FR1197701A - Device suitable for steering rocket-propelled mobiles - Google Patents
Device suitable for steering rocket-propelled mobilesInfo
- Publication number
- FR1197701A FR1197701A FR1197701DA FR1197701A FR 1197701 A FR1197701 A FR 1197701A FR 1197701D A FR1197701D A FR 1197701DA FR 1197701 A FR1197701 A FR 1197701A
- Authority
- FR
- France
- Prior art keywords
- mobiles
- propelled
- device suitable
- steering rocket
- 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
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
- F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
- F02K9/82—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control by injection of a secondary fluid into the rocket exhaust gases
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1197701T | 1957-12-11 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1197701A true FR1197701A (en) | 1959-12-02 |
Family
ID=9669780
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1197701D Expired FR1197701A (en) | 1957-12-11 | 1957-12-11 | Device suitable for steering rocket-propelled mobiles |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1197701A (en) |
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3091924A (en) * | 1960-12-15 | 1963-06-04 | United Aircraft Corp | Gaseous nozzle boundary |
US3092963A (en) * | 1960-12-15 | 1963-06-11 | United Aircraft Corp | Vector control system |
US3101591A (en) * | 1961-03-28 | 1963-08-27 | Thompson Ramo Wooldridge Inc | Vapor-gas injection thrust vector control system |
US3116603A (en) * | 1961-08-15 | 1964-01-07 | United Aircraft Corp | Combined nozzle cooling and thrust vectoring |
US3132476A (en) * | 1961-04-27 | 1964-05-12 | Earl W Conrad | Thrust vector control apparatus |
US3132478A (en) * | 1961-07-13 | 1964-05-12 | Thompson Ramo Wooldridge Inc | Solid propellant gas rotary valve |
US3133413A (en) * | 1960-09-12 | 1964-05-19 | United Aircraft Corp | Control and cooling of rocket motors |
US3137126A (en) * | 1961-01-11 | 1964-06-16 | North American Aviation Inc | Method and means for forming a gaseous passage |
US3144752A (en) * | 1961-10-02 | 1964-08-18 | United Aircraft Corp | Injection thrust vectoring |
US3212259A (en) * | 1962-11-19 | 1965-10-19 | Kepler Charles Edward | Tertiary flow injection thrust vectoring system |
US3213611A (en) * | 1962-04-23 | 1965-10-26 | Bendix Corp | Valve |
US3228188A (en) * | 1963-03-29 | 1966-01-11 | Atlantic Res Corp | Thrust-vector control system |
US3239150A (en) * | 1961-11-29 | 1966-03-08 | Continental Aviat & Eng Corp | Thrust vector control |
US3255971A (en) * | 1962-11-21 | 1966-06-14 | Bendix Corp | Jet thrust vector control apparatus |
-
1957
- 1957-12-11 FR FR1197701D patent/FR1197701A/en not_active Expired
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3133413A (en) * | 1960-09-12 | 1964-05-19 | United Aircraft Corp | Control and cooling of rocket motors |
US3092963A (en) * | 1960-12-15 | 1963-06-11 | United Aircraft Corp | Vector control system |
US3091924A (en) * | 1960-12-15 | 1963-06-04 | United Aircraft Corp | Gaseous nozzle boundary |
US3137126A (en) * | 1961-01-11 | 1964-06-16 | North American Aviation Inc | Method and means for forming a gaseous passage |
US3101591A (en) * | 1961-03-28 | 1963-08-27 | Thompson Ramo Wooldridge Inc | Vapor-gas injection thrust vector control system |
US3132476A (en) * | 1961-04-27 | 1964-05-12 | Earl W Conrad | Thrust vector control apparatus |
US3132478A (en) * | 1961-07-13 | 1964-05-12 | Thompson Ramo Wooldridge Inc | Solid propellant gas rotary valve |
US3116603A (en) * | 1961-08-15 | 1964-01-07 | United Aircraft Corp | Combined nozzle cooling and thrust vectoring |
US3144752A (en) * | 1961-10-02 | 1964-08-18 | United Aircraft Corp | Injection thrust vectoring |
US3239150A (en) * | 1961-11-29 | 1966-03-08 | Continental Aviat & Eng Corp | Thrust vector control |
US3213611A (en) * | 1962-04-23 | 1965-10-26 | Bendix Corp | Valve |
US3212259A (en) * | 1962-11-19 | 1965-10-19 | Kepler Charles Edward | Tertiary flow injection thrust vectoring system |
US3255971A (en) * | 1962-11-21 | 1966-06-14 | Bendix Corp | Jet thrust vector control apparatus |
US3228188A (en) * | 1963-03-29 | 1966-01-11 | Atlantic Res Corp | Thrust-vector control system |
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