Systems Corporation Dual-control scheme for improved missle maneuverability
DE19632893C2 (de) * 1996-08-16 2001-02-08 Industrieanlagen Betr Sgmbh Ia Verfahren zur Herstellung von Flugkörperkomponenten aus faserverstärkter Keramik
DE19640540C1 (de) * 1996-10-01 1998-04-02 Daimler Benz Aerospace Ag Ruderstellsystem für einen Lenkflugkörper
US6308911B1 (en) 1998-10-30 2001-10-30 Lockheed Martin Corp. Method and apparatus for rapidly turning a vehicle in a fluid medium
US6668542B2 (en) 1999-10-27 2003-12-30 Allison Advanced Development Company Pulse detonation bypass engine propulsion pod
AU2001260966A1 (en) 2000-01-12 2001-08-07 Allison Advanced Development Company Propulsion module
US6450443B1 (en) 2000-08-17 2002-09-17 The United States Of America As Represented By The Secretary Of The Navy High torque 2.75-inch rocket nozzle
US6548794B2 (en) 2001-03-13 2003-04-15 Raytheon Company Dissolvable thrust vector control vane
DE10210433C1 (de) * 2002-03-09 2003-08-14 Dornier Gmbh Fluggerät zur IR-Flugzieldarstellung
US6726147B1 (en) * 2003-05-15 2004-04-27 Moog Inc. Multi-function actuator, and method of operating same
NO318772B1 (no) * 2003-09-24 2005-05-02 Nammo Raufoss As Rakettmotor med styrevinger i motorens dyse
DE102004037487A1 (de) 2004-07-27 2006-03-23 Deutsches Zentrum für Luft- und Raumfahrt e.V. Strahlruder und Verfahren zur Herstellung eines Strahlruders
US7026540B1 (en) * 2005-04-04 2006-04-11 The United States Of America As Represented By The Secretary Of The Navy Tailcone assembly for a submarine countermeasure
US7509903B2 (en) 2005-04-08 2009-03-31 Raytheon Company Separable structure material
FR2891618B1 (fr) * 2005-10-05 2010-06-11 Giat Ind Sa Dispositif d'entrainement de gouvernes de projectile.
CA2616982C (en) * 2005-10-13 2013-06-18 Raytheon Company Exhaust assembly for mass ejection drive system
US7800032B1 (en) * 2006-11-30 2010-09-21 Raytheon Company Detachable aerodynamic missile stabilizing system
US7755012B2 (en) * 2007-01-10 2010-07-13 Hr Textron, Inc. Eccentric drive control actuation system
US9341453B2 (en) * 2007-07-10 2016-05-17 Omnitek Partners, Llc Mechanical stepper motors for guided munitions and industrial machinery
US8110785B2 (en) * 2007-07-10 2012-02-07 Omnitek Partners Llc Mechanical stepper motors for gun-fired projectiles, mortars and missiles
US8117847B2 (en) 2008-03-07 2012-02-21 Raytheon Company Hybrid missile propulsion system with reconfigurable multinozzle grid
WO2010019299A2 (en) * 2008-05-21 2010-02-18 Raytheon Company Integral thrust vector and roll control system
KR102464125B1 (ko) 2009-02-02 2022-11-09 에어로바이론먼트, 인크. 멀티모드 무인 항공기
DE102009013150B4 (de) * 2009-03-06 2011-05-05 Deutsches Zentrum für Luft- und Raumfahrt e.V. Bauteil zum Einsatz in Heißgasströmungen
CN105151275B (zh) * 2009-09-09 2017-05-31 威罗门飞行公司 升降副翼控制系统
KR101973914B1 (ko) 2009-09-09 2019-04-29 에어로바이론먼트, 인크. 휴대용 ｒｆ 투명 발사관을 구비한 원격 조종 무인 항공기 포성 억제 발사장치를 위한 시스템 및 장치
US8436285B2 (en) 2010-07-26 2013-05-07 Raytheon Company Projectile that includes a fin adjustment mechanism with changing backlash
KR101244490B1 (ko) * 2010-10-27 2013-03-18 최용준 제트베인 분리식 발사체의 방향 조종 장치
CN104089546B (zh) * 2014-04-29 2015-09-30 北京理工大学 弹体的可变气动布局结构
KR101603154B1 (ko) 2014-08-26 2016-03-14 국방과학연구소 제트베인 분리가 가능한 통합형 구동장치
JP6361404B2 (ja) * 2014-09-17 2018-07-25 三菱重工業株式会社 推力偏向装置、および、推力偏向装置を備える飛しょう体
FR3041744B1 (fr) * 2015-09-29 2018-08-17 Nexter Munitions Projectile d'artillerie ayant une phase pilotee.
US10222189B2 (en) * 2016-07-22 2019-03-05 Raytheon Company Stage separation mechanism and method
CN107416213B (zh) * 2017-05-16 2020-03-24 上海航天控制技术研究所 一种带燃气舵的飞行器尾端防火结构
US10112691B1 (en) * 2017-06-12 2018-10-30 The Boeing Company Releasable forward section of an underwater vehicle
CN108915901B (zh) * 2018-07-26 2021-04-20 西安航天动力技术研究所 一种柔性喷管固定体与扩张段防错位结构及方法
RU2740978C1 (ru) * 2020-02-10 2021-01-22 Акционерное общество Московский научно-производственный комплекс "Авионика" имени О.В. Успенского (АО МНПК "Авионика") Блок рулевых приводов ракеты или снаряда
CN111946461A (zh) * 2020-07-27 2020-11-17 山东鑫聚龙动力科技集团有限公司 一种航天发动机用翼轴及其制造工艺
US11733011B2 (en) * 2020-11-24 2023-08-22 Raytheon Company Steering system with power take-off from actuators
US11879416B1 (en) 2022-09-09 2024-01-23 Raytheon Company Method for reducing jet tab exposure during thrust vectoring

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BE520064A (no) *
US2654552A (en) * 1948-02-24 1953-10-06 Northrop Aircraft Inc Movable jet deflector to compensate for destabilizing moment in a jet aircraft
US5082202A (en) * 1975-01-06 1992-01-21 The United States Of America As Represented By The Secretary Of The Navy Droppable jet vane TVC
US4063685A (en) * 1976-07-30 1977-12-20 The United States Of America As Represented By The Secretary Of The Army Thrust vector control by circulation control over aerodynamic surfaces in a supersonic nozzle
GB2164612B (en) * 1979-09-10 1986-09-03 British Aerospace Vehicles fitted with thrust vector control systems
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
NZ198917A (en) * 1980-11-14 1985-01-31 Commw Of Australia Rocket controlled by spoiler tabs in exhaust
DE3138869C2 (de) * 1981-09-30 1984-07-12 Messerschmitt-Bölkow-Blohm GmbH, 8000 München "Lenkflugkörper"
US4561357A (en) * 1982-09-15 1985-12-31 General Dynamics Pomona Division Steering mechanism for an explosively fired projectile
US4844380A (en) * 1985-11-25 1989-07-04 Hughes Aircraft Company Detachable thrust vector mechanism for an aeronautical vehicle
US4913379A (en) * 1988-02-23 1990-04-03 Japan as represented by Director General, Technical Research and Development Institute, Japan Defence Agency Rocket flight direction control system
US4867393A (en) * 1988-08-17 1989-09-19 Morton Thiokol, Inc. Reduced fin span thrust vector controlled pulsed tactical missile
US5511745A (en) * 1994-12-30 1996-04-30 Thiokol Corporation Vectorable nozzle having jet vanes

Also Published As

Publication number Publication date
TR961035A2 (tr) 1996-12-21
CA2176048C (en) 2000-02-29
EP0878688A1 (en) 1998-11-18
EP0744591A2 (en) 1996-11-27
ES2154487T3 (es) 2001-04-01
NO962105D0 (no) 1996-05-23
DE69611940T2 (de) 2001-06-13
AU5224096A (en) 1996-12-05
IL118251A0 (en) 1996-09-12
US5806791A (en) 1998-09-15
EP0744591A3 (en) 1997-12-03
EP0878688B1 (en) 2001-02-28
CA2176048A1 (en) 1996-11-27
AU686050B2 (en) 1998-01-29
NO962105L (no) 1996-11-27
DE69611940D1 (de) 2001-04-05
NO309668B1 (no) 2001-03-05

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Legal Events

Date Code Title Description
NP Permission for amending the patent specification granted (section 66, patents law 1967)
KB Patent renewed
KB Patent renewed
MM9K Patent not in force due to non-payment of renewal fees