GB902056A - Purge system for rocket propellant system - Google Patents
Purge system for rocket propellant systemInfo
- Publication number
- GB902056A GB902056A GB4041060A GB4041060A GB902056A GB 902056 A GB902056 A GB 902056A GB 4041060 A GB4041060 A GB 4041060A GB 4041060 A GB4041060 A GB 4041060A GB 902056 A GB902056 A GB 902056A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shut
- combustion chamber
- engine
- purging
- valves
- 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
- 239000003380 propellant Substances 0.000 title abstract 4
- 238000010926 purge Methods 0.000 title abstract 3
- 238000002485 combustion reaction Methods 0.000 abstract 3
- 230000009977 dual effect Effects 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
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/44—Feeding propellants
- F02K9/54—Leakage detectors; Purging systems; Filtration systems
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Valve Device For Special Equipments (AREA)
Abstract
902,056. Fluid-pressure servomotor-control systems. UNITED AIRCRAFT CORPORATION. Nov. 24, 1960, No. 40410/60. Drawings to Specification. Class 135. [Also in Group XXVI] A dual propellant rocket engine system comprises a tank and supply conduit for each propellant, a combustion chamber to which the propellants flow, a shut-off valve in each conduit, means for purging the conduits downstream of the shut-off valves and the combustion chamber responsive to the starting of the engine, and means for purging the conduits downstream of the shut-off valves and the combustion chamber responsive to the stopping of the engine. The subject-matter of this Specification is identical with that described in Specification 902,055. Specification 902,054 also is referred to.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB4041060A GB902056A (en) | 1960-11-24 | 1960-11-24 | Purge system for rocket propellant system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB4041060A GB902056A (en) | 1960-11-24 | 1960-11-24 | Purge system for rocket propellant system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB902056A true GB902056A (en) | 1962-07-25 |
Family
ID=10414763
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB4041060A Expired GB902056A (en) | 1960-11-24 | 1960-11-24 | Purge system for rocket propellant system |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB902056A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114251192A (en) * | 2021-11-05 | 2022-03-29 | 航天科工火箭技术有限公司 | Liquid oxygen methane rocket land after-treatment method |
-
1960
- 1960-11-24 GB GB4041060A patent/GB902056A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114251192A (en) * | 2021-11-05 | 2022-03-29 | 航天科工火箭技术有限公司 | Liquid oxygen methane rocket land after-treatment method |
| CN114251192B (en) * | 2021-11-05 | 2023-03-24 | 航天科工火箭技术有限公司 | Liquid oxygen methane rocket land after-treatment method |
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