FR2453279A1 - Statoreacteur pour missiles teleguides - Google Patents
Statoreacteur pour missiles teleguidesInfo
- Publication number
- FR2453279A1 FR2453279A1 FR8006536A FR8006536A FR2453279A1 FR 2453279 A1 FR2453279 A1 FR 2453279A1 FR 8006536 A FR8006536 A FR 8006536A FR 8006536 A FR8006536 A FR 8006536A FR 2453279 A1 FR2453279 A1 FR 2453279A1
- Authority
- FR
- France
- Prior art keywords
- statoreactor
- missiles
- nozzle
- control
- thrust
- 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- Withdrawn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
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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Spray Control Apparatus (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Testing Of Engines (AREA)
Abstract
Statoréacteur pour missiles téléguidés. Statoréacteur pour missiles téleguidés avec déflexion du jet de poussée en particulier supersonique, dans lequel la tuyère de poussée comporte, raccordé à son extrémité sortie, un prolongement élargi au-delà du rapport d'expansion correspondant à la pression environnante et dans lequel, pour la déviation du jet, des impulsions de commande agissant à chaque fois dans le sens de la déflexion voulue sont délivrées au niveau des ouvertures de commande réparties dans le sens périphérique de la tuyère. Les ouvertures de commande 24B, 28A débouchant dans une zone marginale de l'extrémité sortie 10 de la tuyère sont raccordées à un système d'injection 14 les alimentant en gaz comprimé ou en fluide faisant office de fluide de commande.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19792913350 DE2913350A1 (de) | 1979-04-03 | 1979-04-03 | Strahltriebwerk fuer lenkflugkoerper |
Publications (1)
Publication Number | Publication Date |
---|---|
FR2453279A1 true FR2453279A1 (fr) | 1980-10-31 |
Family
ID=6067301
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8006536A Withdrawn FR2453279A1 (fr) | 1979-04-03 | 1980-03-24 | Statoreacteur pour missiles teleguides |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE2913350A1 (fr) |
FR (1) | FR2453279A1 (fr) |
GB (1) | GB2045704A (fr) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1997014873A1 (fr) * | 1995-10-16 | 1997-04-24 | Valentin Semenovich Gorelykh | Procede de conversion d'energie et dispositif de mise en oeuvre |
IL116668A (en) * | 1996-01-03 | 1998-12-06 | Univ Ramot | Apparatus and method for controlling the motion of a solid body or fluid stream |
CN111350615B (zh) * | 2020-03-27 | 2023-09-05 | 惠州学院 | 一种适用于垂直发射飞行器的整体式转弯装置 |
Citations (5)
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 |
GB947751A (en) * | 1961-02-28 | 1964-01-29 | United Aircraft Corp | Improvements relating to navigation control for a propulsive vehicle |
US3166897A (en) * | 1961-08-21 | 1965-01-26 | United Aircraft Corp | Roll control and thrust vector control |
US3221498A (en) * | 1962-08-06 | 1965-12-07 | Lester T Bankston | Secondary fluid injection thrust vectoring methods and apparatus |
US3266732A (en) * | 1963-09-03 | 1966-08-16 | United Aircraft Corp | Roll control system |
-
1979
- 1979-04-03 DE DE19792913350 patent/DE2913350A1/de not_active Withdrawn
-
1980
- 1980-03-21 GB GB8009543A patent/GB2045704A/en not_active Withdrawn
- 1980-03-24 FR FR8006536A patent/FR2453279A1/fr not_active Withdrawn
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB947751A (en) * | 1961-02-28 | 1964-01-29 | United Aircraft Corp | Improvements relating to navigation control for a propulsive vehicle |
US3166897A (en) * | 1961-08-21 | 1965-01-26 | United Aircraft Corp | Roll control and thrust vector control |
FR1316191A (fr) * | 1962-02-26 | 1963-01-25 | United Aircraft Corp | Dispositif de commande pour appareil propulseur |
US3221498A (en) * | 1962-08-06 | 1965-12-07 | Lester T Bankston | Secondary fluid injection thrust vectoring methods and apparatus |
US3266732A (en) * | 1963-09-03 | 1966-08-16 | United Aircraft Corp | Roll control system |
Non-Patent Citations (1)
Title |
---|
EXBK/73 * |
Also Published As
Publication number | Publication date |
---|---|
GB2045704A (en) | 1980-11-05 |
DE2913350A1 (de) | 1980-10-16 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |