ATE331882T1 - Raketenmotor - Google Patents

Raketenmotor

Info

Publication number
ATE331882T1
ATE331882T1 AT03290449T AT03290449T ATE331882T1 AT E331882 T1 ATE331882 T1 AT E331882T1 AT 03290449 T AT03290449 T AT 03290449T AT 03290449 T AT03290449 T AT 03290449T AT E331882 T1 ATE331882 T1 AT E331882T1
Authority
AT
Austria
Prior art keywords
combustion chamber
rocket motor
neck
heart
constituted
Prior art date
Application number
AT03290449T
Other languages
English (en)
Inventor
Max Calabro
Original Assignee
Mbda France
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
Application filed by Mbda France filed Critical Mbda France
Application granted granted Critical
Publication of ATE331882T1 publication Critical patent/ATE331882T1/de

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
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/62—Combustion or thrust chambers
    • F02K9/64—Combustion or thrust chambers having cooling arrangements
    • 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
    • F02K9/52—Injectors
    • 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
    • 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
    • F05D2240/10—Stators
    • F05D2240/12—Fluid guiding means, e.g. vanes
    • F05D2240/128—Nozzles
    • F05D2240/1281—Plug nozzles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Nozzles (AREA)
  • Laminated Bodies (AREA)
  • Testing Of Engines (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Toys (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Porous Artificial Stone Or Porous Ceramic Products (AREA)
  • Moulding By Coating Moulds (AREA)
AT03290449T 2002-03-04 2003-02-26 Raketenmotor ATE331882T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0202686A FR2836699B1 (fr) 2002-03-04 2002-03-04 Moteur de fusee

Publications (1)

Publication Number Publication Date
ATE331882T1 true ATE331882T1 (de) 2006-07-15

Family

ID=27741403

Family Applications (1)

Application Number Title Priority Date Filing Date
AT03290449T ATE331882T1 (de) 2002-03-04 2003-02-26 Raketenmotor

Country Status (11)

Country Link
US (1) US6915627B2 (de)
EP (1) EP1342905B1 (de)
JP (1) JP4439267B2 (de)
AT (1) ATE331882T1 (de)
AU (1) AU2003229842A1 (de)
DE (1) DE60306435T2 (de)
ES (1) ES2268291T3 (de)
FR (1) FR2836699B1 (de)
RU (1) RU2266423C2 (de)
UA (1) UA72352C2 (de)
WO (1) WO2003074859A1 (de)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6895743B1 (en) * 2003-09-05 2005-05-24 Mcelheran Terry Liquid propellant rocket motor
DE102005036137A1 (de) * 2005-07-26 2007-02-01 Deutsches Zentrum für Luft- und Raumfahrt e.V. Brennkammer und Verfahren zur Herstellung einer Brennkammer
RU2344310C2 (ru) * 2005-12-02 2009-01-20 Федеральное государственное унитарное предприятие "Научно-исследовательский институт машиностроения" (ФГУП "НИИМаш") Способ внутреннего охлаждения двухкомпонентного жидкостного ракетного двигателя малой тяги и устройство для его осуществления
RU2304727C1 (ru) * 2006-04-20 2007-08-20 Александр Федорович Чабак Двигательная установка на кислородно-водородном топливе
DE102006029586A1 (de) * 2006-06-20 2007-12-27 Deutsches Zentrum für Luft- und Raumfahrt e.V. Einblaskopf, Mischungsraum und Triebwerk
US20080264372A1 (en) * 2007-03-19 2008-10-30 Sisk David B Two-stage ignition system
US7900435B1 (en) 2007-05-23 2011-03-08 Xcor Aerospace Micro-coaxial injector for rocket engine
RU2403491C2 (ru) * 2008-03-26 2010-11-10 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" Термосиловая охлаждаемая конструкция стенки элемента высокотемпературного воздушно-газового тракта
FR2933744B1 (fr) * 2008-07-11 2011-06-03 Snecma Moteur-fusee et reacteur comportant une pluralite de tels moteurs-fusees.
RU2465482C2 (ru) * 2010-06-28 2012-10-27 Федеральное государственное унитарное предприятие "Научно-исследовательский институт машиностроения" (ФГУП "НИИМаш") Камера жидкостного ракетного двигателя малой тяги
RU2472962C2 (ru) * 2011-02-11 2013-01-20 Открытое акционерное общество "Конструкторское бюро химавтоматики" Жидкостный ракетный двигатель и способ охлаждения теплонапряженных участков его камеры
FR2987081B1 (fr) * 2012-02-21 2017-03-31 Snecma Ensemble et procede propulsifs
GB2518211B (en) * 2013-09-13 2015-11-18 Carolyn Billie Knight Rocket motor with combustion chamber having porous membrane
RU2581756C2 (ru) * 2013-12-17 2016-04-20 Федеральное государственное унитарное предприятие "Научно-исследовательский институт машиностроения" (ФГУП "НИИМаш") Камера жидкостного ракетного двигателя малой тяги
PT3129709T (pt) * 2014-04-09 2019-02-06 Avio Spa Câmara de combustão de um motor propulsor líquido
FR3026675B1 (fr) * 2014-10-02 2016-11-11 Mbda France Procede pour la realisation d'une piece monolithique composite thermostructurale a double paroi et piece obtenue
DE102017106758A1 (de) 2017-03-15 2018-09-20 Deutsches Zentrum für Luft- und Raumfahrt e.V. Schubkammervorrichtung und Verfahren zum Betreiben einer Schubkammervorrichtung
US11629669B1 (en) * 2019-05-31 2023-04-18 Exquadrum, Inc. Liquid monopropellant controlled solid rocket motor with aft end injection deflector
JP7767670B1 (ja) * 2025-05-29 2025-11-11 櫻護謨株式会社 燃焼器

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US3151546A (en) * 1964-10-06 Calculating machine
US3069847A (en) * 1959-12-10 1962-12-25 United Aircraft Corp Rocket wall construction
US3151446A (en) * 1959-12-15 1964-10-06 Arthur R Parilla Propulsion devices
US3307359A (en) * 1963-06-26 1967-03-07 North American Aviation Inc Turbopump assembly
US4245469A (en) * 1979-04-23 1981-01-20 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Heat exchanger and method of making
JPS58214652A (ja) * 1982-06-08 1983-12-13 Natl Aerospace Lab 複合冷却ロケツト燃焼器
JPS6210264U (de) * 1985-07-02 1987-01-22
FR2610044A1 (fr) * 1986-10-14 1988-07-29 Gen Electric Systeme de propulsion comportant une garniture perfectionnee de la chambre de combustion et procede de fabrication d'une telle fabrication
US4840025A (en) * 1986-10-14 1989-06-20 General Electric Company Multiple-propellant air vehicle and propulsion system
FR2647533B1 (fr) * 1989-05-29 1993-03-19 Europ Propulsion Chambre de statoreacteur a combustion supersonique
FR2652615B1 (fr) * 1989-10-04 1992-02-07 Europ Propulsion Chambre de combustion de propulseur.
FR2685655B1 (fr) 1991-12-31 1995-08-18 Europ Propulsion Procede de formation d'un passage etanche dans une piece en materiau composite refractaire, et application a la realisation d'une structure composite refractaire refroidie par circulation de fluide.
FR2691209B1 (fr) * 1992-05-18 1995-09-01 Europ Propulsion Enceinte contenant des gaz chauds refroidie par transpiration, notamment chambre propulsive de moteur-fusee, et procede de fabrication.
FR2699963B1 (fr) * 1992-12-24 1995-03-17 Europ Propulsion Générateur de gaz à combustion rapprochée.
RU2079684C1 (ru) * 1994-07-25 1997-05-20 Малое инновационное предприятие Научно-исследовательского института тепловых процессов "Теплоэн" Парогенератор
FR2733581B1 (fr) * 1995-04-27 1997-07-18 Europ Propulsion Enceinte de combustion avec refroidissement par transpiration
US5582895A (en) * 1995-07-19 1996-12-10 Gencorp Inc. Integrally molded greenhouse trim
US6418973B1 (en) * 1996-10-24 2002-07-16 Boeing North American, Inc. Integrally woven ceramic composites
RU2124639C1 (ru) * 1996-11-12 1999-01-10 Бобров Анатолий Васильевич Устройство для защиты поверхностей от горячих газов или плазмы с помощью жидкости и ее пара
DE19730674A1 (de) * 1997-07-17 1999-01-21 Deutsch Zentr Luft & Raumfahrt Brennkammer und Verfahren zur Herstellung einer Brennkammer
DE19801407C2 (de) * 1998-01-16 1999-12-02 Daimler Chrysler Ag Brennkammer für Hochleistungstriebwerke und Düsen
DE19804232C2 (de) * 1998-02-04 2000-06-29 Daimler Chrysler Ag Brennkammer für Hochleistungstriebwerke und Düsen
DE19901422C2 (de) * 1999-01-18 2000-11-16 Daimler Chrysler Ag Brennkammer-Kühlstruktur für ein Raketentriebwerk
RU2219363C2 (ru) * 1999-03-22 2003-12-20 Государственное предприятие Научно-исследовательский институт машиностроения Камера жидкостного ракетного двигателя малой тяги
US6601380B2 (en) * 1999-03-24 2003-08-05 Orbital Technologies Corporation Hybrid rocket engine and method of propelling a rocket
DE19915082C1 (de) * 1999-04-01 2000-07-13 Daimler Chrysler Ag Verfahren zur Herstellung einer gekühlten Düse für ein Raketentriebwerk
RU2204732C2 (ru) * 2000-02-15 2003-05-20 ОАО "Самарский научно-технический комплекс им. Н.Д. Кузнецова" Газогенератор жидкостного ракетного двигателя

Also Published As

Publication number Publication date
RU2003135210A (ru) 2005-05-20
JP4439267B2 (ja) 2010-03-24
AU2003229842A1 (en) 2003-09-16
JP2005519221A (ja) 2005-06-30
ES2268291T3 (es) 2007-03-16
WO2003074859A1 (fr) 2003-09-12
FR2836699B1 (fr) 2005-02-11
FR2836699A1 (fr) 2003-09-05
US6915627B2 (en) 2005-07-12
UA72352C2 (uk) 2005-02-15
DE60306435T2 (de) 2007-06-21
EP1342905B1 (de) 2006-06-28
DE60306435D1 (de) 2006-08-10
RU2266423C2 (ru) 2005-12-20
EP1342905A1 (de) 2003-09-10
US20040128980A1 (en) 2004-07-08

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