GB2156290B - Rockets and rocket motors - Google Patents
Rockets and rocket motorsInfo
- Publication number
- GB2156290B GB2156290B GB08506956A GB8506956A GB2156290B GB 2156290 B GB2156290 B GB 2156290B GB 08506956 A GB08506956 A GB 08506956A GB 8506956 A GB8506956 A GB 8506956A GB 2156290 B GB2156290 B GB 2156290B
- Authority
- GB
- United Kingdom
- Prior art keywords
- rockets
- rocket motors
- rocket
- motors
- 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
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/60—Steering arrangements
- F42B10/66—Steering by varying intensity or direction of thrust
- F42B10/663—Steering by varying intensity or direction of thrust using a plurality of transversally acting auxiliary nozzles, which are opened or closed by valves
-
- 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
- F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
- F02K9/86—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using nozzle throats of adjustable cross- section
-
- 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
- F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
- F02K9/88—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using auxiliary rocket nozzles
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Testing Of Engines (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8407919 | 1984-03-27 |
Publications (3)
Publication Number | Publication Date |
---|---|
GB8506956D0 GB8506956D0 (en) | 1985-04-24 |
GB2156290A GB2156290A (en) | 1985-10-09 |
GB2156290B true GB2156290B (en) | 1988-06-02 |
Family
ID=10558749
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB08506956A Expired GB2156290B (en) | 1984-03-27 | 1985-03-18 | Rockets and rocket motors |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2156290B (en) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4760694A (en) * | 1986-10-27 | 1988-08-02 | Rockwell International Corporation | Bi-level thruster |
FR2655723B1 (en) * | 1989-12-08 | 1993-01-22 | Thomson Brandt Armements | DEVICE FOR SEALING A NOZZLE FOR A GAS GENERATOR EQUIPPED WITH A FLYING MACHINE. |
FR2784444B1 (en) * | 1998-10-13 | 2000-12-29 | Celerg | METHOD AND DEVICE FOR CONTROLLING HOT GAS VALVE VALVES, PARTICULARLY FOR THE PILOTAGE AND / OR PROPULSION OF A MISSILE |
US6591603B2 (en) * | 2001-03-08 | 2003-07-15 | Trw Inc. | Pintle injector rocket with expansion-deflection nozzle |
DE102004045855B4 (en) | 2004-09-20 | 2006-06-29 | Eads Space Transportation Gmbh | Control and / or drive device for a missile |
FR2970742B1 (en) | 2011-01-20 | 2016-05-20 | Mbda France | DEVICE FOR CONTROLLING THE PASSAGE OF A GASEOUS JET IN A FLYING ENGINE TUYERE, AND FLYING ENGINE COMPRISING SUCH DEVICES |
FR3002982B1 (en) * | 2013-03-07 | 2015-04-10 | Herakles | GAS EJECTION SECTION MODULATION DEVICE. |
CN113687013B (en) * | 2021-07-30 | 2022-07-05 | 西北工业大学 | Device for shooting solid propellant combustion test under overload condition |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1488794A (en) * | 1973-10-04 | 1977-10-12 | Dresser Europe Sa | Control valve |
DE2424321A1 (en) * | 1974-05-18 | 1975-11-20 | Woma Maasberg Co Gmbh W | SHUT-OFF VALVE FOR HIGH AND HIGHEST PRESSURES, IN PARTICULAR FOR HIGH PRESSURE GUNS |
US4174824A (en) * | 1977-05-13 | 1979-11-20 | Eaton Corporation | Pressure operated pilot control shut-off valve |
ZA784019B (en) * | 1978-07-14 | 1980-01-30 | De Beers Ind Diamond | Ejector valve assemblies |
FR2504085A1 (en) * | 1981-04-21 | 1982-10-22 | Thomson Brandt | DEVICE FOR STEAMING BY GAS JETS AND PROJECTILE COMPRISING SUCH A DEVICE |
FR2508414B1 (en) * | 1981-06-30 | 1985-06-07 | Thomson Brandt | GAS JET STEERING DEVICE FOR A GUIDED MACHINE |
DE3144532A1 (en) * | 1981-11-10 | 1983-05-19 | Rheinmetall GmbH, 4000 Düsseldorf | WING STABILIZED SHELL |
FR2536720A1 (en) * | 1982-11-29 | 1984-06-01 | Aerospatiale | SYSTEM FOR CONTROLLING A MISSILE USING LATERAL GAS JETS AND MISSILE HAVING SUCH A SYSTEM |
-
1985
- 1985-03-18 GB GB08506956A patent/GB2156290B/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
GB8506956D0 (en) | 1985-04-24 |
GB2156290A (en) | 1985-10-09 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
732E | Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977) | ||
PE20 | Patent expired after termination of 20 years |
Effective date: 20050317 |