AU2003304089A1 - Multi-nozzle grid missile propulsion system - Google Patents
Multi-nozzle grid missile propulsion systemInfo
- Publication number
- AU2003304089A1 AU2003304089A1 AU2003304089A AU2003304089A AU2003304089A1 AU 2003304089 A1 AU2003304089 A1 AU 2003304089A1 AU 2003304089 A AU2003304089 A AU 2003304089A AU 2003304089 A AU2003304089 A AU 2003304089A AU 2003304089 A1 AU2003304089 A1 AU 2003304089A1
- Authority
- AU
- Australia
- Prior art keywords
- propulsion system
- nozzle grid
- missile propulsion
- missile
- grid
- 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.)
- Abandoned
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
- F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
- F02K9/30—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants with the propulsion gases exhausting through a plurality of 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
- F02K9/97—Rocket nozzles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
- F42B15/10—Missiles having a trajectory only in the air
-
- 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
- F05D2240/00—Components
- F05D2240/40—Use of a multiplicity of similar components
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/20—Oxide or non-oxide ceramics
- F05D2300/21—Oxide ceramics
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/20—Oxide or non-oxide ceramics
- F05D2300/22—Non-oxide ceramics
- F05D2300/224—Carbon, e.g. graphite
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/603—Composites; e.g. fibre-reinforced
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/614—Fibres or filaments
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Testing Of Engines (AREA)
- Nozzles (AREA)
Applications Claiming Priority (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US42366802P | 2002-11-04 | 2002-11-04 | |
US60/423,668 | 2002-11-04 | ||
US10/288,943 | 2002-11-06 | ||
US10/288,943 US20040084566A1 (en) | 2002-11-06 | 2002-11-06 | Multi-nozzle grid missile propulsion system |
PCT/US2003/035150 WO2004099601A2 (en) | 2002-11-04 | 2003-11-04 | Multi-nozzle grid missile propulsion system |
Publications (2)
Publication Number | Publication Date |
---|---|
AU2003304089A8 AU2003304089A8 (en) | 2004-11-26 |
AU2003304089A1 true AU2003304089A1 (en) | 2004-11-26 |
Family
ID=33436634
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AU2003304089A Abandoned AU2003304089A1 (en) | 2002-11-04 | 2003-11-04 | Multi-nozzle grid missile propulsion system |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP1576334A2 (en) |
JP (1) | JP2006513362A (en) |
AU (1) | AU2003304089A1 (en) |
WO (1) | WO2004099601A2 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7856806B1 (en) | 2006-11-06 | 2010-12-28 | Raytheon Company | Propulsion system with canted multinozzle grid |
DE102014011101A1 (en) * | 2014-07-24 | 2016-01-28 | Astrium Gmbh | Injection element for a rocket combustion chamber |
US10378483B2 (en) | 2015-11-12 | 2019-08-13 | Raytheon Company | Aerospike rocket motor assembly |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3046736A (en) * | 1958-02-10 | 1962-07-31 | Thompson Ramo Wooldridge Inc | Direction control for gelatin monopropellant rocket engine |
US4023749A (en) * | 1975-12-08 | 1977-05-17 | The United States Of America As Represented By The Secretary Of The Army | Directional control system for artillery missiles |
US4432512A (en) * | 1978-08-31 | 1984-02-21 | British Aerospace Public Limited Company | Jet propulsion efflux outlets |
EP0228781B1 (en) * | 1985-10-31 | 1992-08-05 | British Aerospace Public Limited Company | Missile expulsion motor |
US4826104A (en) * | 1986-10-09 | 1989-05-02 | British Aerospace Public Limited Company | Thruster system |
US5343698A (en) * | 1993-04-28 | 1994-09-06 | United Technologies Corporation | Hexagonal cluster nozzle for a rocket engine |
-
2003
- 2003-11-04 AU AU2003304089A patent/AU2003304089A1/en not_active Abandoned
- 2003-11-04 JP JP2004571715A patent/JP2006513362A/en active Pending
- 2003-11-04 WO PCT/US2003/035150 patent/WO2004099601A2/en not_active Application Discontinuation
- 2003-11-04 EP EP03816221A patent/EP1576334A2/en not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
AU2003304089A8 (en) | 2004-11-26 |
EP1576334A2 (en) | 2005-09-21 |
JP2006513362A (en) | 2006-04-20 |
WO2004099601A3 (en) | 2005-02-10 |
WO2004099601A2 (en) | 2004-11-18 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
MK6 | Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase |