DE68927060D1 - Mittels Schubvektorsteuerung arbeitende Lenkvorrichtung für einen Flugkörper - Google Patents

Mittels Schubvektorsteuerung arbeitende Lenkvorrichtung für einen Flugkörper

Info

Publication number
DE68927060D1
DE68927060D1 DE68927060T DE68927060T DE68927060D1 DE 68927060 D1 DE68927060 D1 DE 68927060D1 DE 68927060 T DE68927060 T DE 68927060T DE 68927060 T DE68927060 T DE 68927060T DE 68927060 D1 DE68927060 D1 DE 68927060D1
Authority
DE
Germany
Prior art keywords
steering device
vector control
thrust vector
missile operating
missile
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
DE68927060T
Other languages
English (en)
Other versions
DE68927060T2 (de
Inventor
Anthony Machell
Peter G Foulsham
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.)
MBDA UK Ltd
Original Assignee
British Aerospace PLC
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 British Aerospace PLC filed Critical British Aerospace PLC
Application granted granted Critical
Publication of DE68927060D1 publication Critical patent/DE68927060D1/de
Publication of DE68927060T2 publication Critical patent/DE68927060T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • F02K9/88—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using auxiliary rocket nozzles
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Transmission Devices (AREA)
DE68927060T 1988-02-11 1989-02-10 Mittels Schubvektorsteuerung arbeitende Lenkvorrichtung für einen Flugkörper Expired - Lifetime DE68927060T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB888803164A GB8803164D0 (en) 1988-02-11 1988-02-11 Reaction control system

Publications (2)

Publication Number Publication Date
DE68927060D1 true DE68927060D1 (de) 1996-10-02
DE68927060T2 DE68927060T2 (de) 1997-01-23

Family

ID=10631525

Family Applications (2)

Application Number Title Priority Date Filing Date
DE8989301284T Expired - Lifetime DE68902655T2 (de) 1988-02-11 1989-02-10 Stabilisierung und lageaenderung durch kleine triebwerke.
DE68927060T Expired - Lifetime DE68927060T2 (de) 1988-02-11 1989-02-10 Mittels Schubvektorsteuerung arbeitende Lenkvorrichtung für einen Flugkörper

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE8989301284T Expired - Lifetime DE68902655T2 (de) 1988-02-11 1989-02-10 Stabilisierung und lageaenderung durch kleine triebwerke.

Country Status (4)

Country Link
US (1) US4955558A (de)
EP (2) EP0489712B1 (de)
DE (2) DE68902655T2 (de)
GB (1) GB8803164D0 (de)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6231003B1 (en) * 1990-03-12 2001-05-15 The Boeing Company Apparatus for defending a vehicle against an approaching threat
USH1098H (en) 1991-02-20 1992-09-01 Hallum Charles E Integrated valve assembly
FR2684723B1 (fr) * 1991-12-10 1995-05-19 Thomson Csf Propulseur a propergol solide a poussee modulable et missile equipe.
GB2504254B (en) * 1992-04-30 2014-11-26 Loral Aerospace Corp Walking beam hot gas valve
US6460801B1 (en) * 1993-11-18 2002-10-08 Lockheed Martin Corp. Precision guidance system for aircraft launched bombs
US6254031B1 (en) * 1994-08-24 2001-07-03 Lockhead Martin Corporation Precision guidance system for aircraft launched bombs
IL115749A (en) * 1994-10-27 2000-02-29 Thomson Csf Missile launching and orientating system
US5631830A (en) * 1995-02-03 1997-05-20 Loral Vought Systems Corporation Dual-control scheme for improved missle maneuverability
US5590850A (en) * 1995-06-05 1997-01-07 Hughes Missile Systems Company Blended missile autopilot
JP3027558B2 (ja) 1997-08-29 2000-04-04 川崎重工業株式会社 推力制御ノズル
US6315239B1 (en) * 1997-09-23 2001-11-13 Versatron, Inc. Variable coupling arrangement for an integrated missile steering system
US6308911B1 (en) 1998-10-30 2001-10-30 Lockheed Martin Corp. Method and apparatus for rapidly turning a vehicle in a fluid medium
US6780170B2 (en) 2002-05-15 2004-08-24 Liebel-Flarsheim Company Hydraulic remote for a medical fluid injector
JP3788973B2 (ja) 2003-02-19 2006-06-21 川崎重工業株式会社 推力制御バルブ
US7509796B2 (en) * 2006-09-13 2009-03-31 Aerojet-General Corporation Pintle-controlled propulsion system with external dynamic seal
US8735788B2 (en) * 2011-02-18 2014-05-27 Raytheon Company Propulsion and maneuvering system with axial thrusters and method for axial divert attitude and control
US8816261B1 (en) * 2011-06-29 2014-08-26 Raytheon Company Bang-bang control using tangentially mounted surfaces
US9068808B2 (en) * 2013-01-17 2015-06-30 Raytheon Company Air vehicle with bilateral steering thrusters
DE102014004251A1 (de) * 2013-11-20 2015-06-25 Mbda Deutschland Gmbh Lenkflugkörper und Verfahren zum Lenken eines Lenkflugkörpers
DE102016101560A1 (de) * 2016-01-28 2017-08-03 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Querschubeinrichtung zur aktiven Bahn- und Lagesteuerung von Flugkörpern
DE102017130117A1 (de) * 2017-12-15 2019-06-19 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Um eine Achse drehbarer Ventilkörper für ein regelbares Querschubtriebwerk
JP6981894B2 (ja) 2018-02-23 2021-12-17 三菱重工業株式会社 スラスタ制御装置及びスラスタ制御方法
RU2770972C2 (ru) * 2019-08-30 2022-04-25 Акционерное общество "НПО Энергомаш имени академика В.П. Глушко" Блок сопел крена

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4085909A (en) * 1976-10-04 1978-04-25 Ford Motor Company Combined warm gas fin and reaction control servo
DE3144532A1 (de) * 1981-11-10 1983-05-19 Rheinmetall GmbH, 4000 Düsseldorf Fluegelstabilisiertes geschoss
FR2557926B1 (fr) * 1984-01-06 1986-04-11 Brandt Armements Propulseur a gaz pour projectile guide.
EP0201316A3 (de) * 1985-05-07 1987-08-19 The Garrett Corporation Vorrichtung zum Steuern eines selbstangetriebenen Körpers
DE3531686A1 (de) * 1985-09-05 1987-03-12 Rheinmetall Gmbh Steuerblock
GB8611406D0 (en) * 1986-05-09 1986-08-20 Lucas Ind Plc Missile flight control system
FR2620812B1 (fr) * 1987-09-18 1992-04-17 Thomson Brandt Armements Dispositif de commutation de jets de gaz lateraux destine au pilotage d'engins

Also Published As

Publication number Publication date
DE68902655T2 (de) 1993-01-28
DE68902655D1 (de) 1992-10-08
EP0489712A2 (de) 1992-06-10
EP0329342B1 (de) 1992-09-02
EP0489712B1 (de) 1996-08-28
GB8803164D0 (en) 1988-08-24
US4955558A (en) 1990-09-11
EP0489712A3 (en) 1993-02-03
EP0329342A1 (de) 1989-08-23
DE68927060T2 (de) 1997-01-23

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: MATRA BAE DYNAMICS (UK) LTD., STEVENAGE, HERTFORDS

8327 Change in the person/name/address of the patent owner

Owner name: MBDA UK LTD., STEVENAGE, HERTFORDSHIRE, GB