GB2343424B - Transverse thrust control arrangement for missiles - Google Patents

Transverse thrust control arrangement for missiles

Info

Publication number
GB2343424B
GB2343424B GB9824042A GB9824042A GB2343424B GB 2343424 B GB2343424 B GB 2343424B GB 9824042 A GB9824042 A GB 9824042A GB 9824042 A GB9824042 A GB 9824042A GB 2343424 B GB2343424 B GB 2343424B
Authority
GB
United Kingdom
Prior art keywords
missiles
control arrangement
thrust control
transverse thrust
transverse
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 - Fee Related
Application number
GB9824042A
Other versions
GB2343424A (en
GB9824042D0 (en
Inventor
Karl Smirra
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.)
LFK Lenkflugkoerpersysteme GmbH
Original Assignee
LFK Lenkflugkoerpersysteme GmbH
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 to DE19735279A priority Critical patent/DE19735279C1/en
Priority to FR9809785A priority patent/FR2767382B1/en
Priority to IT1998MI001868A priority patent/IT1302150B1/en
Priority to NO19985004A priority patent/NO311454B1/en
Application filed by LFK Lenkflugkoerpersysteme GmbH filed Critical LFK Lenkflugkoerpersysteme GmbH
Priority to GB9824042A priority patent/GB2343424B/en
Publication of GB9824042D0 publication Critical patent/GB9824042D0/en
Publication of GB2343424A publication Critical patent/GB2343424A/en
Application granted granted Critical
Publication of GB2343424B publication Critical patent/GB2343424B/en
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F02K9/86—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using nozzle throats of adjustable cross- section
    • 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
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Fluid Mechanics (AREA)
  • Physics & Mathematics (AREA)
  • Air Bags (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Feeding, Discharge, Calcimining, Fusing, And Gas-Generation Devices (AREA)
  • Tents Or Canopies (AREA)
  • Mechanically-Actuated Valves (AREA)
  • Exhaust Gas After Treatment (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
GB9824042A 1997-08-14 1998-11-03 Transverse thrust control arrangement for missiles Expired - Fee Related GB2343424B (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
DE19735279A DE19735279C1 (en) 1997-08-14 1997-08-14 Cross thrust control arrangement for missiles with solid hot gas generator
FR9809785A FR2767382B1 (en) 1997-08-14 1998-07-30 TRANSVERSE THRUST CONTROL DEVICE FOR MISSILES, INCLUDING A HOT GAS GENERATOR OF SOLID MATERIAL
IT1998MI001868A IT1302150B1 (en) 1997-08-14 1998-08-07 COMMAND ARRANGEMENT OF TRANSVERSAL JETS FOR AERODINE HOT GAS CONGENERATOR WITH SOLID PROPELLENT.
NO19985004A NO311454B1 (en) 1997-08-14 1998-10-27 Transverse sliding control device for aircraft bodies with solid gas generator
GB9824042A GB2343424B (en) 1997-08-14 1998-11-03 Transverse thrust control arrangement for missiles

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE19735279A DE19735279C1 (en) 1997-08-14 1997-08-14 Cross thrust control arrangement for missiles with solid hot gas generator
NO19985004A NO311454B1 (en) 1997-08-14 1998-10-27 Transverse sliding control device for aircraft bodies with solid gas generator
GB9824042A GB2343424B (en) 1997-08-14 1998-11-03 Transverse thrust control arrangement for missiles

Publications (3)

Publication Number Publication Date
GB9824042D0 GB9824042D0 (en) 1998-12-30
GB2343424A GB2343424A (en) 2000-05-10
GB2343424B true GB2343424B (en) 2001-06-13

Family

ID=27217648

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9824042A Expired - Fee Related GB2343424B (en) 1997-08-14 1998-11-03 Transverse thrust control arrangement for missiles

Country Status (5)

Country Link
DE (1) DE19735279C1 (en)
FR (1) FR2767382B1 (en)
GB (1) GB2343424B (en)
IT (1) IT1302150B1 (en)
NO (1) NO311454B1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107314716A (en) * 2017-07-13 2017-11-03 王海龙 One kind tracking emitter

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102582827A (en) * 2012-02-11 2012-07-18 黄廷华 Flying device capable of moving randomly
DE102017129941A1 (en) 2017-12-14 2019-06-19 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Valve for a controllable transverse thrust engine
DE102017130117A1 (en) 2017-12-15 2019-06-19 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Around an axis rotatable valve body for a controllable transverse thrust engine

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4017040A (en) * 1976-01-12 1977-04-12 The United States Of America As Represented By The Secretary Of The Navy Steerable extraction rocket
US4463921A (en) * 1981-04-21 1984-08-07 Thomson-Brandt Gas jet steering device and method missile comprising such a device
GB2176446A (en) * 1985-06-04 1986-12-31 Messerschmitt Boelkow Blohm A braking and releasing mechanism for a steering nozzle body
EP0309327A1 (en) * 1987-09-18 1989-03-29 Thomson-Brandt Armements Lateral jet-commutating device for steering missiles
US5016835A (en) * 1989-01-14 1991-05-21 Messerschmitt-Bolkow-Blohm Gmbh Guided missile
GB2316464A (en) * 1996-08-14 1998-02-25 Moog Inc Hot gas control valve

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3537079C1 (en) * 1985-10-18 1987-02-19 Messerschmitt Boelkow Blohm Quick-acting fluid control valve esp. for supersonic aircraft - has piston actuated by gas to deflect retaining balls
FR2659734B1 (en) * 1990-03-14 1992-07-03 Aerospatiale SYSTEM FOR THE PILOTAGE OF A MISSILE USING LATERAL GAS JETS.
FR2730302B1 (en) * 1995-02-03 1997-03-14 Tda Armements Sas CONTROL OF A PROJECTILE BY MULTI-CHAMBER AND SINGLE-TUBE IMPELLER

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4017040A (en) * 1976-01-12 1977-04-12 The United States Of America As Represented By The Secretary Of The Navy Steerable extraction rocket
US4463921A (en) * 1981-04-21 1984-08-07 Thomson-Brandt Gas jet steering device and method missile comprising such a device
GB2176446A (en) * 1985-06-04 1986-12-31 Messerschmitt Boelkow Blohm A braking and releasing mechanism for a steering nozzle body
EP0309327A1 (en) * 1987-09-18 1989-03-29 Thomson-Brandt Armements Lateral jet-commutating device for steering missiles
US5016835A (en) * 1989-01-14 1991-05-21 Messerschmitt-Bolkow-Blohm Gmbh Guided missile
GB2316464A (en) * 1996-08-14 1998-02-25 Moog Inc Hot gas control valve

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107314716A (en) * 2017-07-13 2017-11-03 王海龙 One kind tracking emitter
CN107314716B (en) * 2017-07-13 2019-02-12 乐清市拓展机械科技有限公司 A kind of tracking emitter

Also Published As

Publication number Publication date
ITMI981868A1 (en) 2000-02-07
NO311454B1 (en) 2001-11-26
GB2343424A (en) 2000-05-10
ITMI981868A0 (en) 1998-08-07
NO985004D0 (en) 1998-10-27
FR2767382B1 (en) 2003-10-03
DE19735279C1 (en) 1999-03-11
NO985004L (en) 2000-04-28
IT1302150B1 (en) 2000-07-31
GB9824042D0 (en) 1998-12-30
FR2767382A1 (en) 1999-02-19

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 20111103