IT201700115681A1 - Procedimento di collaudo per collaudare un motore a propellente solido, e motore a propellente solido per attuare tale procedimento - Google Patents
Procedimento di collaudo per collaudare un motore a propellente solido, e motore a propellente solido per attuare tale procedimentoInfo
- Publication number
- IT201700115681A1 IT201700115681A1 IT102017000115681A IT201700115681A IT201700115681A1 IT 201700115681 A1 IT201700115681 A1 IT 201700115681A1 IT 102017000115681 A IT102017000115681 A IT 102017000115681A IT 201700115681 A IT201700115681 A IT 201700115681A IT 201700115681 A1 IT201700115681 A1 IT 201700115681A1
- Authority
- IT
- Italy
- Prior art keywords
- engine
- procedure
- test
- solid propellent
- implement
- Prior art date
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
- F02K9/10—Shape or structure of solid propellant charges
-
- 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
- F02K9/24—Charging rocket engines with solid propellants; Methods or apparatus specially adapted for working solid propellant charges
-
- 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
- F02K9/32—Constructional parts; Details not otherwise provided for
- F02K9/34—Casings; Combustion chambers; Liners thereof
- F02K9/343—Joints, connections, seals therefor
-
- 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
- F02K9/32—Constructional parts; Details not otherwise provided for
- F02K9/36—Propellant charge supports
-
- 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
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/231—Preventing heat transfer
-
- 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
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/6111—Properties or characteristics given to material by treatment or manufacturing functionally graded coating
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Testing Of Engines (AREA)
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT102017000115681A IT201700115681A1 (it) | 2017-10-13 | 2017-10-13 | Procedimento di collaudo per collaudare un motore a propellente solido, e motore a propellente solido per attuare tale procedimento |
EP18796496.0A EP3695106B1 (en) | 2017-10-13 | 2018-10-11 | Test method for testing a solid-propellant rocket engine, solid-propellant rocket engine and system for implementing the method |
ES18796496T ES2898314T3 (es) | 2017-10-13 | 2018-10-11 | Método de ensayo para probar un motor de cohete con propergol sólido, un motor de cohete con propergol sólido y sistema para implementar el método |
PCT/IB2018/057896 WO2019073437A1 (en) | 2017-10-13 | 2018-10-11 | TESTING METHOD FOR TESTING A SOLID PROPERGOL FUSED ENGINE, SOLID PROPERGOL FUSED ENGINE-FUSE AND SYSTEM FOR IMPLEMENTING THE METHOD |
US16/755,068 US11280296B2 (en) | 2017-10-13 | 2018-10-11 | Test method for testing a solid-propellant rocket engine, solid-propellant rocket engine and system for implementing the method |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT102017000115681A IT201700115681A1 (it) | 2017-10-13 | 2017-10-13 | Procedimento di collaudo per collaudare un motore a propellente solido, e motore a propellente solido per attuare tale procedimento |
Publications (1)
Publication Number | Publication Date |
---|---|
IT201700115681A1 true IT201700115681A1 (it) | 2019-04-13 |
Family
ID=61224315
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT102017000115681A IT201700115681A1 (it) | 2017-10-13 | 2017-10-13 | Procedimento di collaudo per collaudare un motore a propellente solido, e motore a propellente solido per attuare tale procedimento |
Country Status (5)
Country | Link |
---|---|
US (1) | US11280296B2 (it) |
EP (1) | EP3695106B1 (it) |
ES (1) | ES2898314T3 (it) |
IT (1) | IT201700115681A1 (it) |
WO (1) | WO2019073437A1 (it) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN117367808A (zh) * | 2023-04-24 | 2024-01-09 | 中国人民解放军国防科技大学 | 一种用于发动机静止试验的免焊接自相似防护结构 |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114184386B (zh) * | 2021-11-29 | 2023-07-21 | 西安航天动力测控技术研究所 | 一种球形固体火箭发动机测试装置 |
CN113915029A (zh) * | 2021-12-14 | 2022-01-11 | 星河动力(北京)空间科技有限公司 | 火箭发动机喷管喉衬的测试装置 |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2466627A1 (fr) * | 1979-10-05 | 1981-04-10 | Europ Propulsion | Dispositif anti-clappement pour propulseur a propergol solide |
EP0226499A1 (fr) * | 1985-12-05 | 1987-06-24 | Societe Europeenne De Propulsion | Aménagement interne anti-clappement pour propulseur à poudre et son procédé de fabrication |
US4711086A (en) * | 1986-10-24 | 1987-12-08 | The United States Of America As Represented By The Secretary Of The Navy | Trident II first and second stage internal insulation |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4149404A (en) * | 1978-05-24 | 1979-04-17 | The United States Of America As Represented By The Secretary Of The Army | Pressure testing of rocket motor cases |
US5289723A (en) * | 1992-06-05 | 1994-03-01 | Thiokol Corporation | Antisymmetric grain support test device and methods |
-
2017
- 2017-10-13 IT IT102017000115681A patent/IT201700115681A1/it unknown
-
2018
- 2018-10-11 US US16/755,068 patent/US11280296B2/en active Active
- 2018-10-11 EP EP18796496.0A patent/EP3695106B1/en active Active
- 2018-10-11 WO PCT/IB2018/057896 patent/WO2019073437A1/en unknown
- 2018-10-11 ES ES18796496T patent/ES2898314T3/es active Active
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2466627A1 (fr) * | 1979-10-05 | 1981-04-10 | Europ Propulsion | Dispositif anti-clappement pour propulseur a propergol solide |
EP0226499A1 (fr) * | 1985-12-05 | 1987-06-24 | Societe Europeenne De Propulsion | Aménagement interne anti-clappement pour propulseur à poudre et son procédé de fabrication |
US4711086A (en) * | 1986-10-24 | 1987-12-08 | The United States Of America As Represented By The Secretary Of The Navy | Trident II first and second stage internal insulation |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN117367808A (zh) * | 2023-04-24 | 2024-01-09 | 中国人民解放军国防科技大学 | 一种用于发动机静止试验的免焊接自相似防护结构 |
CN117367808B (zh) * | 2023-04-24 | 2024-04-30 | 中国人民解放军国防科技大学 | 一种用于发动机静止试验的免焊接自相似防护结构 |
Also Published As
Publication number | Publication date |
---|---|
WO2019073437A1 (en) | 2019-04-18 |
EP3695106A1 (en) | 2020-08-19 |
US11280296B2 (en) | 2022-03-22 |
ES2898314T3 (es) | 2022-03-07 |
EP3695106B1 (en) | 2021-08-25 |
US20210190014A1 (en) | 2021-06-24 |
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