GB739417A - Improvements in rocket motors - Google Patents
Improvements in rocket motorsInfo
- Publication number
- GB739417A GB739417A GB3661/54A GB366154A GB739417A GB 739417 A GB739417 A GB 739417A GB 3661/54 A GB3661/54 A GB 3661/54A GB 366154 A GB366154 A GB 366154A GB 739417 A GB739417 A GB 739417A
- Authority
- GB
- United Kingdom
- Prior art keywords
- grid
- plug
- propellant
- openings
- casing
- 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
- 239000003380 propellant Substances 0.000 abstract 3
- 239000007789 gas Substances 0.000 abstract 1
- 239000002184 metal Substances 0.000 abstract 1
- 239000000203 mixture Substances 0.000 abstract 1
- 238000009527 percussion Methods 0.000 abstract 1
- 230000003019 stabilising effect Effects 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
-
- 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
- F02K9/30—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants with the propulsion gases exhausting through a plurality of nozzles
-
- 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
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Devices Affording Protection Of Roads Or Walls For Sound Insulation (AREA)
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH739417X | 1953-03-14 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB739417A true GB739417A (en) | 1955-10-26 |
Family
ID=4533013
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3661/54A Expired GB739417A (en) | 1953-03-14 | 1954-02-08 | Improvements in rocket motors |
Country Status (5)
Country | Link |
---|---|
BE (1) | BE525998A (enrdf_load_stackoverflow) |
CH (1) | CH324499A (enrdf_load_stackoverflow) |
DE (1) | DE934996C (enrdf_load_stackoverflow) |
FR (1) | FR1154410A (enrdf_load_stackoverflow) |
GB (1) | GB739417A (enrdf_load_stackoverflow) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2456217A1 (fr) * | 1979-05-11 | 1980-12-05 | Raytheon Co | Moteur-fusee |
RU2132964C1 (ru) * | 1996-08-14 | 1999-07-10 | Полканов Юрий Федорович | Активно-реактивный двигатель |
CN113202563A (zh) * | 2021-04-22 | 2021-08-03 | 沈阳航空航天大学 | 减弱导弹发射尾焰能量的同轴反转双级涡轮装置 |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1104867B (de) * | 1958-02-11 | 1961-04-13 | J G W Berckholtz Fa | Rakete mit Stabilisiereinrichtung |
DE1154978B (de) * | 1961-06-12 | 1963-09-26 | Rheinmetall Gmbh | Treibsatz fuer Feststoffraketen, insbesondere fuer Kurzbrennraketen |
-
0
- BE BE525998D patent/BE525998A/xx unknown
-
1953
- 1953-03-14 CH CH324499D patent/CH324499A/fr unknown
-
1954
- 1954-01-27 DE DEA19578A patent/DE934996C/de not_active Expired
- 1954-02-01 FR FR1154410D patent/FR1154410A/fr not_active Expired
- 1954-02-08 GB GB3661/54A patent/GB739417A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2456217A1 (fr) * | 1979-05-11 | 1980-12-05 | Raytheon Co | Moteur-fusee |
RU2132964C1 (ru) * | 1996-08-14 | 1999-07-10 | Полканов Юрий Федорович | Активно-реактивный двигатель |
CN113202563A (zh) * | 2021-04-22 | 2021-08-03 | 沈阳航空航天大学 | 减弱导弹发射尾焰能量的同轴反转双级涡轮装置 |
CN113202563B (zh) * | 2021-04-22 | 2022-08-16 | 沈阳航空航天大学 | 减弱导弹发射尾焰能量的同轴反转双级涡轮装置 |
Also Published As
Publication number | Publication date |
---|---|
FR1154410A (fr) | 1958-04-10 |
DE934996C (de) | 1955-11-10 |
BE525998A (enrdf_load_stackoverflow) | |
CH324499A (fr) | 1957-09-30 |
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