DE1132029B - Steuervorrichtung fuer Raketen - Google Patents
Steuervorrichtung fuer RaketenInfo
- Publication number
- DE1132029B DE1132029B DEI17424A DEI0017424A DE1132029B DE 1132029 B DE1132029 B DE 1132029B DE I17424 A DEI17424 A DE I17424A DE I0017424 A DEI0017424 A DE I0017424A DE 1132029 B DE1132029 B DE 1132029B
- Authority
- DE
- Germany
- Prior art keywords
- nozzle
- nozzles
- rocket
- missile
- axis
- 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.)
- Granted
Links
Classifications
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/38—Jet flaps
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Casting Support Devices, Ladles, And Melt Control Thereby (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Processing And Handling Of Plastics And Other Materials For Molding In General (AREA)
- Transmission Devices (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB42271/58A GB875205A (en) | 1958-12-31 | 1958-12-31 | Improvements relating to rocket propulsion |
Publications (2)
Publication Number | Publication Date |
---|---|
DE1132029B true DE1132029B (de) | 1962-06-20 |
DE1132029C2 DE1132029C2 (es) | 1962-12-27 |
Family
ID=10423674
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DEI17424A Granted DE1132029B (de) | 1958-12-31 | 1959-12-21 | Steuervorrichtung fuer Raketen |
Country Status (3)
Country | Link |
---|---|
BE (1) | BE602973A (es) |
DE (1) | DE1132029B (es) |
GB (1) | GB875205A (es) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1332562A (fr) * | 1962-03-20 | 1963-07-19 | Snecma | Dispositif de tourillonnement et d'étanchéité pour tuyère, applicable notamment aux fusées |
US3235184A (en) * | 1963-03-20 | 1966-02-15 | Curtiss Wright Corp | Vectoring nozzle |
US3362646A (en) * | 1965-08-23 | 1968-01-09 | Thiokol Chemical Corp | Variable direction thrust nozzle |
US4432512A (en) * | 1978-08-31 | 1984-02-21 | British Aerospace Public Limited Company | Jet propulsion efflux outlets |
DE3003231C2 (de) * | 1980-01-30 | 1984-01-05 | Dornier Gmbh, 7990 Friedrichshafen | Steuereinrichtung für durch Strahlreaktion angetriebene Flugkörper, Raketen o.dgl. |
EP3330189B1 (en) | 2016-12-05 | 2019-06-19 | Airbus Defence and Space GmbH | Pointing mechanism for use in an electric propulsion system of a spacecraft |
CN115898701A (zh) * | 2022-10-28 | 2023-04-04 | 西安航天发动机有限公司 | 一种用于推力室头部的组合自紧式密封结构 |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH196692A (fr) * | 1936-12-31 | 1938-03-31 | Sageb Societe Anonyme De Gesti | Projectile comportant une fusée à réaction. |
US2611317A (en) * | 1946-03-08 | 1952-09-23 | Africano Alfred | Rotating nozzle for rockets |
US2849955A (en) * | 1955-06-30 | 1958-09-02 | Spurgeon E Smathers | Rocket construction |
-
1958
- 1958-12-31 GB GB42271/58A patent/GB875205A/en not_active Expired
-
1959
- 1959-12-21 DE DEI17424A patent/DE1132029B/de active Granted
-
1961
- 1961-04-24 BE BE602973A patent/BE602973A/fr unknown
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH196692A (fr) * | 1936-12-31 | 1938-03-31 | Sageb Societe Anonyme De Gesti | Projectile comportant une fusée à réaction. |
US2611317A (en) * | 1946-03-08 | 1952-09-23 | Africano Alfred | Rotating nozzle for rockets |
US2849955A (en) * | 1955-06-30 | 1958-09-02 | Spurgeon E Smathers | Rocket construction |
Also Published As
Publication number | Publication date |
---|---|
GB875205A (en) | 1961-08-16 |
BE602973A (fr) | 1961-10-24 |
DE1132029C2 (es) | 1962-12-27 |
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