NO3009650T3 - - Google Patents
Info
- Publication number
- NO3009650T3 NO3009650T3 NO13891432A NO13891432A NO3009650T3 NO 3009650 T3 NO3009650 T3 NO 3009650T3 NO 13891432 A NO13891432 A NO 13891432A NO 13891432 A NO13891432 A NO 13891432A NO 3009650 T3 NO3009650 T3 NO 3009650T3
- Authority
- NO
- Norway
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
- F02K9/86—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using nozzle throats of adjustable cross- section
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/023—Aircraft characterised by the type or position of power plants of rocket type, e.g. for assisting taking-off or braking
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
-
- 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
-
- 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
- F02K9/94—Re-ignitable or restartable rocket- engine plants; Intermittently operated rocket-engine plants
-
- 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
- F05D2250/00—Geometry
- F05D2250/70—Shape
- F05D2250/75—Shape given by its similarity to a letter, e.g. T-shaped
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Lift Valve (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2013167921A JP6129682B2 (ja) | 2013-08-12 | 2013-08-12 | 推力制御バルブ及び飛翔体 |
PCT/JP2013/078381 WO2015022758A1 (ja) | 2013-08-12 | 2013-10-18 | 推力制御バルブ及び飛翔体 |
Publications (1)
Publication Number | Publication Date |
---|---|
NO3009650T3 true NO3009650T3 (ja) | 2018-08-18 |
Family
ID=52468156
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
NO13891432A NO3009650T3 (ja) | 2013-08-12 | 2013-10-18 |
Country Status (7)
Country | Link |
---|---|
US (1) | US10138844B2 (ja) |
EP (1) | EP3009650B1 (ja) |
JP (1) | JP6129682B2 (ja) |
ES (1) | ES2666669T3 (ja) |
NO (1) | NO3009650T3 (ja) |
PL (1) | PL3009650T3 (ja) |
WO (1) | WO2015022758A1 (ja) |
Family Cites Families (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3317184A (en) * | 1967-05-02 | Pintle valve and flow collimator | ||
US2583570A (en) | 1945-06-28 | 1952-01-29 | Clarence N Hickman | Nozzle for rocket motors |
FR1012021A (fr) * | 1949-05-19 | 1952-07-02 | Soc Tech De Rech Ind | Perfectionnements aux réacteurs |
US3182447A (en) * | 1957-02-27 | 1965-05-11 | Thiokol Chemical Corp | Reaction motor |
NL111420C (ja) * | 1958-12-31 | |||
US3210928A (en) * | 1960-08-19 | 1965-10-12 | Joseph J Zelinski | Fuel cooled combustor assembly |
US3302890A (en) * | 1964-07-10 | 1967-02-07 | Atlantic Res Corp | Rocket nozzle |
US3914935A (en) * | 1969-03-17 | 1975-10-28 | Rockwell International Corp | Dual area nozzle |
GB1480723A (en) * | 1971-05-06 | 1977-07-20 | Rockwell International Corp | Dual area solid propellant rocket nozzle |
US4478040A (en) * | 1982-09-28 | 1984-10-23 | Thiokol Corporation | Dual area nozzle actuating mechanical actuation system |
FR2594490B1 (fr) * | 1986-02-18 | 1989-09-15 | Aerospatiale | Dispositif pour faire varier la poussee d'un propulseur a propergol solide |
US4826104A (en) * | 1986-10-09 | 1989-05-02 | British Aerospace Public Limited Company | Thruster system |
FR2734025B1 (fr) * | 1995-05-11 | 1997-08-01 | Europ Propulsion | Moteur fusee a propergol liquide, a impulsions |
FR2740106B1 (fr) * | 1995-10-20 | 1998-01-09 | Europ Propulsion | Dispositif pour le pilotage d'engin spatial par vannage de gaz par tuyere mobile |
JP3581302B2 (ja) | 2000-07-21 | 2004-10-27 | 川崎重工業株式会社 | ガス吐出装置 |
JP3697222B2 (ja) | 2002-05-21 | 2005-09-21 | 三菱重工業株式会社 | サイドスラスタバルブ及びサイドスラスタ装置 |
US6988705B1 (en) * | 2002-09-24 | 2006-01-24 | Hoose Karl V | Fluent control valve |
JP3788973B2 (ja) * | 2003-02-19 | 2006-06-21 | 川崎重工業株式会社 | 推力制御バルブ |
US8016211B2 (en) * | 2007-03-30 | 2011-09-13 | Aerojet-General Corporation | Pintle-controlled propulsion system with external ring actuator |
FR2933745B1 (fr) * | 2008-07-11 | 2011-07-01 | Snecma | Moteur-fusee a propergol liquide avec obturateur de chambre propulsive. |
-
2013
- 2013-08-12 JP JP2013167921A patent/JP6129682B2/ja active Active
- 2013-10-18 ES ES13891432.0T patent/ES2666669T3/es active Active
- 2013-10-18 PL PL13891432T patent/PL3009650T3/pl unknown
- 2013-10-18 NO NO13891432A patent/NO3009650T3/no unknown
- 2013-10-18 WO PCT/JP2013/078381 patent/WO2015022758A1/ja active Application Filing
- 2013-10-18 US US14/908,349 patent/US10138844B2/en active Active
- 2013-10-18 EP EP13891432.0A patent/EP3009650B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
EP3009650A1 (en) | 2016-04-20 |
ES2666669T3 (es) | 2018-05-07 |
JP6129682B2 (ja) | 2017-05-17 |
EP3009650B1 (en) | 2018-03-21 |
US20160208743A1 (en) | 2016-07-21 |
US10138844B2 (en) | 2018-11-27 |
WO2015022758A1 (ja) | 2015-02-19 |
PL3009650T3 (pl) | 2018-08-31 |
JP2015036531A (ja) | 2015-02-23 |
EP3009650A4 (en) | 2016-05-25 |