FR2732409B1 - Dispositif pour controler la direction de la poussee d'un moteur-fusee - Google Patents
Dispositif pour controler la direction de la poussee d'un moteur-fuseeInfo
- Publication number
- FR2732409B1 FR2732409B1 FR9604010A FR9604010A FR2732409B1 FR 2732409 B1 FR2732409 B1 FR 2732409B1 FR 9604010 A FR9604010 A FR 9604010A FR 9604010 A FR9604010 A FR 9604010A FR 2732409 B1 FR2732409 B1 FR 2732409B1
- Authority
- FR
- France
- Prior art keywords
- push
- controlling
- rocket motor
- rocket
- motor
- 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 - Fee Related
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
- F02K9/90—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using deflectors
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Thermal Insulation (AREA)
- Supercharger (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP07659095A JP3710099B2 (ja) | 1995-03-31 | 1995-03-31 | ジェッタベータ |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2732409A1 FR2732409A1 (fr) | 1996-10-04 |
FR2732409B1 true FR2732409B1 (fr) | 1998-05-22 |
Family
ID=13609531
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR9604010A Expired - Fee Related FR2732409B1 (fr) | 1995-03-31 | 1996-03-29 | Dispositif pour controler la direction de la poussee d'un moteur-fusee |
Country Status (4)
Country | Link |
---|---|
US (1) | US5735463A (fr) |
JP (1) | JP3710099B2 (fr) |
FR (1) | FR2732409B1 (fr) |
GB (1) | GB2299558B (fr) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6823677B2 (en) * | 2002-09-03 | 2004-11-30 | Pratt & Whitney Canada Corp. | Stress relief feature for aerated gas turbine fuel injector |
US20080120931A1 (en) * | 2006-06-30 | 2008-05-29 | Mark Joslyn | Masonry block arrangements; wall units; and, methods |
JP6603313B2 (ja) * | 2014-10-01 | 2019-11-06 | キューエスエー グローバル インコーポレイティド | γ線ラジオグラフィー用の保護装置 |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB807011A (en) * | 1954-02-01 | 1959-01-07 | Harrison Caleb Whittleman | Improvements in or relating to liquid fuel burners or atomisers |
FR1112699A (fr) * | 1954-06-03 | 1956-03-16 | Snecma | Perfectionnements aux chambres de combustion et tuyères, en particulier à celles des fusées |
FR1112030A (fr) * | 1954-06-03 | 1956-03-07 | Snecma | Chambre de combustion, tuyère et plus particulièrement fusée |
US2900789A (en) * | 1954-11-26 | 1959-08-25 | Philpot Peter De Buriatte | Discharge nozzles for propulsive jets |
GB916692A (en) * | 1958-06-19 | 1963-01-23 | Snecma | Improvements in jet control apparatus |
US3182452A (en) * | 1959-04-15 | 1965-05-11 | Bendix Corp | Movable thrust nozzle and sealing means therefor |
FR1246339A (fr) * | 1959-10-09 | 1960-11-18 | Soc Et Propulsion Par Reaction | Tuyère d'éjection orientable |
US3291397A (en) * | 1963-02-11 | 1966-12-13 | Gen Motors Corp | Rocket nozzle liner ring mounting |
US3224193A (en) * | 1963-06-25 | 1965-12-21 | Curtiss Wright Corp | Anisotropic heat shield construction |
GB1248573A (en) * | 1967-10-18 | 1971-10-06 | Rolls Royce | Jet propulsion thrust-producing means having a nozzle mounted for swivelling |
GB1189052A (en) * | 1968-01-09 | 1970-04-22 | Lockheed Aircraft Corp | Flexible Joint Means |
GB1291586A (en) * | 1969-10-23 | 1972-10-04 | Rolls Royce | Propulsive jet nozzle assembly |
FR2165695B1 (fr) * | 1970-04-30 | 1976-02-06 | Hawker Siddeley Dynamics Gb | |
GB1334592A (en) * | 1971-01-21 | 1973-10-24 | Imp Metal Ind Kynoch Ltd | Flexible duct assemblies |
US3972475A (en) * | 1975-07-31 | 1976-08-03 | United Technologies Corporation | Nozzle construction providing for thermal growth |
US4649701A (en) * | 1986-02-11 | 1987-03-17 | The United States Of America As Represented By The Secretary Of The Navy | Thrust nozzle with insulation |
JP2998409B2 (ja) * | 1992-03-30 | 2000-01-11 | 日産自動車株式会社 | ロケットノズル |
US5392596A (en) * | 1993-12-21 | 1995-02-28 | Solar Turbines Incorporated | Combustor assembly construction |
-
1995
- 1995-03-31 JP JP07659095A patent/JP3710099B2/ja not_active Expired - Fee Related
-
1996
- 1996-03-21 US US08/620,691 patent/US5735463A/en not_active Expired - Fee Related
- 1996-03-22 GB GB9606057A patent/GB2299558B/en not_active Expired - Fee Related
- 1996-03-29 FR FR9604010A patent/FR2732409B1/fr not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
GB9606057D0 (en) | 1996-05-22 |
GB2299558A (en) | 1996-10-09 |
JP3710099B2 (ja) | 2005-10-26 |
GB2299558B (en) | 1997-06-04 |
JPH08270507A (ja) | 1996-10-15 |
FR2732409A1 (fr) | 1996-10-04 |
US5735463A (en) | 1998-04-07 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
TP | Transmission of property | ||
ST | Notification of lapse |
Effective date: 20121130 |