GB1220223A - A liquid cooled rocket combustion chamber with thrust nozzle - Google Patents
A liquid cooled rocket combustion chamber with thrust nozzleInfo
- Publication number
- GB1220223A GB1220223A GB55363/67A GB5536367A GB1220223A GB 1220223 A GB1220223 A GB 1220223A GB 55363/67 A GB55363/67 A GB 55363/67A GB 5536367 A GB5536367 A GB 5536367A GB 1220223 A GB1220223 A GB 1220223A
- Authority
- GB
- United Kingdom
- Prior art keywords
- cooling
- conduit
- insert
- combustion chamber
- thrust nozzle
- 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
- 238000002485 combustion reaction Methods 0.000 title abstract 3
- 239000007788 liquid Substances 0.000 title abstract 2
- 238000001816 cooling Methods 0.000 abstract 7
- 239000000463 material Substances 0.000 abstract 3
- 238000011144 upstream manufacturing Methods 0.000 abstract 3
- QGZKDVFQNNGYKY-UHFFFAOYSA-N Ammonia Chemical compound N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 abstract 2
- 239000000110 cooling liquid Substances 0.000 abstract 2
- MYMOFIZGZYHOMD-UHFFFAOYSA-N Dioxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 abstract 1
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 abstract 1
- 229910021529 ammonia Inorganic materials 0.000 abstract 1
- 239000011248 coating agent Substances 0.000 abstract 1
- 238000000576 coating method Methods 0.000 abstract 1
- 239000002826 coolant Substances 0.000 abstract 1
- 238000001704 evaporation Methods 0.000 abstract 1
- 230000008020 evaporation Effects 0.000 abstract 1
- 230000001681 protective effect Effects 0.000 abstract 1
- 230000001172 regenerating effect Effects 0.000 abstract 1
- 239000000126 substance Substances 0.000 abstract 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 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
- F02K9/97—Rocket nozzles
- F02K9/972—Fluid cooling arrangements for 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
- F02K9/42—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)
- Testing Of Engines (AREA)
- Physical Or Chemical Processes And Apparatus (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DEB0090747 | 1967-01-16 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1220223A true GB1220223A (en) | 1971-01-20 |
Family
ID=6985460
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB55363/67A Expired GB1220223A (en) | 1967-01-16 | 1967-12-05 | A liquid cooled rocket combustion chamber with thrust nozzle |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US3595023A (enExample) |
| FR (1) | FR1604143A (enExample) |
| GB (1) | GB1220223A (enExample) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4299804A (en) * | 1978-03-09 | 1981-11-10 | Agrico Chemical Company | Removal of magnesium and aluminum impurities from wet process phosphoric acid |
| US5016436A (en) * | 1987-10-20 | 1991-05-21 | Rolls-Royce Plc | Interturbine duct |
| CN113006970A (zh) * | 2021-02-26 | 2021-06-22 | 陕西蓝箭航天技术有限公司 | 液体火箭发动机旋流液膜冷却结构及火箭发动机 |
| US11629669B1 (en) * | 2019-05-31 | 2023-04-18 | Exquadrum, Inc. | Liquid monopropellant controlled solid rocket motor with aft end injection deflector |
Families Citing this family (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2137109C3 (de) * | 1971-07-24 | 1980-04-30 | Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen | Herstellung einer regenerativ gekühlten Raketenbrennkammer |
| DE2356572C3 (de) * | 1973-11-13 | 1979-03-29 | Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen | Flüssigkeitsgekühlte Raketenbrennkammer mit Schubdüse |
| US4353679A (en) * | 1976-07-29 | 1982-10-12 | General Electric Company | Fluid-cooled element |
| US4643356A (en) * | 1977-08-31 | 1987-02-17 | United Technologies Corporation | Cooling liner for convergent-divergent exhaust nozzle |
| US5255849A (en) * | 1991-11-05 | 1993-10-26 | General Electric Company | Cooling air transfer apparatus for aircraft gas turbine engine exhaust nozzles |
| US5269132A (en) * | 1992-10-29 | 1993-12-14 | E-Systems, Inc. | Method and apparatus for controlling infrared emissions |
| US6003301A (en) * | 1993-04-14 | 1999-12-21 | Adroit Systems, Inc. | Exhaust nozzle for multi-tube detonative engines |
| RU2158841C2 (ru) * | 1999-01-21 | 2000-11-10 | Открытое акционерное общество "НПО Энергомаш им. акад. В.П. Глушко" | Камера жидкостного ракетного двигателя и ее корпус |
| US7213392B2 (en) * | 2003-06-10 | 2007-05-08 | United Technologies Corporation | Rocket engine combustion chamber |
| RU2511942C1 (ru) * | 2013-03-18 | 2014-04-10 | Николай Борисович Болотин | Система охлаждения камеры жидкостного ракетного двигателя |
| CN112746912B (zh) * | 2021-01-18 | 2022-05-13 | 天津大学 | 可液气分离的液体火箭发动机多层主动冷却装置 |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2183313A (en) * | 1938-07-07 | 1939-12-12 | Robert H Goddard | Combustion chamber for aircraft |
| US2551112A (en) * | 1946-09-05 | 1951-05-01 | Daniel And Florence Guggenheim | Premixing combustion chamber |
| US2487435A (en) * | 1948-02-07 | 1949-11-08 | Esther C Goodard | Fuel and water feeding and steam discharge arrangement for combustion chambers |
| GB759901A (en) * | 1951-12-06 | 1956-10-24 | Armstrong Siddeley Motors Ltd | Combustion chambers |
| US3157026A (en) * | 1962-10-19 | 1964-11-17 | Super Temp Corp | Composite nozzle structure |
| US3304008A (en) * | 1963-06-24 | 1967-02-14 | Gen Motors Corp | Temperature responsive rocket nozzle cooling system |
| US3313488A (en) * | 1964-10-02 | 1967-04-11 | Thiokol Chemical Corp | Rocket thrust chamber |
-
1967
- 1967-12-05 GB GB55363/67A patent/GB1220223A/en not_active Expired
-
1968
- 1968-01-11 US US698377A patent/US3595023A/en not_active Expired - Lifetime
- 1968-01-15 FR FR1604143D patent/FR1604143A/fr not_active Expired
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4299804A (en) * | 1978-03-09 | 1981-11-10 | Agrico Chemical Company | Removal of magnesium and aluminum impurities from wet process phosphoric acid |
| US5016436A (en) * | 1987-10-20 | 1991-05-21 | Rolls-Royce Plc | Interturbine duct |
| US11629669B1 (en) * | 2019-05-31 | 2023-04-18 | Exquadrum, Inc. | Liquid monopropellant controlled solid rocket motor with aft end injection deflector |
| CN113006970A (zh) * | 2021-02-26 | 2021-06-22 | 陕西蓝箭航天技术有限公司 | 液体火箭发动机旋流液膜冷却结构及火箭发动机 |
| CN113006970B (zh) * | 2021-02-26 | 2022-05-27 | 陕西蓝箭航天技术有限公司 | 液体火箭发动机旋流液膜冷却结构及火箭发动机 |
Also Published As
| Publication number | Publication date |
|---|---|
| FR1604143A (enExample) | 1971-07-12 |
| US3595023A (en) | 1971-07-27 |
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