GB2571915B - Use of metal foam or lattice structures to support solid propellant - Google Patents
Use of metal foam or lattice structures to support solid propellant Download PDFInfo
- Publication number
- GB2571915B GB2571915B GB1802649.2A GB201802649A GB2571915B GB 2571915 B GB2571915 B GB 2571915B GB 201802649 A GB201802649 A GB 201802649A GB 2571915 B GB2571915 B GB 2571915B
- Authority
- GB
- United Kingdom
- Prior art keywords
- metal foam
- solid propellant
- lattice structures
- support solid
- support
- 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
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
- F02K9/32—Constructional parts; Details not otherwise provided for
- F02K9/34—Casings; Combustion chambers; Liners thereof
- F02K9/346—Liners, e.g. inhibitors
-
- 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
- F02K9/10—Shape or structure of solid propellant charges
- F02K9/16—Shape or structure of solid propellant charges of honeycomb structure
-
- 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
- F02K9/18—Shape or structure of solid propellant charges of the internal-burning type having a star or like shaped internal cavity
-
- 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
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/612—Foam
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1802649.2A GB2571915B (en) | 2018-02-19 | 2018-02-19 | Use of metal foam or lattice structures to support solid propellant |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1802649.2A GB2571915B (en) | 2018-02-19 | 2018-02-19 | Use of metal foam or lattice structures to support solid propellant |
Publications (3)
Publication Number | Publication Date |
---|---|
GB201802649D0 GB201802649D0 (en) | 2018-04-04 |
GB2571915A GB2571915A (en) | 2019-09-18 |
GB2571915B true GB2571915B (en) | 2023-07-19 |
Family
ID=61783848
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1802649.2A Active GB2571915B (en) | 2018-02-19 | 2018-02-19 | Use of metal foam or lattice structures to support solid propellant |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2571915B (en) |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3578520A (en) * | 1968-07-17 | 1971-05-11 | Gen Electric | Thermal insulation and bond for solid fuel motors and method of making same |
US3686868A (en) * | 1968-12-19 | 1972-08-29 | Michael John Chase | Rocket motors |
GB2103349A (en) * | 1981-05-26 | 1983-02-16 | Messerschmitt Boelkow Blohm | Combustion chamber |
GB2113811A (en) * | 1982-01-21 | 1983-08-10 | Messerschmitt Boelkow Blohm | Rocket motors |
GB2191115A (en) * | 1980-12-18 | 1987-12-09 | Secr Defence | Ablative material |
-
2018
- 2018-02-19 GB GB1802649.2A patent/GB2571915B/en active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3578520A (en) * | 1968-07-17 | 1971-05-11 | Gen Electric | Thermal insulation and bond for solid fuel motors and method of making same |
US3686868A (en) * | 1968-12-19 | 1972-08-29 | Michael John Chase | Rocket motors |
GB2191115A (en) * | 1980-12-18 | 1987-12-09 | Secr Defence | Ablative material |
GB2103349A (en) * | 1981-05-26 | 1983-02-16 | Messerschmitt Boelkow Blohm | Combustion chamber |
GB2113811A (en) * | 1982-01-21 | 1983-08-10 | Messerschmitt Boelkow Blohm | Rocket motors |
Also Published As
Publication number | Publication date |
---|---|
GB2571915A (en) | 2019-09-18 |
GB201802649D0 (en) | 2018-04-04 |
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