GB1250491A - - Google Patents
Info
- Publication number
- GB1250491A GB1250491A GB5700667A GB1250491DA GB1250491A GB 1250491 A GB1250491 A GB 1250491A GB 5700667 A GB5700667 A GB 5700667A GB 1250491D A GB1250491D A GB 1250491DA GB 1250491 A GB1250491 A GB 1250491A
- Authority
- GB
- United Kingdom
- Prior art keywords
- nozzle
- pipes
- supplied
- bearing surface
- rocket
- 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
- 238000001816 cooling Methods 0.000 abstract 2
- 239000007788 liquid Substances 0.000 abstract 2
- 238000002485 combustion reaction Methods 0.000 abstract 1
- 230000000295 complement effect Effects 0.000 abstract 1
- 239000012809 cooling fluid Substances 0.000 abstract 1
- 230000000694 effects 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
- 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
- F42B10/666—Steering by varying intensity or direction of thrust characterised by using a nozzle rotatable about an axis transverse to the axis of the projectile
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/38—Jet flaps
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/40—Arrangements or adaptations of propulsion systems
- B64G1/401—Liquid propellant rocket engines
-
- 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
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/44—Feeding propellants
- F02K9/50—Feeding propellants using pressurised fluid to pressurise the propellants
-
- 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
- F02K9/84—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using movable nozzles
-
- 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
- F42B15/34—Protection against overheating or radiation, e.g. heat shields; Additional cooling arrangements
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/40—Arrangements or adaptations of propulsion systems
- B64G1/402—Propellant tanks; Feeding propellants
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Remote Sensing (AREA)
- Mechanical Engineering (AREA)
- Fluid Mechanics (AREA)
- Nozzles (AREA)
- Testing Of Engines (AREA)
- Magnetic Bearings And Hydrostatic Bearings (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB5700667 | 1967-12-15 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1250491A true GB1250491A (de) | 1971-10-20 |
Family
ID=10478117
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB5700667A Expired GB1250491A (de) | 1967-12-15 | 1967-12-15 |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE1814636A1 (de) |
FR (1) | FR1596085A (de) |
GB (1) | GB1250491A (de) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2017011208A1 (en) * | 2015-07-13 | 2017-01-19 | Aerojet Rocketdyne, Inc. | Flow control system with parallel fuel passage network |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2580038B1 (de) * | 1985-04-04 | 1987-06-19 | Centre Nat Etd Spatiales | |
DE3826180A1 (de) * | 1988-08-02 | 1990-02-08 | Happich Gmbh Gebr | Behaelter, insbesondere ascher fuer fahrzeuge |
-
1967
- 1967-12-15 GB GB5700667A patent/GB1250491A/en not_active Expired
-
1968
- 1968-12-13 DE DE19681814636 patent/DE1814636A1/de active Pending
- 1968-12-13 FR FR1596085D patent/FR1596085A/fr not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2017011208A1 (en) * | 2015-07-13 | 2017-01-19 | Aerojet Rocketdyne, Inc. | Flow control system with parallel fuel passage network |
US10837406B2 (en) | 2015-07-13 | 2020-11-17 | Aerojet Rocketdyne, Inc. | Flow control system for a rocket engine with parallel fuel passage network |
Also Published As
Publication number | Publication date |
---|---|
FR1596085A (de) | 1970-06-15 |
DE1814636A1 (de) | 1969-09-25 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3659788A (en) | Jet nozzle assembly | |
TW360607B (en) | Underwater two-phrase ramjet engine | |
US3049877A (en) | Nozzle for reaction motor | |
GB1386232A (en) | Fluid propulsion systems | |
GB881513A (en) | Improvements relating to turbo-jet propulsion units in aircraft | |
US2780914A (en) | Ambient pressure responsive control for fuel oxidizer and nozzle exhaust area of reaction motors | |
US3171379A (en) | Hydro-pneumatic ramjet | |
US3230708A (en) | Steerable rocket motor with gimballed nozzle means and cooling means | |
US3270505A (en) | Control system for rocket vehicles | |
US2594766A (en) | Apparatus for steering aircraft | |
US3276466A (en) | Rotary hot gas valve | |
GB955050A (en) | Improvements relating to a rocket power-plant | |
US2407852A (en) | Reaction motor | |
US3232049A (en) | Fluid injection apparatus | |
GB1250491A (de) | ||
US4318271A (en) | Igniter and gas generator for rocket motor | |
US3058304A (en) | Steering control for rocket | |
GB1407428A (en) | Gas turbine engine having a power turbine system adapted to be selectively cut in | |
US3819117A (en) | Thrust vector {13 {11 jet interaction vehicle control system | |
US2974902A (en) | Power plant for helicopter | |
GB1248573A (en) | Jet propulsion thrust-producing means having a nozzle mounted for swivelling | |
GB1177954A (en) | Fluid Flow Duct | |
US3058449A (en) | Rocket engine control | |
RU2390648C1 (ru) | Жидкостный ракетный двигатель | |
US3386688A (en) | Aircraft provided with an engine and a retractable fairing therefor |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PLNP | Patent lapsed through nonpayment of renewal fees |