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 MISSILESInfo
- 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
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)
- 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)
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)
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)
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 |
-
1979
- 1979-09-10 GB GB07931390A patent/GB2164612B/en not_active Expired
-
1981
- 1981-02-03 FR FR8102373A patent/FR2585667A1/en not_active Withdrawn
- 1981-04-03 IT IT86211/81A patent/IT1172212B/en active
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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