FR2307138B3 - - Google Patents
Info
- Publication number
- FR2307138B3 FR2307138B3 FR7610276A FR7610276A FR2307138B3 FR 2307138 B3 FR2307138 B3 FR 2307138B3 FR 7610276 A FR7610276 A FR 7610276A FR 7610276 A FR7610276 A FR 7610276A FR 2307138 B3 FR2307138 B3 FR 2307138B3
- Authority
- FR
- France
- 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
- 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
- F02K9/86—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using nozzle throats of adjustable cross- section
-
- 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
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/60—Constructional parts; Details not otherwise provided for
- F02K9/62—Combustion or thrust chambers
- F02K9/64—Combustion or thrust chambers having cooling arrangements
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Nozzles (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
- Fuel-Injection Apparatus (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE2515845A DE2515845C3 (de) | 1975-04-11 | 1975-04-11 | Flüssigkeitsraketentriebwerk regelbaren Schubs |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2307138A1 FR2307138A1 (fr) | 1976-11-05 |
| FR2307138B3 true FR2307138B3 (US20020051482A1-20020502-M00012.png) | 1979-01-05 |
Family
ID=5943606
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR7610276A Granted FR2307138A1 (fr) | 1975-04-11 | 1976-04-08 | Moteur-fusee a propergol liquide |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US4109460A (US20020051482A1-20020502-M00012.png) |
| DE (1) | DE2515845C3 (US20020051482A1-20020502-M00012.png) |
| FR (1) | FR2307138A1 (US20020051482A1-20020502-M00012.png) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6579085B1 (en) | 2000-05-05 | 2003-06-17 | The Boc Group, Inc. | Burner and combustion method for the production of flame jet sheets in industrial furnaces |
| WO2002029233A1 (fr) * | 2000-10-05 | 2002-04-11 | Federal State Unitary Enterprise Chemical Automatic Design Bureau (Cadb) | Chambre annulaire de moteur-fusee a propergol liquide |
| DE102017102160A1 (de) * | 2016-02-05 | 2017-08-10 | Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh | Vorrichtung und System zur Steuerung von Flugkörpern und Kill-Vehicles, die mit gelförmigen Treibstoffen betrieben wird |
| US11220979B1 (en) * | 2020-11-10 | 2022-01-11 | Mountain Aerospace Research Solutions, Inc. | Liquid-cooled air-breathing rocket engine |
| CN116252970B (zh) * | 2022-09-07 | 2023-08-29 | 中国科学院空间应用工程与技术中心 | 用于微小卫星的变推力气体推力器、气体供应系统及方法 |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2570629A (en) * | 1945-10-05 | 1951-10-09 | Anxionnaz | Adjustable pipe for the intake of air and expansion of the driving gases in reactionjet propellers for projectiles and vehicles |
| US2637973A (en) * | 1949-04-01 | 1953-05-12 | Reaction Motors Inc | Rocket engine having turbine located in nozzle for driving auxiliaries |
| DE1191178B (de) * | 1959-06-11 | 1965-04-15 | Bendix Corp | Strahltriebwerk |
| US3377803A (en) * | 1960-08-10 | 1968-04-16 | Gen Motors Corp | Jet engine cooling system |
| US3286469A (en) * | 1961-07-07 | 1966-11-22 | United Aircraft Corp | Rocket nozzle cooling and thrust recovery device |
| US3871173A (en) * | 1970-03-24 | 1975-03-18 | Us Navy | Constant chamber pressure throttling injector |
-
1975
- 1975-04-11 DE DE2515845A patent/DE2515845C3/de not_active Expired
-
1976
- 1976-04-06 US US05/674,089 patent/US4109460A/en not_active Expired - Lifetime
- 1976-04-08 FR FR7610276A patent/FR2307138A1/fr active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| FR2307138A1 (fr) | 1976-11-05 |
| DE2515845C3 (de) | 1981-10-15 |
| US4109460A (en) | 1978-08-29 |
| DE2515845A1 (de) | 1976-10-21 |
| DE2515845B2 (de) | 1981-02-19 |
