IT1167303B - DIRECTION DEVICE FOR ROCKET AND SIMILAR AIRCRAFT WITH JET PROPULSION - Google Patents
DIRECTION DEVICE FOR ROCKET AND SIMILAR AIRCRAFT WITH JET PROPULSIONInfo
- Publication number
- IT1167303B IT1167303B IT68752/80A IT6875280A IT1167303B IT 1167303 B IT1167303 B IT 1167303B IT 68752/80 A IT68752/80 A IT 68752/80A IT 6875280 A IT6875280 A IT 6875280A IT 1167303 B IT1167303 B IT 1167303B
- Authority
- IT
- Italy
- Prior art keywords
- rocket
- jet propulsion
- direction device
- similar aircraft
- aircraft
- Prior art date
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
- F02K9/90—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using deflectors
-
- 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
- F42B10/665—Steering by varying intensity or direction of thrust characterised by using a nozzle provided with at least a deflector mounted within the nozzle
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Nozzles (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE3003231A DE3003231C2 (en) | 1980-01-30 | 1980-01-30 | Control device for missiles, rockets or the like driven by beam reaction. |
Publications (2)
Publication Number | Publication Date |
---|---|
IT8068752A0 IT8068752A0 (en) | 1980-11-14 |
IT1167303B true IT1167303B (en) | 1987-05-13 |
Family
ID=6093235
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT68752/80A IT1167303B (en) | 1980-01-30 | 1980-11-14 | DIRECTION DEVICE FOR ROCKET AND SIMILAR AIRCRAFT WITH JET PROPULSION |
Country Status (5)
Country | Link |
---|---|
DE (1) | DE3003231C2 (en) |
FR (1) | FR2474439A1 (en) |
GB (1) | GB2068311B (en) |
IT (1) | IT1167303B (en) |
SE (1) | SE8100747L (en) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2251834B (en) * | 1983-02-22 | 1992-12-16 | George Alexander Tarrant | Guided missiles |
GB2148875B (en) * | 1983-10-24 | 1987-01-28 | Standard Telephones Cables Ltd | Optical fibre preform manufacture |
DE102008022289B4 (en) * | 2008-04-25 | 2010-07-29 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | missile |
JP5123964B2 (en) | 2010-02-26 | 2013-01-23 | 三菱重工業株式会社 | Aircraft control system, aircraft control method, and aircraft |
GB201312593D0 (en) * | 2013-07-13 | 2013-08-28 | Mbda Uk Ltd | A thrust flow powered vehicle |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB875205A (en) * | 1958-12-31 | 1961-08-16 | Ici Ltd | Improvements relating to rocket propulsion |
US3057581A (en) * | 1959-06-25 | 1962-10-09 | United Aircraft Corp | Rocket vectoring arrangement |
US3070330A (en) * | 1961-03-20 | 1962-12-25 | William J D Escher | Attitude and propellant flow control system and method |
US3127740A (en) * | 1962-10-17 | 1964-04-07 | United Aircraft Corp | Clustered rocket nozzles |
US4254620A (en) * | 1978-02-27 | 1981-03-10 | The Boeing Company | Jet engine multiduct noise suppressor |
-
1980
- 1980-01-30 DE DE3003231A patent/DE3003231C2/en not_active Expired
- 1980-11-14 IT IT68752/80A patent/IT1167303B/en active
- 1980-12-17 FR FR8027164A patent/FR2474439A1/en active Pending
- 1980-12-22 GB GB8041067A patent/GB2068311B/en not_active Expired
-
1981
- 1981-01-30 SE SE8100747A patent/SE8100747L/en not_active Application Discontinuation
Also Published As
Publication number | Publication date |
---|---|
DE3003231C2 (en) | 1984-01-05 |
SE8100747L (en) | 1981-07-31 |
GB2068311B (en) | 1984-02-15 |
IT8068752A0 (en) | 1980-11-14 |
FR2474439A1 (en) | 1981-07-31 |
GB2068311A (en) | 1981-08-12 |
DE3003231A1 (en) | 1981-08-06 |
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