GB1320766A - Rocket propulsion system - Google Patents
Rocket propulsion systemInfo
- Publication number
- GB1320766A GB1320766A GB4755570A GB4755570A GB1320766A GB 1320766 A GB1320766 A GB 1320766A GB 4755570 A GB4755570 A GB 4755570A GB 4755570 A GB4755570 A GB 4755570A GB 1320766 A GB1320766 A GB 1320766A
- Authority
- GB
- United Kingdom
- Prior art keywords
- propellants
- lines
- turbines
- combustion chamber
- propellant
- 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
- 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
- F02K9/44—Feeding propellants
-
- 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
- F02K9/44—Feeding propellants
- F02K9/46—Feeding propellants using pumps
- F02K9/48—Feeding propellants using pumps driven by a gas turbine fed by propellant combustion gases or fed by vaporized propellants or other gases
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
- Supercharger (AREA)
Abstract
1320766 Rocket engines; supply of propellants MASCHINENFABRIK AUGSBURG-NURNBERG AG 6 Oct 1970 [7 Oct 1969] 47555/70 Addition to 1210601 Heading FIT The invention relates to a rocket propulsion system and is a modification or improvement in the invention of parent Specification 1210601. The system comprises a turbine connected to receive, on ignition, one of the propellants in its gaseous form before this propellant reaches the injection nozzle means, the turbine being arranged to drive a propellant supply pump. In the embodiment shown two propellant tanks 14, 19 are provided, the tanks being insulated and the propellants such as hydrogen and oxygen being stored in liquefied form. The system comprises also a combustion chamber and propulsion nozzle assembly 1, 2 there being passages 8, 9 in the walls thereof for flow of propellants for cooling purposes. At starting propellants flows through lines 69, 70 which are uninsulated so that the liquid propellants are vapourized and pass through non-return valves 61, 62 to lines 71, 72 thence through passages 9, 8, all respectively, in the walls of the combustion chamber and nozzle assembly, then passing to turbines 67, 68 to drive them. The propellants discharge from the turbines 67, 68 through lines 73, 74 and pass through valves 4, 5 and nozzles 6, 7 into the combustion chamber. The turbines 67, 68 drive propellant pumps 65, 66 which in normal operation receive liquid propellants through lines 75, 76 and valves 63, 64, the pumps discharging the propellants through lines 77, 78 into the lines 71, 72 and so to the coolant passages 9, 8, turbines 67, 68 and so into the combustion chamber.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19691950407 DE1950407B2 (en) | 1969-10-07 | 1969-10-07 | FUEL SUPPLY SYSTEM FOR A ROCKET ENGINE |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1320766A true GB1320766A (en) | 1973-06-20 |
Family
ID=5747482
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB4755570A Expired GB1320766A (en) | 1969-10-07 | 1970-10-06 | Rocket propulsion system |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE1950407B2 (en) |
FR (1) | FR2031047A6 (en) |
GB (1) | GB1320766A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103133183A (en) * | 2013-02-06 | 2013-06-05 | 北京航天试验技术研究所 | Safe processing device of low-temperature hydrogen in rocket engine thrust chamber |
US20140260181A1 (en) * | 2011-10-11 | 2014-09-18 | Snecma | Jet propulsion device and fuel supply method |
CN113404621A (en) * | 2021-06-19 | 2021-09-17 | 西北工业大学 | Solid-liquid mixed engine and method for Mars ascending aircraft |
CN113586286A (en) * | 2021-07-08 | 2021-11-02 | 北京星途探索科技有限公司 | Liquid oxygen methane propellant supply system |
CN114030656A (en) * | 2021-11-09 | 2022-02-11 | 西安交通大学 | Novel variable-thrust nuclear heat propulsion system |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2743983C2 (en) * | 1977-09-30 | 1982-11-11 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | By-pass liquid rocket engine for operation in a vacuum |
US4583362A (en) * | 1983-12-12 | 1986-04-22 | Rockwell International Corporation | Expander-cycle, turbine-drive, regenerative rocket engine |
JPS62261652A (en) * | 1986-05-07 | 1987-11-13 | Natl Space Dev Agency Japan<Nasda> | Liquid rocket engine |
-
1969
- 1969-10-07 DE DE19691950407 patent/DE1950407B2/en active Pending
- 1969-12-31 FR FR6945657A patent/FR2031047A6/fr not_active Expired
-
1970
- 1970-10-06 GB GB4755570A patent/GB1320766A/en not_active Expired
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20140260181A1 (en) * | 2011-10-11 | 2014-09-18 | Snecma | Jet propulsion device and fuel supply method |
US9771897B2 (en) * | 2011-10-11 | 2017-09-26 | Snecma | Jet propulsion device and fuel supply method |
CN103133183A (en) * | 2013-02-06 | 2013-06-05 | 北京航天试验技术研究所 | Safe processing device of low-temperature hydrogen in rocket engine thrust chamber |
CN103133183B (en) * | 2013-02-06 | 2015-11-04 | 北京航天试验技术研究所 | A kind of thrust chamber low temperature hydrogen secure processing device |
CN113404621A (en) * | 2021-06-19 | 2021-09-17 | 西北工业大学 | Solid-liquid mixed engine and method for Mars ascending aircraft |
CN113404621B (en) * | 2021-06-19 | 2022-08-16 | 西北工业大学 | Solid-liquid mixed engine and method for Mars ascending aircraft |
CN113586286A (en) * | 2021-07-08 | 2021-11-02 | 北京星途探索科技有限公司 | Liquid oxygen methane propellant supply system |
CN114030656A (en) * | 2021-11-09 | 2022-02-11 | 西安交通大学 | Novel variable-thrust nuclear heat propulsion system |
Also Published As
Publication number | Publication date |
---|---|
DE1950407A1 (en) | 1971-04-22 |
FR2031047A6 (en) | 1970-11-13 |
DE1950407B2 (en) | 1972-03-30 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PLNP | Patent lapsed through nonpayment of renewal fees |