FR2861810B1 - Tete d'injection pour moteur-fusee a propergol liquide - Google Patents

Tete d'injection pour moteur-fusee a propergol liquide

Info

Publication number
FR2861810B1
FR2861810B1 FR0411839A FR0411839A FR2861810B1 FR 2861810 B1 FR2861810 B1 FR 2861810B1 FR 0411839 A FR0411839 A FR 0411839A FR 0411839 A FR0411839 A FR 0411839A FR 2861810 B1 FR2861810 B1 FR 2861810B1
Authority
FR
France
Prior art keywords
propergol
liquid
injection head
rocket engine
rocket
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.)
Active
Application number
FR0411839A
Other languages
English (en)
Other versions
FR2861810A1 (fr
Inventor
Wolfgang Muller
Christoph Tscherwitschke
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.)
EADS Space Transportation GmbH
Original Assignee
EADS Space Transportation GmbH
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 EADS Space Transportation GmbH filed Critical EADS Space Transportation GmbH
Publication of FR2861810A1 publication Critical patent/FR2861810A1/fr
Application granted granted Critical
Publication of FR2861810B1 publication Critical patent/FR2861810B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F02K9/44—Feeding propellants
    • F02K9/52—Injectors
FR0411839A 2003-11-05 2004-11-05 Tete d'injection pour moteur-fusee a propergol liquide Active FR2861810B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE10351715A DE10351715B4 (de) 2003-11-05 2003-11-05 Einspritzkopf für ein Flüssigkeitsraketentriebwerk

Publications (2)

Publication Number Publication Date
FR2861810A1 FR2861810A1 (fr) 2005-05-06
FR2861810B1 true FR2861810B1 (fr) 2006-01-27

Family

ID=34428574

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0411839A Active FR2861810B1 (fr) 2003-11-05 2004-11-05 Tete d'injection pour moteur-fusee a propergol liquide

Country Status (3)

Country Link
US (1) US7293402B2 (fr)
DE (1) DE10351715B4 (fr)
FR (1) FR2861810B1 (fr)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102005024608B4 (de) * 2005-05-25 2009-05-07 Astrium Gmbh Einspritzvorrichtung für Brennkammern von Flüssigkeitsraketentriebwerken
US20080264372A1 (en) * 2007-03-19 2008-10-30 Sisk David B Two-stage ignition system
EP2613887A4 (fr) * 2010-09-09 2014-09-17 Wells Gelven Fractal Technology Llc Plaque à orifices fractaux
RU2560117C1 (ru) * 2014-02-14 2015-08-20 Федеральное государственное унитарное предприятие "Государственный космический научно-производственный центр имени М.В. Хруничева" (ФГУП "ГКНПЦ им. М.В. Хруничева") Способ изготовления смесительной головки камеры сгорания жидкостного ракетного двигателя (жрд)
RU2680281C1 (ru) * 2018-06-04 2019-02-19 Владислав Юрьевич Климов Смесительная головка газогенератора
RU2684701C1 (ru) * 2018-07-23 2019-04-11 Владислав Юрьевич Климов Смесительная головка камеры сгорания жрд
RU2698171C1 (ru) * 2018-12-06 2019-08-22 Владимир Викторович Черниченко Смесительная головка камеры жидкостного ракетного двигателя
RU2725397C1 (ru) * 2019-08-28 2020-07-02 Акционерное общество "Конструкторское бюро химавтоматики" Щелевая смесительная головка камеры жидкостного ракетного двигателя

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3071925A (en) * 1959-06-23 1963-01-08 United Aircraft Corp Injector head for liquid rocket
US3132481A (en) * 1959-06-23 1964-05-12 United Aircraft Corp Injector head for liquid rocket
US3122885A (en) * 1961-06-19 1964-03-03 Marcus F Heidmann Injector for bipropellant rocket engines
US3625435A (en) * 1967-02-14 1971-12-07 United Aircraft Corp Dual orifice quadruplet impingement injector
US3603092A (en) * 1969-09-24 1971-09-07 Nasa Injection head for delivering liquid fuel and oxidizers
US4586226A (en) * 1983-09-30 1986-05-06 Rockwell International Corporation Method for fabricating a small-orifice fuel injector
US4650416A (en) * 1985-11-08 1987-03-17 The United States Of America As Represented By The Secretary Of The Air Force NF3 combustor for cylindrical laser
DE3818623C1 (fr) * 1988-06-01 1989-07-13 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De
US5161379A (en) * 1991-12-23 1992-11-10 United Technologies Corporation Combustor injector face plate cooling scheme
US6253539B1 (en) * 1996-09-24 2001-07-03 Boeing North America Inc. Convective and turbulent shear mixing injector

Also Published As

Publication number Publication date
US20060090453A1 (en) 2006-05-04
US7293402B2 (en) 2007-11-13
DE10351715B4 (de) 2005-09-29
DE10351715A1 (de) 2005-06-16
FR2861810A1 (fr) 2005-05-06

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