GB2612455B - 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 connection Download PDFInfo
- Publication number
- GB2612455B GB2612455B GB2216941.1A GB202216941A GB2612455B GB 2612455 B GB2612455 B GB 2612455B GB 202216941 A GB202216941 A GB 202216941A GB 2612455 B GB2612455 B GB 2612455B
- 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.)
- Active
Links
- 239000007787 solid Substances 0.000 title 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
- F02K9/08—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
- 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
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Testing Of Engines (AREA)
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 (3)
Publication Number | Publication Date |
---|---|
GB202216941D0 GB202216941D0 (en) | 2022-12-28 |
GB2612455A GB2612455A (en) | 2023-05-03 |
GB2612455B true GB2612455B (en) | 2024-06-19 |
Family
ID=73528116
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2216941.1A Active GB2612455B (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) | GB2612455B (en) |
WO (1) | WO2022068703A1 (en) |
Families Citing this family (9)
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 |
CN114135421B (en) * | 2021-11-29 | 2024-05-17 | 西安航天动力测控技术研究所 | Solid rocket engine head separation test device |
CN114104489B (en) * | 2021-12-16 | 2024-06-25 | 上海空间推进研究所 | Liquid rocket engine packing case |
CN114199574A (en) * | 2021-12-24 | 2022-03-18 | 内蒙航天动力机械测试所 | Solid rocket engine integration test tool |
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 |
CN117685134B (en) * | 2023-11-24 | 2024-05-17 | 北京航天试验技术研究所 | Supporting device, vertical injection system and installation method of vertical injection system |
Citations (7)
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 |
CN102818671A (en) * | 2012-08-16 | 2012-12-12 | 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 |
CN104019994A (en) * | 2014-04-24 | 2014-09-03 | 北京理工大学 | Overload testing device and method of solid rocket engine |
CN107100761A (en) * | 2017-06-29 | 2017-08-29 | 湖北三江航天江河化工科技有限公司 | A kind of test engine |
CN108590889A (en) * | 2018-05-09 | 2018-09-28 | 北京理工大学 | A kind of larynx hydrant change propulsive solid propellant rocket ground test device |
CN112012853A (en) * | 2020-10-04 | 2020-12-01 | 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 |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9140215B2 (en) * | 2012-03-14 | 2015-09-22 | Aerojet Rocketoyne Of De, Inc. | Rocket engine pressure sense line |
CN205785819U (en) * | 2016-05-24 | 2016-12-07 | 华中科技大学 | A kind of test device for rocket engine ground firing |
-
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/GB2612455B/en active Active
Patent Citations (7)
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 |
CN102818671A (en) * | 2012-08-16 | 2012-12-12 | 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 |
CN104019994A (en) * | 2014-04-24 | 2014-09-03 | 北京理工大学 | Overload testing device and method of solid rocket engine |
CN107100761A (en) * | 2017-06-29 | 2017-08-29 | 湖北三江航天江河化工科技有限公司 | A kind of test engine |
CN108590889A (en) * | 2018-05-09 | 2018-09-28 | 北京理工大学 | A kind of larynx hydrant change propulsive solid propellant rocket ground test device |
CN112012853A (en) * | 2020-10-04 | 2020-12-01 | 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 |
Also Published As
Publication number | Publication date |
---|---|
CN112012853B (en) | 2021-07-06 |
GB202216941D0 (en) | 2022-12-28 |
CN112012853A (en) | 2020-12-01 |
GB2612455A (en) | 2023-05-03 |
WO2022068703A1 (en) | 2022-04-07 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB2612455B (en) | Thrust transfer apparatus for ignition test of solid rocket engine in form of rear skirt connection | |
GB202314655D0 (en) | Solid rocket engine rear skirt connection mechanical arm type interstage separation test device and method | |
ZA202006130B (en) | Composition and method for preventing or reducing low speed pre-ignition in spark-ignited internal combustion engines | |
EP4121643A4 (en) | A homogeneous charge compression ignition (hcci-type) combustion system for an engine and powertrain using wet-alcohol as a fuel and including hot assist ignition | |
US11643997B2 (en) | Propulsion system with single initiator for multiple rocket motors | |
GB2592880B (en) | Method and gas fuel injection unit for operating an internal combustion engine | |
RU2012152897A (en) | METHOD FOR INCREASING THE RANGE OF THE FLIGHT OF THE ARTILLERY shell | |
GB202304227D0 (en) | Jet experiment bench for measurement of temperature field of engine piston | |
RU2544253C1 (en) | Method of missile takeoff from transporter-launcher container and device for its implementation | |
PL3766859T3 (en) | Hypergolic dual fuel system for rocket engines | |
EP3686421A4 (en) | Fuel injection control method and fuel injection device of spark ignition type internal-combustion engine | |
Teslenko et al. | GAS COMBUSTION IN WATER | |
ZA202207646B (en) | Test platform for rocket engine nozzle atomization test | |
Gradl | Hot-fire Testing of Additively Manufactured C-18150 (CuCrZr) Combustion Chamber Liner | |
RU2587186C1 (en) | Method of creating lift and thrust vector wing | |
GB202401822D0 (en) | Rocket engine | |
Tavakolifar et al. | Experimental investigation and numerical simulation of solid fuel rocket engine internal ballistic | |
US20230073547A1 (en) | Propulsion system with single initiator for multiple rocket motors | |
GB773190A (en) | Improvements relating to missiles and like bodies | |
Yu et al. | Research on synchronistic multi-ignitions of hydrogen-oxygen resonance ignitor | |
RU2075722C1 (en) | Process of filling of model of rocket with working medium and structure for its implementation | |
AU2023901162A0 (en) | Method and apparatus for priming diesel engines | |
AU2021900178A0 (en) | System and Method for Providing Additives to Internal Combustion Engines | |
RU2482425C1 (en) | Method to imitate conditions of mortar launch of rocket from submarine and system for its realisation | |
GB2580904B (en) | An internal combustion engine where fuel jets are directed towards pockets in the piston |