FR2405456A1 - Missile teleguide avec dispositif pour engendrer un moment de tangage, de lacet et de roulis - Google Patents
Missile teleguide avec dispositif pour engendrer un moment de tangage, de lacet et de roulisInfo
- Publication number
- FR2405456A1 FR2405456A1 FR7828241A FR7828241A FR2405456A1 FR 2405456 A1 FR2405456 A1 FR 2405456A1 FR 7828241 A FR7828241 A FR 7828241A FR 7828241 A FR7828241 A FR 7828241A FR 2405456 A1 FR2405456 A1 FR 2405456A1
- Authority
- FR
- France
- Prior art keywords
- moment
- thrust
- nozzle
- missile
- roll
- 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.)
- Withdrawn
Links
- 239000012530 fluid Substances 0.000 abstract 2
- 238000002485 combustion reaction Methods 0.000 abstract 1
- 230000006835 compression Effects 0.000 abstract 1
- 238000007906 compression Methods 0.000 abstract 1
- 238000004519 manufacturing process Methods 0.000 abstract 1
- 238000005096 rolling process Methods 0.000 abstract 1
- 239000004449 solid propellant Substances 0.000 abstract 1
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
- F02K9/82—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control by injection of a secondary fluid into the rocket exhaust gases
-
- 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)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Nozzles (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Storing, Repeated Paying-Out, And Re-Storing Of Elongated Articles (AREA)
Abstract
Missile téléguidé comportant un statoréacteur, en particulier à propergol solide, constitué d'une partie chambre de combustion et d'une partie tuyère de poussée, et une commande du vecteur 5 de poussée agissant sur le jet et destinée à engendrer un moment de tangage, de lacet et de roulis. Le dispositif de commande du vecteur de poussée comporte, pour la commande du moment de tangage et de lacet, un mécanisme d'actionnement 22 réglant angulairement, par rapport à l'axe longitudinal A-A du missile 2, la partie de tuyère de poussé 10 réalisée sous la forme d'une tuyère pivotante 12, en combinaison avec un dispositif de commande à fluide, associé à la tuyère pivotante 12 et injectant dans le jet de poussée une quantité de fluide dosée avec production d'une impulsion de compression soumettant la tuyere 12 à un moment de roulis.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19772744897 DE2744897A1 (de) | 1977-10-06 | 1977-10-06 | Lenkflugkoerper |
Publications (1)
Publication Number | Publication Date |
---|---|
FR2405456A1 true FR2405456A1 (fr) | 1979-05-04 |
Family
ID=6020761
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7828241A Withdrawn FR2405456A1 (fr) | 1977-10-06 | 1978-10-03 | Missile teleguide avec dispositif pour engendrer un moment de tangage, de lacet et de roulis |
Country Status (4)
Country | Link |
---|---|
DE (1) | DE2744897A1 (fr) |
FR (1) | FR2405456A1 (fr) |
GB (1) | GB2005606B (fr) |
IT (1) | IT1099232B (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112572840A (zh) * | 2020-12-14 | 2021-03-30 | 兰州空间技术物理研究所 | 一种电推进***贮供单元及其制造方法 |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9291410B2 (en) | 2010-07-22 | 2016-03-22 | Saab Ab | Cooling device for cooling combustion gases from recoilless anti-tank weapons |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1316191A (fr) * | 1962-02-26 | 1963-01-25 | United Aircraft Corp | Dispositif de commande pour appareil propulseur |
US3147590A (en) * | 1961-03-16 | 1964-09-08 | Thompson Ramo Wooldridge Inc | Reaction motor with nozzle vector control having ablative port means and cooled valve means |
US3266732A (en) * | 1963-09-03 | 1966-08-16 | United Aircraft Corp | Roll control system |
US3270505A (en) * | 1964-10-21 | 1966-09-06 | Norman L Crabill | Control system for rocket vehicles |
GB1134835A (en) * | 1965-12-06 | 1968-11-27 | Us Navy | Liquid injection thrust vectoring |
US4063685A (en) * | 1976-07-30 | 1977-12-20 | The United States Of America As Represented By The Secretary Of The Army | Thrust vector control by circulation control over aerodynamic surfaces in a supersonic nozzle |
-
1977
- 1977-10-06 DE DE19772744897 patent/DE2744897A1/de not_active Withdrawn
-
1978
- 1978-10-03 FR FR7828241A patent/FR2405456A1/fr not_active Withdrawn
- 1978-10-04 GB GB7839345A patent/GB2005606B/en not_active Expired
- 1978-10-04 IT IT28403/78A patent/IT1099232B/it active
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3147590A (en) * | 1961-03-16 | 1964-09-08 | Thompson Ramo Wooldridge Inc | Reaction motor with nozzle vector control having ablative port means and cooled valve means |
FR1316191A (fr) * | 1962-02-26 | 1963-01-25 | United Aircraft Corp | Dispositif de commande pour appareil propulseur |
US3266732A (en) * | 1963-09-03 | 1966-08-16 | United Aircraft Corp | Roll control system |
US3270505A (en) * | 1964-10-21 | 1966-09-06 | Norman L Crabill | Control system for rocket vehicles |
GB1134835A (en) * | 1965-12-06 | 1968-11-27 | Us Navy | Liquid injection thrust vectoring |
US4063685A (en) * | 1976-07-30 | 1977-12-20 | The United States Of America As Represented By The Secretary Of The Army | Thrust vector control by circulation control over aerodynamic surfaces in a supersonic nozzle |
Non-Patent Citations (1)
Title |
---|
EXBK/73 * |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112572840A (zh) * | 2020-12-14 | 2021-03-30 | 兰州空间技术物理研究所 | 一种电推进***贮供单元及其制造方法 |
Also Published As
Publication number | Publication date |
---|---|
IT1099232B (it) | 1985-09-18 |
GB2005606B (en) | 1982-06-30 |
DE2744897A1 (de) | 1979-04-19 |
IT7828403A0 (it) | 1978-10-04 |
GB2005606A (en) | 1979-04-25 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |