FR2197118B1 - - Google Patents
Info
- Publication number
- FR2197118B1 FR2197118B1 FR7330512A FR7330512A FR2197118B1 FR 2197118 B1 FR2197118 B1 FR 2197118B1 FR 7330512 A FR7330512 A FR 7330512A FR 7330512 A FR7330512 A FR 7330512A FR 2197118 B1 FR2197118 B1 FR 2197118B1
- Authority
- FR
- France
- 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
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/44—Feeding 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
- F02K9/60—Constructional parts; Details not otherwise provided for
- F02K9/68—Decomposition chambers
-
- 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
- F02K9/88—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using auxiliary rocket nozzles
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19722241424 DE2241424C3 (de) | 1972-08-23 | 1972-08-23 | Verfahren zum Betreiben eines Flüssigkeitsraketentriebwerkes |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2197118A1 FR2197118A1 (US20070167544A1-20070719-C00007.png) | 1974-03-22 |
| FR2197118B1 true FR2197118B1 (US20070167544A1-20070719-C00007.png) | 1978-01-06 |
Family
ID=5854307
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR7330512A Expired FR2197118B1 (US20070167544A1-20070719-C00007.png) | 1972-08-23 | 1973-08-22 |
Country Status (3)
| Country | Link |
|---|---|
| DE (1) | DE2241424C3 (US20070167544A1-20070719-C00007.png) |
| FR (1) | FR2197118B1 (US20070167544A1-20070719-C00007.png) |
| GB (1) | GB1439368A (US20070167544A1-20070719-C00007.png) |
Families Citing this family (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB8609228D0 (en) * | 1986-04-16 | 1986-05-21 | Marconi Co Ltd | Thrusters |
| GB8610849D0 (en) * | 1986-05-02 | 1986-08-20 | Marconi Co Ltd | Gas thruster |
| WO1987007877A1 (en) * | 1986-06-19 | 1987-12-30 | Hughes Aircraft Company | Hybrid spacecraft control system |
| US5263666A (en) * | 1988-12-16 | 1993-11-23 | General Electric Co. | Spacecraft with increased stationkeeping fuel load |
| US5282357A (en) * | 1990-04-19 | 1994-02-01 | Trw Inc. | High-performance dual-mode integral propulsion system |
| US5417049A (en) * | 1990-04-19 | 1995-05-23 | Trw Inc. | Satellite propulsion and power system |
| FR2697587B1 (fr) * | 1992-11-04 | 1995-01-20 | Europ Propulsion | Système optimisé d'alimentation de moteur fusée réallumable. |
| US6135393A (en) * | 1997-11-25 | 2000-10-24 | Trw Inc. | Spacecraft attitude and velocity control thruster system |
| DE60005497T2 (de) * | 1999-03-26 | 2004-05-06 | Alliant Techsystems Inc., Hopkins | Hybrid-raketenantrieb mit einer anordnung von zusatzraketenmotoren zur positionskontrolle |
| EP1172545B1 (de) * | 2000-07-15 | 2013-05-29 | Astrium GmbH | Zündsystem für Brennkammern in Raketentriebwerken |
| FR2828524B1 (fr) * | 2001-08-07 | 2003-10-31 | Air Liquide | Systeme propulsif annexe d'etage cryotechnique de lanceur et etage de lanceur comprenant un tel systeme |
| DE102005005156B4 (de) * | 2005-02-04 | 2007-06-06 | Astrium Gmbh | Triebwerk |
| CN107701330B (zh) * | 2017-09-14 | 2019-08-09 | 北京控制工程研究所 | 一种不基于气体旁路的系统混合比主动控制方法 |
-
1972
- 1972-08-23 DE DE19722241424 patent/DE2241424C3/de not_active Expired
-
1973
- 1973-07-09 GB GB3257873A patent/GB1439368A/en not_active Expired
- 1973-08-22 FR FR7330512A patent/FR2197118B1/fr not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| GB1439368A (en) | 1976-06-16 |
| DE2241424C3 (de) | 1978-06-22 |
| FR2197118A1 (US20070167544A1-20070719-C00007.png) | 1974-03-22 |
| DE2241424A1 (de) | 1974-03-07 |
| DE2241424B2 (de) | 1977-10-06 |
Similar Documents
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| ST | Notification of lapse |