CH466088A - Ensemble constitué, d'une part, d'un missile et, d'autre part, d'une installation de lancement - Google Patents
Ensemble constitué, d'une part, d'un missile et, d'autre part, d'une installation de lancementInfo
- Publication number
- CH466088A CH466088A CH1883966A CH1883966A CH466088A CH 466088 A CH466088 A CH 466088A CH 1883966 A CH1883966 A CH 1883966A CH 1883966 A CH1883966 A CH 1883966A CH 466088 A CH466088 A CH 466088A
- Authority
- CH
- Switzerland
- Prior art keywords
- hand
- missile
- assembly consisting
- launch facility
- launch
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
-
- 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
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/44—Feeding propellants
- F02K9/56—Control
- F02K9/58—Propellant feed 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
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/60—Constructional parts; Details not otherwise provided for
- F02K9/605—Reservoirs
-
- 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
- F02K9/72—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid and solid propellants, i.e. hybrid rocket-engine plants
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR44317A FR1469194A (fr) | 1965-12-30 | 1965-12-30 | Perfectionnements apportés aux missiles à générateur de gaz à au moins un ergolliquide soumis à la pression directe d'un gaz de chasse et aux installations de lancement de tels missiles |
Publications (1)
Publication Number | Publication Date |
---|---|
CH466088A true CH466088A (fr) | 1968-11-30 |
Family
ID=8597317
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH1883966A CH466088A (fr) | 1965-12-30 | 1966-12-29 | Ensemble constitué, d'une part, d'un missile et, d'autre part, d'une installation de lancement |
Country Status (5)
Country | Link |
---|---|
US (1) | US3443475A (fr) |
CH (1) | CH466088A (fr) |
FR (1) | FR1469194A (fr) |
IL (1) | IL27151A (fr) |
SE (1) | SE302906B (fr) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2249620B (en) * | 1981-08-19 | 1992-08-19 | British Aerospace | Cryogenic system |
FR2580038B1 (fr) * | 1985-04-04 | 1987-06-19 | Centre Nat Etd Spatiales | |
US5767973A (en) * | 1996-02-07 | 1998-06-16 | Simmons Machine Tool Corporation | Wheelset sensing system |
US5722232A (en) * | 1994-10-13 | 1998-03-03 | Martin Marietta Corporation | Hybrid helium heater pressurization system and electrical ignition system for pressure-fed hybrid rockets |
US6016652A (en) * | 1994-10-21 | 2000-01-25 | Hy-Pat Corporation | Hybrid rocket system with disposable cartridge |
US5715675A (en) * | 1994-10-21 | 1998-02-10 | Environmental Aeroscience Corp. | Hybrid rocket system and integrated motor for use therein |
US5582366A (en) * | 1995-01-19 | 1996-12-10 | Motorola, Inc. | Satellite fueling system and method therefor |
US5794435A (en) * | 1996-02-07 | 1998-08-18 | Lockhhed Martin Corporation | Stable-combustion oxidizer vaporizer for hybrid rockets |
US5939491A (en) * | 1997-08-01 | 1999-08-17 | Ppg Industries Ohio, Inc. | Curable compositions based on functional polysiloxanes |
US6125763A (en) * | 1998-08-14 | 2000-10-03 | Environmental Aeroscience Corp. | Integral solid booster and hybrid thrust sustaining system and projectile incorporating the same |
RU2572179C2 (ru) * | 2014-08-12 | 2015-12-27 | Анатолий Степанович Дресвянкин | Пусковая установка |
WO2018013504A1 (fr) * | 2016-07-11 | 2018-01-18 | Aerojet Rocketdyne, Inc. | Injection par écoulement piston de carburant hypergolique de système hydraulique au sol |
CN109595098B (zh) * | 2019-01-29 | 2024-02-27 | 九州云箭(北京)空间科技有限公司 | 一种液体火箭发动机的混合比多开度调节阀 |
CN115127394B (zh) * | 2022-06-08 | 2023-07-28 | 中国人民解放军96901部队22分队 | 一种火箭弹射动力气体均压减压整流装置及控制方法 |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2441363A (en) * | 1945-05-19 | 1948-05-11 | Accessories Mfg And Engineerin | Coupling |
US2962934A (en) * | 1955-06-13 | 1960-12-06 | Garrett Corp | Vehicle propulsion apparatus |
US3116599A (en) * | 1962-02-26 | 1964-01-07 | Lockheed Aircraft Corp | Starter for rocket motor |
US3340691A (en) * | 1965-10-14 | 1967-09-12 | Thiokol Chemical Corp | Command controllable self-pressurizing liquid injection system |
-
1965
- 1965-12-30 FR FR44317A patent/FR1469194A/fr not_active Expired
-
1966
- 1966-12-26 IL IL27151A patent/IL27151A/xx unknown
- 1966-12-27 US US606517A patent/US3443475A/en not_active Expired - Lifetime
- 1966-12-29 CH CH1883966A patent/CH466088A/fr unknown
- 1966-12-29 SE SE17843/66A patent/SE302906B/xx unknown
Also Published As
Publication number | Publication date |
---|---|
FR1469194A (fr) | 1967-02-10 |
IL27151A (en) | 1970-12-24 |
SE302906B (fr) | 1968-08-05 |
US3443475A (en) | 1969-05-13 |
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