GB202216941D0 - Thrust transfer apparatus for ignition test of solid rocket engine in form of rear skirt connection - Google Patents
Thrust transfer apparatus for ignition test of solid rocket engine in form of rear skirt connectionInfo
- Publication number
- GB202216941D0 GB202216941D0 GBGB2216941.1A GB202216941A GB202216941D0 GB 202216941 D0 GB202216941 D0 GB 202216941D0 GB 202216941 A GB202216941 A GB 202216941A GB 202216941 D0 GB202216941 D0 GB 202216941D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- transfer apparatus
- rocket engine
- solid rocket
- rear skirt
- ignition test
- 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.)
- Pending
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
- F02K9/96—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by specially adapted arrangements for testing or measuring
-
- 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
- F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid 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
- F02K9/95—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by starting or ignition means or arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/83—Testing, e.g. methods, components or tools therefor
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202011066998.7A CN112012853B (en) | 2020-10-04 | 2020-10-04 | Solid rocket engine of back skirt connection form thrust transmission device for ignition test |
PCT/CN2021/120509 WO2022068703A1 (en) | 2020-10-04 | 2021-09-25 | Thrust transfer apparatus for ignition test of solid rocket engine in form of rear skirt connection |
Publications (2)
Publication Number | Publication Date |
---|---|
GB202216941D0 true GB202216941D0 (en) | 2022-12-28 |
GB2612455A GB2612455A (en) | 2023-05-03 |
Family
ID=73528116
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2216941.1A Pending GB2612455A (en) | 2020-10-04 | 2021-09-25 | Thrust transfer apparatus for ignition test of solid rocket engine in form of rear skirt connection |
Country Status (3)
Country | Link |
---|---|
CN (1) | CN112012853B (en) |
GB (1) | GB2612455A (en) |
WO (1) | WO2022068703A1 (en) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112012853B (en) * | 2020-10-04 | 2021-07-06 | 西安航天动力测控技术研究所 | Solid rocket engine of back skirt connection form thrust transmission device for ignition test |
CN113638822B (en) * | 2021-06-30 | 2023-12-29 | 西安航天动力测控技术研究所 | Mechanical arm type interstage separation test device for rear skirt connection of solid rocket engine |
CN114184386B (en) * | 2021-11-29 | 2023-07-21 | 西安航天动力测控技术研究所 | Spherical solid rocket engine testing device |
CN114856867B (en) * | 2022-05-27 | 2024-02-06 | 哈尔滨工程大学 | Active vibration damper of solid rocket engine |
CN115184028B (en) * | 2022-08-25 | 2023-09-01 | 芜湖中科飞机制造有限公司 | Fixing device for aeroengine detection |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6032545A (en) * | 1998-04-17 | 2000-03-07 | California Polytechnic State University Foundation | Nozzle flow thrust vector measurement |
US9140215B2 (en) * | 2012-03-14 | 2015-09-22 | Aerojet Rocketoyne Of De, Inc. | Rocket engine pressure sense line |
CN102818671B (en) * | 2012-08-16 | 2014-06-18 | 北京航空航天大学 | High-precision liquid or gas rocket engine thrust rack |
CN103115716A (en) * | 2013-01-25 | 2013-05-22 | 南京理工大学 | Thrust block device of six-component test stand |
CN104019994B (en) * | 2014-04-24 | 2017-03-01 | 北京理工大学 | A kind of solid propellant rocket overload test device |
CN205785819U (en) * | 2016-05-24 | 2016-12-07 | 华中科技大学 | A kind of test device for rocket engine ground firing |
CN107100761B (en) * | 2017-06-29 | 2019-07-02 | 湖北三江航天江河化工科技有限公司 | A kind of test engine |
CN108590889B (en) * | 2018-05-09 | 2020-04-14 | 北京理工大学 | Throat bolt type variable thrust solid rocket engine ground testing device |
CN112012853B (en) * | 2020-10-04 | 2021-07-06 | 西安航天动力测控技术研究所 | Solid rocket engine of back skirt connection form thrust transmission device for ignition test |
-
2020
- 2020-10-04 CN CN202011066998.7A patent/CN112012853B/en active Active
-
2021
- 2021-09-25 WO PCT/CN2021/120509 patent/WO2022068703A1/en active Application Filing
- 2021-09-25 GB GB2216941.1A patent/GB2612455A/en active Pending
Also Published As
Publication number | Publication date |
---|---|
WO2022068703A1 (en) | 2022-04-07 |
CN112012853A (en) | 2020-12-01 |
GB2612455A (en) | 2023-05-03 |
CN112012853B (en) | 2021-07-06 |
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