GB729525A - Improvements in or relating to solid propellant jet reaction motors - Google Patents
Improvements in or relating to solid propellant jet reaction motorsInfo
- Publication number
- GB729525A GB729525A GB992153A GB992153A GB729525A GB 729525 A GB729525 A GB 729525A GB 992153 A GB992153 A GB 992153A GB 992153 A GB992153 A GB 992153A GB 729525 A GB729525 A GB 729525A
- Authority
- GB
- United Kingdom
- Prior art keywords
- casing
- charge
- solid propellant
- ring
- relating
- 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
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
- F02K9/36—Propellant charge supports
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
- Jet Pumps And Other Pumps (AREA)
Abstract
729,525. Rocket motors. MINISTER OF SUPPLY. April 12, 1954 [April 11, 1953], No. 9921/53. Class 9(2). A rocket motor containing a cordite or other solid propellant charge, in the form of a hollow cylinder 11 inhibited from burning on the outer and end faces, is provided with a resilient U- section sealing ring 12, through which the charge extends, to prevent the flow of hot gases along the outer surface of the charge. The casing may be in two parts 14, 15, the part 15 remote from the exit nozzle 16 being less resistant to heat than the part 14. The part 14 is shown integral with the nozzle and made of steel, while the part 15 is of light alloy. The fore-part of the casing is recessed to form a seating for the ring and is connected by screw-threads to the rear part 14. Projections 17, 18 on the inner end faces of the casing allow free passage of the gases. The ring 12 may be partly embedded in the charge and the recess in the casing may be omitted.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB992153A GB729525A (en) | 1953-04-11 | 1953-04-11 | Improvements in or relating to solid propellant jet reaction motors |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB992153A GB729525A (en) | 1953-04-11 | 1953-04-11 | Improvements in or relating to solid propellant jet reaction motors |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB729525A true GB729525A (en) | 1955-05-04 |
Family
ID=9881242
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB992153A Expired GB729525A (en) | 1953-04-11 | 1953-04-11 | Improvements in or relating to solid propellant jet reaction motors |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB729525A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2591281A1 (en) * | 1985-12-05 | 1987-06-12 | Europ Propulsion | INTERNAL ANTI-CLAPPING ARRANGEMENT FOR A POWDER PROPELLER AND METHOD OF MANUFACTURING THE SAME |
-
1953
- 1953-04-11 GB GB992153A patent/GB729525A/en not_active Expired
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2591281A1 (en) * | 1985-12-05 | 1987-06-12 | Europ Propulsion | INTERNAL ANTI-CLAPPING ARRANGEMENT FOR A POWDER PROPELLER AND METHOD OF MANUFACTURING THE SAME |
| EP0226499A1 (en) * | 1985-12-05 | 1987-06-24 | Societe Europeenne De Propulsion | Internal stress relief arrangement for a solid-propulsion device, and method for its manufacture |
| US4803038A (en) * | 1985-12-05 | 1989-02-07 | Societe Europeenne De Propulsion | Internal anti-popping assembly for solid propellant rocket motor and its manufacturing process |
| US4823548A (en) * | 1985-12-05 | 1989-04-25 | Societe Europeenne De Propulsion | Internal anti-popping assembly for solid propellant rocket motor |
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