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AU2003304089A1 - Multi-nozzle grid missile propulsion system - Google Patents

Multi-nozzle grid missile propulsion system

Info

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
Application number
AU2003304089A
Other versions
AU2003304089A8 (en
Inventor
Daniel Chasman
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Priority claimed from US10/288,943 external-priority patent/US20040084566A1/en
Application filed by Individual filed Critical Individual
Publication of AU2003304089A8 publication Critical patent/AU2003304089A8/en
Publication of AU2003304089A1 publication Critical patent/AU2003304089A1/en
Abandoned legal-status Critical Current

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)
AU2003304089A 2002-11-04 2003-11-04 Multi-nozzle grid missile propulsion system Abandoned AU2003304089A1 (en)

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 US20040084566A1 (en) 2002-11-06 2002-11-06 Multi-nozzle grid missile propulsion system
US10/288,943 2002-11-06
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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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
DE3686321T2 (en) * 1985-10-31 1992-12-17 British Aerospace EXHAUST DRIVE FOR AIRCRAFT.
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

Also Published As

Publication number Publication date
AU2003304089A8 (en) 2004-11-26
JP2006513362A (en) 2006-04-20
WO2004099601A3 (en) 2005-02-10
WO2004099601A2 (en) 2004-11-18
EP1576334A2 (en) 2005-09-21

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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