IT9067979A0 - DEVICE FOR CLOSING A NOZZLE FOR A GAS GENERATOR EQUIPPING A FLYING ORDN - Google Patents
DEVICE FOR CLOSING A NOZZLE FOR A GAS GENERATOR EQUIPPING A FLYING ORDNInfo
- Publication number
- IT9067979A0 IT9067979A0 IT67979A IT6797990A IT9067979A0 IT 9067979 A0 IT9067979 A0 IT 9067979A0 IT 67979 A IT67979 A IT 67979A IT 6797990 A IT6797990 A IT 6797990A IT 9067979 A0 IT9067979 A0 IT 9067979A0
- Authority
- IT
- Italy
- Prior art keywords
- ordn
- flying
- nozzle
- closing
- gas generator
- Prior art date
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
- F02K9/74—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant
- F02K9/76—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant with another rocket-engine plant; Multistage rocket-engine plants
-
- 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
-
- 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
- F42B15/36—Means for interconnecting rocket-motor and body section; Multi-stage connectors; Disconnecting means
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Chemical & Material Sciences (AREA)
- Fluid Mechanics (AREA)
- Physics & Mathematics (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Plasma Technology (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
- Slot Machines And Peripheral Devices (AREA)
- Devices For Medical Bathing And Washing (AREA)
- Portable Nailing Machines And Staplers (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8916263A FR2655723B1 (en) | 1989-12-08 | 1989-12-08 | DEVICE FOR SEALING A NOZZLE FOR A GAS GENERATOR EQUIPPED WITH A FLYING MACHINE. |
Publications (3)
Publication Number | Publication Date |
---|---|
IT9067979A0 true IT9067979A0 (en) | 1990-12-07 |
IT9067979A1 IT9067979A1 (en) | 1991-06-09 |
IT1241020B IT1241020B (en) | 1993-12-27 |
Family
ID=9388298
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT67979A IT1241020B (en) | 1989-12-08 | 1990-12-07 | NOZZLE CLOSING DEVICE FOR A GAS GENERATOR PROVIDED WITH A FLYING ORDER |
Country Status (3)
Country | Link |
---|---|
FR (1) | FR2655723B1 (en) |
GB (1) | GB2238857A (en) |
IT (1) | IT1241020B (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5435128A (en) * | 1993-11-15 | 1995-07-25 | Thiokol Corporation | Pyrotechnically driven nozzle restrictor |
RU2461729C1 (en) * | 2011-08-02 | 2012-09-20 | Николай Евгеньевич Староверов | Self-adjusted two-mode nozzle (versions) |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2613497A (en) * | 1947-04-01 | 1952-10-14 | Macdonald Gilmour Craig | Controllable rocket thrust device |
US3230704A (en) * | 1961-10-30 | 1966-01-25 | Thiokol Chemical Corp | Rocket engine |
US3329089A (en) * | 1964-12-24 | 1967-07-04 | Herbert L Harrison | Retention-release mechanism for reaction motors and rocket interstages |
US3691770A (en) * | 1966-12-02 | 1972-09-19 | Us Navy | Thrust control means for a solid propellant rocket motor |
GB1538192A (en) * | 1968-05-18 | 1979-01-10 | Karlsruhe Augsburg Iweka | Cartridge-type missile |
DE2320076A1 (en) * | 1973-04-19 | 1974-11-14 | Norbert Mieseler | ADJUSTABLE ROCKET MOTOR |
DE2605428A1 (en) * | 1976-02-12 | 1977-08-18 | Messerschmitt Boelkow Blohm | COMPRESSED GAS TANK FOR ONE FLOOR |
SE419800B (en) * | 1978-02-23 | 1981-08-24 | Sven Landstrom | REMSPROJEKTIL |
GB2156290B (en) * | 1984-03-27 | 1988-06-02 | British Aerospace | Rockets and rocket motors |
-
1989
- 1989-12-08 FR FR8916263A patent/FR2655723B1/en not_active Expired - Fee Related
-
1990
- 1990-12-06 GB GB9026535A patent/GB2238857A/en not_active Withdrawn
- 1990-12-07 IT IT67979A patent/IT1241020B/en active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
FR2655723B1 (en) | 1993-01-22 |
GB2238857A (en) | 1991-06-12 |
IT1241020B (en) | 1993-12-27 |
FR2655723A1 (en) | 1991-06-14 |
GB9026535D0 (en) | 1991-01-23 |
IT9067979A1 (en) | 1991-06-09 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
0001 | Granted |