BE562285A - - Google Patents
Info
- Publication number
- BE562285A BE562285A BE562285DA BE562285A BE 562285 A BE562285 A BE 562285A BE 562285D A BE562285D A BE 562285DA BE 562285 A BE562285 A BE 562285A
- Authority
- BE
- Belgium
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
- F02K9/42—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
-
- 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
- F02K9/68—Decomposition chambers
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Hydrogen, Water And Hydrids (AREA)
- Gas Burners (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB3426856A GB847084A (en) | 1956-11-09 | 1956-11-09 | Combustion chamber for a gas turbine or rocket motor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE562285A true BE562285A (xx) |
Family
ID=10363522
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE562285D BE562285A (xx) | 1956-11-09 |
Country Status (4)
| Country | Link |
|---|---|
| BE (1) | BE562285A (xx) |
| DE (1) | DE1071421B (xx) |
| FR (1) | FR1187946A (xx) |
| GB (1) | GB847084A (xx) |
Families Citing this family (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1164753B (de) * | 1959-12-12 | 1964-03-05 | Boelkow Entwicklungen Kg | Raketentriebwerk fuer fluessige Treibstoffe |
| DE1142253B (de) * | 1960-01-29 | 1963-01-10 | Boelkow Entwicklungen Kg | Brennkammer fuer Fluessigtreibstoffe |
| GB1196489A (en) * | 1966-11-29 | 1970-06-24 | Lutz Tilo Kayser | Improvements in or relating to Rocket Engines |
| DE1297942B (de) * | 1966-11-29 | 1969-06-19 | Kayser Lutz T | Anordnung zur Raketentriebwerkskuehlung |
| US3451223A (en) * | 1966-12-06 | 1969-06-24 | Howard Vern Main | Rocket engine chamber cooling and injection system |
| DE2519538C2 (de) * | 1975-05-02 | 1982-12-30 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Verbindung zwischen dem Kühlmittel-Zulaufring und der Brennkammer-oder Schubdüsenwand eines Raketentriebwerks |
| FR2503794B1 (fr) * | 1981-04-13 | 1986-04-25 | Europ Propulsion | Chambre de combustion de propulseur-fusee a divergent multiple |
| US4817890A (en) * | 1986-10-14 | 1989-04-04 | General Electric Company | Multiple-propellant air vehicle and propulsion system |
| US4840025A (en) * | 1986-10-14 | 1989-06-20 | General Electric Company | Multiple-propellant air vehicle and propulsion system |
| US4811556A (en) * | 1986-10-14 | 1989-03-14 | General Electric Company | Multiple-propellant air vehicle and propulsion system |
| US4835959A (en) * | 1986-10-14 | 1989-06-06 | General Electric Company | Multiple-propellant air vehicle and propulsion system |
| US4841723A (en) * | 1986-10-14 | 1989-06-27 | General Electric Company | Multiple-propellant air vehicle and propulsion system |
| DE3728706A1 (de) * | 1987-08-28 | 1988-10-27 | Kurt Mannl | Rotierendes einspritzsystem fuer raketentriebwerke |
| US4882904A (en) * | 1988-03-24 | 1989-11-28 | Aerojet-General Corporation | Two stage rocket combustor |
| DE102016208731A1 (de) * | 2016-05-20 | 2017-11-23 | Airbus Ds Gmbh | Raketenantriebssystem und Verfahren zum Betreiben eines Raketenantriebssystems |
| CN111456866A (zh) * | 2020-04-14 | 2020-07-28 | 合肥中科重明科技有限公司 | 一种液体火箭发动机的冷却液膜成型结构 |
| CN112177801B (zh) * | 2020-08-31 | 2021-12-24 | 西北工业大学 | 一种基于第三流体的过氧化氢/煤油火箭发动机推力室 |
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0
- DE DENDAT1071421D patent/DE1071421B/de active Pending
- BE BE562285D patent/BE562285A/xx unknown
-
1956
- 1956-11-09 GB GB3426856A patent/GB847084A/en not_active Expired
-
1957
- 1957-11-08 FR FR1187946D patent/FR1187946A/fr not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| FR1187946A (fr) | 1959-09-17 |
| GB847084A (en) | 1960-09-07 |
| DE1071421B (de) | 1959-12-17 |