IT8186211A0 - IMPROVEMENT IN VEHICLES EQUIPPED WITH A THRUST VECTOR CONTROL SYSTEM, PARTICULARLY GUIDED MISSILES - Google Patents

IMPROVEMENT IN VEHICLES EQUIPPED WITH A THRUST VECTOR CONTROL SYSTEM, PARTICULARLY GUIDED MISSILES

Info

Publication number
IT8186211A0
IT8186211A0 IT8186211A IT8621181A IT8186211A0 IT 8186211 A0 IT8186211 A0 IT 8186211A0 IT 8186211 A IT8186211 A IT 8186211A IT 8621181 A IT8621181 A IT 8621181A IT 8186211 A0 IT8186211 A0 IT 8186211A0
Authority
IT
Italy
Prior art keywords
improvement
control system
vector control
vehicles equipped
thrust vector
Prior art date
Application number
IT8186211A
Other languages
Italian (it)
Other versions
IT1172212B (en
Inventor
Malcom A Hicks
Carol L Priest
Original Assignee
Sperry Ltd
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 Sperry Ltd filed Critical Sperry Ltd
Publication of IT8186211A0 publication Critical patent/IT8186211A0/en
Application granted granted Critical
Publication of IT1172212B publication Critical patent/IT1172212B/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63GOFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
    • B63G8/00Underwater vessels, e.g. submarines; Equipment specially adapted therefor
    • B63G8/14Control of attitude or depth
    • B63G8/18Control of attitude or depth by hydrofoils
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/84Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using movable nozzles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/60Steering arrangements
    • F42B10/62Steering by movement of flight surfaces
    • F42B10/64Steering by movement of flight surfaces of fins
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/60Steering arrangements
    • F42B10/66Steering by varying intensity or direction of thrust
    • F42B10/666Steering by varying intensity or direction of thrust characterised by using a nozzle rotatable about an axis transverse to the axis of the projectile
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B19/00Marine torpedoes, e.g. launched by surface vessels or submarines; Sea mines having self-propulsion means
    • F42B19/01Steering control
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B19/00Marine torpedoes, e.g. launched by surface vessels or submarines; Sea mines having self-propulsion means
    • F42B19/12Propulsion specially adapted for torpedoes
    • F42B19/26Propulsion 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)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
IT86211/81A 1979-09-10 1981-04-03 IMPROVEMENT IN VEHICLES EQUIPPED WITH A PUSHING VECTOR CONTROL SYSTEM, IN PARTICULAR GUIDED MISSILES IT1172212B (en)

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
IT8186211A0 true IT8186211A0 (en) 1981-04-03
IT1172212B IT1172212B (en) 1987-06-18

Family

ID=10507739

Family Applications (1)

Application Number Title Priority Date Filing Date
IT86211/81A IT1172212B (en) 1979-09-10 1981-04-03 IMPROVEMENT IN VEHICLES EQUIPPED WITH A PUSHING VECTOR CONTROL SYSTEM, IN PARTICULAR GUIDED MISSILES

Country Status (3)

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

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
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
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

Also Published As

Publication number Publication date
GB2164612B (en) 1986-09-03
FR2585667A1 (en) 1987-02-06
GB2164612A (en) 1986-03-26
IT1172212B (en) 1987-06-18

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