GB2164612B - Vehicles fitted with thrust vector control systems - Google Patents

Vehicles fitted with thrust vector control systems

Info

Publication number
GB2164612B
GB2164612B GB07931390A GB7931390A GB2164612B GB 2164612 B GB2164612 B GB 2164612B GB 07931390 A GB07931390 A GB 07931390A GB 7931390 A GB7931390 A GB 7931390A GB 2164612 B GB2164612 B GB 2164612B
Authority
GB
United Kingdom
Prior art keywords
control systems
vector control
thrust vector
vehicles fitted
vehicles
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
Application number
GB07931390A
Other versions
GB2164612A (en
Inventor
Malcolm Anthony Hicks
Carol Lynne Priest
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.)
BAE Systems PLC
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
Priority to GB07931390A priority Critical patent/GB2164612B/en
Priority to FR8102373A priority patent/FR2585667A1/en
Priority to IT86211/81A priority patent/IT1172212B/en
Publication of GB2164612A publication Critical patent/GB2164612A/en
Application granted granted Critical
Publication of GB2164612B publication Critical patent/GB2164612B/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63G—OFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
    • B63G8/00—Underwater vessels, e.g. submarines; Equipment specially adapted therefor
    • B63G8/14—Control of attitude or depth
    • B63G8/18—Control of attitude or depth by hydrofoils
    • 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
    • F02K9/84—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using movable 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
    • F42B10/62—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
    • F42B10/666—Steering by varying intensity or direction of thrust characterised by using a nozzle rotatable about an axis transverse to the axis of the projectile
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B19/00—Marine torpedoes, e.g. launched by surface vessels or submarines; Sea mines having self-propulsion means
    • F42B19/01—Steering control
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B19/00—Marine torpedoes, e.g. launched by surface vessels or submarines; Sea mines having self-propulsion means
    • F42B19/12—Propulsion specially adapted for torpedoes
    • F42B19/26—Propulsion specially adapted for torpedoes by jet propulsion

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
GB07931390A 1979-09-10 1979-09-10 Vehicles fitted with thrust vector control systems Expired GB2164612B (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GB07931390A GB2164612B (en) 1979-09-10 1979-09-10 Vehicles fitted with thrust vector control systems
FR8102373A FR2585667A1 (en) 1979-09-10 1981-02-03 VEHICLE WITH PUSHED VECTOR ADJUSTMENT SYSTEM
IT86211/81A IT1172212B (en) 1979-09-10 1981-04-03 IMPROVEMENT IN VEHICLES EQUIPPED WITH A PUSHING VECTOR CONTROL SYSTEM, IN PARTICULAR GUIDED MISSILES

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB07931390A GB2164612B (en) 1979-09-10 1979-09-10 Vehicles fitted with thrust vector control systems

Publications (2)

Publication Number Publication Date
GB2164612A GB2164612A (en) 1986-03-26
GB2164612B true GB2164612B (en) 1986-09-03

Family

ID=10507739

Family Applications (1)

Application Number Title Priority Date Filing Date
GB07931390A Expired GB2164612B (en) 1979-09-10 1979-09-10 Vehicles fitted with thrust vector control systems

Country Status (3)

Country Link
FR (1) FR2585667A1 (en)
GB (1) GB2164612B (en)
IT (1) IT1172212B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107792325A (en) * 2017-10-12 2018-03-13 中国船舶重工集团公司第七〇九研究所 Suitable for the tail integration structure and its steering method of micro-unmanned submariner device

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB8721291D0 (en) * 1987-09-10 1990-05-16 British Aerospace Projectile guidance
US5806791A (en) * 1995-05-26 1998-09-15 Raytheon Company Missile jet vane control system and method
DE19624187C1 (en) * 1996-06-18 1998-01-15 Diehl Gmbh & Co rocket
DE102012210499A1 (en) * 2012-06-21 2013-12-24 Thyssenkrupp Marine Systems Gmbh submarine
US9630686B2 (en) 2013-03-15 2017-04-25 Hadal, Inc. Systems and methods for pressure tolerant energy systems
DE102016004363A1 (en) * 2015-08-27 2017-03-02 Diehl Bgt Defence Gmbh & Co. Kg Flight control device for a missile and method for steering a missile
DE102018005480A1 (en) * 2018-07-11 2020-01-16 Mbda Deutschland Gmbh missile
US11781844B2 (en) * 2021-08-03 2023-10-10 Raytheon Company Missile component attachment assembly

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB829183A (en) * 1955-04-11 1960-03-02 Aerotecnica S A Improvements in rotary-wing aircraft
GB844254A (en) * 1956-06-01 1960-08-10 Alexandre Korganoff Improvements in or relating to submarines
BE584539A (en) * 1959-05-02 1960-03-01 Messerschmitt Boelkow Blohm Jet plane for takeoff and landing with minimum bearings.
US3240448A (en) * 1962-07-13 1966-03-15 Messerschmitt Ag Tail and elevator construction for airplanes
GB1176465A (en) * 1966-03-25 1970-01-01 Hydroconic Ltd Improvements in or relating to Ships' Steering and Propulsion Equipment

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107792325A (en) * 2017-10-12 2018-03-13 中国船舶重工集团公司第七〇九研究所 Suitable for the tail integration structure and its steering method of micro-unmanned submariner device
CN107792325B (en) * 2017-10-12 2020-04-14 中国船舶重工集团公司第七一九研究所 Tail integrated structure suitable for miniature unmanned underwater vehicle and steering method thereof

Also Published As

Publication number Publication date
IT8186211A0 (en) 1981-04-03
FR2585667A1 (en) 1987-02-06
GB2164612A (en) 1986-03-26
IT1172212B (en) 1987-06-18

Similar Documents

Publication Publication Date Title
GB2040513B (en) Active nutation control system for space vehicle
JPS55153004A (en) Control system
GB2062290B (en) Fuel control system
GB2018472A (en) Attitude control system
GB2039619B (en) Rocket propulsion system
ZA792694B (en) Vehicle speed control systems
GB2060952B (en) Control system
GB2041582B (en) Position control system
ZA804694B (en) Speed control systems
GB1520393A (en) Aircraft control system
DE2961986D1 (en) Vehicle control system with conditional transmission-brake interlock
GB2067488B (en) Driverless vehicle with speed control
DE2964416D1 (en) Vehicle propulsion control systems
GB2164612B (en) Vehicles fitted with thrust vector control systems
DE2861521D1 (en) Vehicle control system
GB2054229B (en) Vehicle control system
GB2065836B (en) Engine control systems
GB2060809B (en) Bowden control system
GB2041604B (en) Override arrangement for vehicle control system
GB2056392B (en) Attitude control system for spacecraft utilizing the thruster plume
GB1549544A (en) Attitude control systems for space vehicles
JPS55129082A (en) Cable control type aircraft
JPS5692700A (en) Overall parkingglot control system
GB2056125B (en) Vehicle speed control system
AU533101B2 (en) Conveyor system with driverless vehicle

Legal Events

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