FR2235283A1 - Propellant blocks for rockers - with central combustion channel having unequal branches - Google Patents
Propellant blocks for rockers - with central combustion channel having unequal branchesInfo
- Publication number
- FR2235283A1 FR2235283A1 FR7323864A FR7323864A FR2235283A1 FR 2235283 A1 FR2235283 A1 FR 2235283A1 FR 7323864 A FR7323864 A FR 7323864A FR 7323864 A FR7323864 A FR 7323864A FR 2235283 A1 FR2235283 A1 FR 2235283A1
- Authority
- FR
- France
- Prior art keywords
- branches
- block
- combustion
- rockers
- radius
- 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.)
- Granted
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
- F02K9/10—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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Testing Of Engines (AREA)
Abstract
Propellant blocks, for central or internal combustion are partic. intended for the propulsion of rockets. The channel has several branches >=1 has its end situated at a distance greater than the ends of the other branches. The shorter branches are all equal and their ends lie on a cylinder with a radius of R-e, R being the radius of the block and the thickness of the combustible matl. of the block. The distance between the ends of the shorter branches and the external surface is therefore slightly less than e. Non-combustible zones are arranged on the periphery of the block, opposite the longest branches; they consist of thermal insulating material which resist the high combustion temp. They also thermal protect the inner wall of the power plant against which the block is applied they have an effect in restraining the progress of the combustion around the periphery. The surface of the central channel constitutes the initial combustion surface, by keeping this constant a constant thrust is obtd. during the course of the trajectory of the rocket.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7323864A FR2235283A1 (en) | 1973-06-29 | 1973-06-29 | Propellant blocks for rockers - with central combustion channel having unequal branches |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7323864A FR2235283A1 (en) | 1973-06-29 | 1973-06-29 | Propellant blocks for rockers - with central combustion channel having unequal branches |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2235283A1 true FR2235283A1 (en) | 1975-01-24 |
FR2235283B1 FR2235283B1 (en) | 1976-05-07 |
Family
ID=9121778
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7323864A Granted FR2235283A1 (en) | 1973-06-29 | 1973-06-29 | Propellant blocks for rockers - with central combustion channel having unequal branches |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2235283A1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2018510293A (en) * | 2015-02-12 | 2018-04-12 | チェアマン, ディフェンス リサーチ アンド ディヴェロップメント オーガナイゼーション (ディーアールディーオー)Chairman, Defence Research & Development Organisation (Drdo) | Propellant grain for solid rocket motors |
CN110529288A (en) * | 2019-08-28 | 2019-12-03 | 湖北三江航天江北机械工程有限公司 | Solid propellant rocket, the method and chamber structure for inhibiting medicine more than its powder charge |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3260045A (en) * | 1962-01-30 | 1966-07-12 | Propelling charge for solid-fuel rockets |
-
1973
- 1973-06-29 FR FR7323864A patent/FR2235283A1/en active Granted
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3260045A (en) * | 1962-01-30 | 1966-07-12 | Propelling charge for solid-fuel rockets |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2018510293A (en) * | 2015-02-12 | 2018-04-12 | チェアマン, ディフェンス リサーチ アンド ディヴェロップメント オーガナイゼーション (ディーアールディーオー)Chairman, Defence Research & Development Organisation (Drdo) | Propellant grain for solid rocket motors |
CN110529288A (en) * | 2019-08-28 | 2019-12-03 | 湖北三江航天江北机械工程有限公司 | Solid propellant rocket, the method and chamber structure for inhibiting medicine more than its powder charge |
Also Published As
Publication number | Publication date |
---|---|
FR2235283B1 (en) | 1976-05-07 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |