FR1108090A - Perfectionnement aux fusées - Google Patents
Perfectionnement aux fuséesInfo
- Publication number
- FR1108090A FR1108090A FR1108090DA FR1108090A FR 1108090 A FR1108090 A FR 1108090A FR 1108090D A FR1108090D A FR 1108090DA FR 1108090 A FR1108090 A FR 1108090A
- Authority
- FR
- France
- Prior art keywords
- rocket
- training
- rocket training
- 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
- F02K9/97—Rocket nozzles
- F02K9/972—Fluid cooling arrangements for nozzles
-
- 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
- F02K9/62—Combustion or thrust chambers
- F02K9/64—Combustion or thrust chambers having cooling arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/203—Heat transfer, e.g. cooling by transpiration cooling
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 |
---|---|---|---|
FR1108090T | 1954-07-01 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1108090A true FR1108090A (fr) | 1956-01-09 |
Family
ID=9624819
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1108090D Expired FR1108090A (fr) | 1954-07-01 | 1954-07-01 | Perfectionnement aux fusées |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1108090A (fr) |
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3073111A (en) * | 1959-04-23 | 1963-01-15 | United Aircraft Corp | Rocket nozzle |
US3113429A (en) * | 1961-02-14 | 1963-12-10 | Cievite Corp | Steering and speed control for jet propelled vehicles |
US3122883A (en) * | 1959-11-20 | 1964-03-03 | Thompson Ramo Wooldridge Inc | Heat resistant wall structure for rocket motor nozzles and the like |
US3129560A (en) * | 1960-06-13 | 1964-04-21 | Stanley P Prosen | Convectively cooled rocket nozzle |
US3145529A (en) * | 1960-03-10 | 1964-08-25 | Avco Corp | Refractory composite rocket nozzle and method of making same |
US3251554A (en) * | 1962-01-29 | 1966-05-17 | Aerojet General Co | Rocket motor nozzle |
DE1218802B (de) * | 1960-05-11 | 1966-06-08 | Snecma | Rakete |
EP0242162A2 (fr) * | 1986-04-14 | 1987-10-21 | AlliedSignal Inc. | Groupe de secours pour avion |
US4811556A (en) * | 1986-10-14 | 1989-03-14 | General Electric Company | Multiple-propellant air vehicle and propulsion system |
US4817890A (en) * | 1986-10-14 | 1989-04-04 | General Electric Company | Multiple-propellant air vehicle and propulsion system |
US4835959A (en) * | 1986-10-14 | 1989-06-06 | General Electric Company | Multiple-propellant air vehicle and propulsion system |
US4840025A (en) * | 1986-10-14 | 1989-06-20 | General Electric Company | Multiple-propellant air vehicle and propulsion system |
US4841723A (en) * | 1986-10-14 | 1989-06-27 | General Electric Company | Multiple-propellant air vehicle and propulsion system |
EP0455487A1 (fr) * | 1990-05-03 | 1991-11-06 | General Electric Company | Chambre de combustion de turbine à gaz |
-
1954
- 1954-07-01 FR FR1108090D patent/FR1108090A/fr not_active Expired
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3073111A (en) * | 1959-04-23 | 1963-01-15 | United Aircraft Corp | Rocket nozzle |
US3122883A (en) * | 1959-11-20 | 1964-03-03 | Thompson Ramo Wooldridge Inc | Heat resistant wall structure for rocket motor nozzles and the like |
US3145529A (en) * | 1960-03-10 | 1964-08-25 | Avco Corp | Refractory composite rocket nozzle and method of making same |
DE1218802B (de) * | 1960-05-11 | 1966-06-08 | Snecma | Rakete |
US3129560A (en) * | 1960-06-13 | 1964-04-21 | Stanley P Prosen | Convectively cooled rocket nozzle |
US3113429A (en) * | 1961-02-14 | 1963-12-10 | Cievite Corp | Steering and speed control for jet propelled vehicles |
US3251554A (en) * | 1962-01-29 | 1966-05-17 | Aerojet General Co | Rocket motor nozzle |
EP0242162A2 (fr) * | 1986-04-14 | 1987-10-21 | AlliedSignal Inc. | Groupe de secours pour avion |
EP0242162A3 (en) * | 1986-04-14 | 1989-03-22 | The Garrett Corporation | Emergency power unit for aircraft |
US4811556A (en) * | 1986-10-14 | 1989-03-14 | General Electric Company | Multiple-propellant air vehicle and propulsion system |
US4817890A (en) * | 1986-10-14 | 1989-04-04 | General Electric Company | Multiple-propellant air vehicle and propulsion system |
US4835959A (en) * | 1986-10-14 | 1989-06-06 | General Electric Company | Multiple-propellant air vehicle and propulsion system |
US4840025A (en) * | 1986-10-14 | 1989-06-20 | General Electric Company | Multiple-propellant air vehicle and propulsion system |
US4841723A (en) * | 1986-10-14 | 1989-06-27 | General Electric Company | Multiple-propellant air vehicle and propulsion system |
EP0455487A1 (fr) * | 1990-05-03 | 1991-11-06 | General Electric Company | Chambre de combustion de turbine à gaz |
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