FR1217708A - Dispositif de gouvernes par tuyères orientables pour engins - Google Patents
Dispositif de gouvernes par tuyères orientables pour enginsInfo
- Publication number
- FR1217708A FR1217708A FR779425A FR779425A FR1217708A FR 1217708 A FR1217708 A FR 1217708A FR 779425 A FR779425 A FR 779425A FR 779425 A FR779425 A FR 779425A FR 1217708 A FR1217708 A FR 1217708A
- Authority
- FR
- France
- Prior art keywords
- machines
- control device
- orientable nozzles
- orientable
- nozzles
- 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.)
- Expired
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
-
- 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
- F02K9/88—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using auxiliary rocket nozzles
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)
- Aviation & Aerospace Engineering (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR779425A FR1217708A (fr) | 1958-11-18 | 1958-11-18 | Dispositif de gouvernes par tuyères orientables pour engins |
DEN16323A DE1087909B (de) | 1958-11-18 | 1959-02-26 | Ruderanlage fuer Flugkoerper mit einer Brennkammer fuer einen festen Treibsatz |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR779425A FR1217708A (fr) | 1958-11-18 | 1958-11-18 | Dispositif de gouvernes par tuyères orientables pour engins |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1217708A true FR1217708A (fr) | 1960-05-05 |
Family
ID=8708394
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR779425A Expired FR1217708A (fr) | 1958-11-18 | 1958-11-18 | Dispositif de gouvernes par tuyères orientables pour engins |
Country Status (2)
Country | Link |
---|---|
DE (1) | DE1087909B (fr) |
FR (1) | FR1217708A (fr) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2612289A1 (fr) * | 1987-03-14 | 1988-09-16 | Messerschmitt Boelkow Blohm | Dispositif pour piloter un engin volant |
WO2004044519A1 (fr) * | 2002-11-07 | 2004-05-27 | Raytheon Company | Procede et systeme de commande de missile |
US7287725B2 (en) | 2005-04-25 | 2007-10-30 | Raytheon Company | Missile control system and method |
US7856806B1 (en) | 2006-11-06 | 2010-12-28 | Raytheon Company | Propulsion system with canted multinozzle grid |
US8117847B2 (en) | 2008-03-07 | 2012-02-21 | Raytheon Company | Hybrid missile propulsion system with reconfigurable multinozzle grid |
FR3072732A1 (fr) * | 2017-10-24 | 2019-04-26 | Centre National D'etudes Spatiales | Tuyere rotative, systeme de propulsion comprenant une telle tuyere et lanceur spatial comprenant un tel systeme de propulsion |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3143354A (en) * | 1961-05-16 | 1964-08-04 | United Aircraft Corp | Seal for swivelled nozzle |
US3139725A (en) * | 1961-10-31 | 1964-07-07 | James E Webb | Steerable solid propellant rocket motor |
US3266244A (en) * | 1963-01-28 | 1966-08-16 | William A Schulze | Liquid-fueled rocket roll control device |
RU2514327C1 (ru) * | 2012-12-26 | 2014-04-27 | Открытое акционерное общество "Машиностроительное конструкторское бюро "Искра" имени Ивана Ивановича Картукова" | Управляющий ракетный двигатель |
WO2021094710A1 (fr) * | 2019-11-11 | 2021-05-20 | Mbda Uk Limited | Ensemble buses d'éjection et procédé de commande d'un véhicule aérien |
EP3819491A1 (fr) * | 2019-11-11 | 2021-05-12 | MBDA UK Limited | Ensemble de buse d'échappement et procédé de reglage d'un véhicule aeronautique |
-
1958
- 1958-11-18 FR FR779425A patent/FR1217708A/fr not_active Expired
-
1959
- 1959-02-26 DE DEN16323A patent/DE1087909B/de active Pending
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2612289A1 (fr) * | 1987-03-14 | 1988-09-16 | Messerschmitt Boelkow Blohm | Dispositif pour piloter un engin volant |
WO2004044519A1 (fr) * | 2002-11-07 | 2004-05-27 | Raytheon Company | Procede et systeme de commande de missile |
US7108223B2 (en) | 2002-11-07 | 2006-09-19 | Raytheon Company | Missile control system and method |
US7287725B2 (en) | 2005-04-25 | 2007-10-30 | Raytheon Company | Missile control system and method |
US7856806B1 (en) | 2006-11-06 | 2010-12-28 | Raytheon Company | Propulsion system with canted multinozzle grid |
US8117847B2 (en) | 2008-03-07 | 2012-02-21 | Raytheon Company | Hybrid missile propulsion system with reconfigurable multinozzle grid |
FR3072732A1 (fr) * | 2017-10-24 | 2019-04-26 | Centre National D'etudes Spatiales | Tuyere rotative, systeme de propulsion comprenant une telle tuyere et lanceur spatial comprenant un tel systeme de propulsion |
Also Published As
Publication number | Publication date |
---|---|
DE1087909B (de) | 1960-08-25 |
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