FR2698914B1 - Moteur-fusée à ergols liquides à flux dérivé et générateur de gaz intégré. - Google Patents

Moteur-fusée à ergols liquides à flux dérivé et générateur de gaz intégré.

Info

Publication number
FR2698914B1
FR2698914B1 FR9214852A FR9214852A FR2698914B1 FR 2698914 B1 FR2698914 B1 FR 2698914B1 FR 9214852 A FR9214852 A FR 9214852A FR 9214852 A FR9214852 A FR 9214852A FR 2698914 B1 FR2698914 B1 FR 2698914B1
Authority
FR
France
Prior art keywords
gas generator
rocket motor
integrated gas
liquid propellants
derivative flow
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.)
Expired - Fee Related
Application number
FR9214852A
Other languages
English (en)
Other versions
FR2698914A1 (fr
Inventor
Didier Vuillamy
Pierre Desclos
Andre Beaurain
Jean-Paul Dumont
Pierre-Andre Baudart
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.)
Societe Europeenne de Propulsion SEP SA
Original Assignee
Societe Europeenne de Propulsion SEP SA
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 Societe Europeenne de Propulsion SEP SA filed Critical Societe Europeenne de Propulsion SEP SA
Priority to FR9214852A priority Critical patent/FR2698914B1/fr
Priority to DE4341376A priority patent/DE4341376B4/de
Priority to US08/163,713 priority patent/US5404715A/en
Priority to JP30895593A priority patent/JP3310078B2/ja
Publication of FR2698914A1 publication Critical patent/FR2698914A1/fr
Application granted granted Critical
Publication of FR2698914B1 publication Critical patent/FR2698914B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44—Feeding propellants
    • F02K9/46—Feeding propellants using pumps
    • F02K9/48—Feeding propellants using pumps driven by a gas turbine fed by propellant combustion gases or fed by vaporized propellants or other gases
    • 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
    • F02K9/42—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
FR9214852A 1992-12-09 1992-12-09 Moteur-fusée à ergols liquides à flux dérivé et générateur de gaz intégré. Expired - Fee Related FR2698914B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR9214852A FR2698914B1 (fr) 1992-12-09 1992-12-09 Moteur-fusée à ergols liquides à flux dérivé et générateur de gaz intégré.
DE4341376A DE4341376B4 (de) 1992-12-09 1993-12-04 Raketenmotor
US08/163,713 US5404715A (en) 1992-12-09 1993-12-09 Liquid propellant rocket engine with parallel auxiliary flow, and an integrated gas generator
JP30895593A JP3310078B2 (ja) 1992-12-09 1993-12-09 平行補助流を有する液体推進燃料ロケットエンジンおよび統合されたガス発生機

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9214852A FR2698914B1 (fr) 1992-12-09 1992-12-09 Moteur-fusée à ergols liquides à flux dérivé et générateur de gaz intégré.

Publications (2)

Publication Number Publication Date
FR2698914A1 FR2698914A1 (fr) 1994-06-10
FR2698914B1 true FR2698914B1 (fr) 1995-03-03

Family

ID=9436399

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9214852A Expired - Fee Related FR2698914B1 (fr) 1992-12-09 1992-12-09 Moteur-fusée à ergols liquides à flux dérivé et générateur de gaz intégré.

Country Status (4)

Country Link
US (1) US5404715A (fr)
JP (1) JP3310078B2 (fr)
DE (1) DE4341376B4 (fr)
FR (1) FR2698914B1 (fr)

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US7124574B2 (en) * 2002-12-04 2006-10-24 United Technologies Corporation Method and apparatus for a substantially coaxial injector element
US6860099B1 (en) * 2003-01-09 2005-03-01 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Liquid propellant tracing impingement injector
US6832471B2 (en) * 2003-03-12 2004-12-21 Aerojet-General Corporation Expander cycle rocket engine with staged combustion and heat exchange
US6918243B2 (en) * 2003-05-19 2005-07-19 The Boeing Company Bi-propellant injector with flame-holding zone igniter
DE10353423B3 (de) * 2003-11-15 2005-04-14 Eads Space Transportation Gmbh Einspritzelement
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DE102004018725B4 (de) * 2004-04-17 2015-02-12 Astrium Gmbh Dämpfung von Schwingungen einer Brennkammer durch Resonatoren
JP4100518B2 (ja) * 2005-04-18 2008-06-11 独立行政法人 宇宙航空研究開発機構 ピントル噴射器
US8122703B2 (en) 2006-04-28 2012-02-28 United Technologies Corporation Coaxial ignition assembly
US20100326043A1 (en) * 2007-01-31 2010-12-30 Florida Turbine Technologies, Inc. Expander cycle rocket engine nozzle
US20080264035A1 (en) * 2007-04-25 2008-10-30 Ricciardo Mark J Coolant flow swirler for a rocket engine
JP5481978B2 (ja) * 2009-07-10 2014-04-23 株式会社Ｉｈｉ ロケットエンジン
JP2012189014A (ja) * 2011-03-11 2012-10-04 Ihi Aerospace Co Ltd ガス発生器
JP2012189018A (ja) * 2011-03-11 2012-10-04 Ihi Aerospace Co Ltd ガス発生器用の燃料／酸化剤供給装置
RU2445494C1 (ru) * 2011-03-24 2012-03-20 Владимир Викторович Черниченко Камера жидкостного ракетного двигателя
RU2445496C1 (ru) * 2011-03-24 2012-03-20 Владимир Викторович Черниченко Жидкостный ракетный двигатель
RU2445498C1 (ru) * 2011-03-24 2012-03-20 Владимир Викторович Черниченко Жидкостный ракетный двигатель
RU2488517C1 (ru) * 2012-03-23 2013-07-27 Николай Борисович Болотин Атомная подводная лодка и жидкостный ракетный двигатель морского исполнения
RU2494004C1 (ru) * 2012-03-29 2013-09-27 Николай Борисович Болотин Атомная подводная лодка
RU2493410C1 (ru) * 2012-06-27 2013-09-20 Владимир Викторович Черниченко Жидкостный ракетный двигатель
RU2490503C1 (ru) * 2012-06-27 2013-08-20 Владимир Викторович Черниченко Жидкостный ракетный двигатель
RU2490505C1 (ru) * 2012-06-27 2013-08-20 Владимир Викторович Черниченко Камера жидкостного ракетного двигателя
RU2490507C1 (ru) * 2012-06-27 2013-08-20 Владимир Викторович Черниченко Жидкостный ракетный двигатель
RU2493411C1 (ru) * 2012-06-27 2013-09-20 Владимир Викторович Черниченко Жидкостный ракетный двигатель
RU2493412C1 (ru) * 2012-06-27 2013-09-20 Владимир Викторович Черниченко Жидкостный ракетный двигатель
RU2493409C1 (ru) * 2012-06-27 2013-09-20 Владимир Викторович Черниченко Камера жидкостного ракетного двигателя
RU2496021C1 (ru) * 2012-06-27 2013-10-20 Владимир Викторович Черниченко Жидкостный ракетный двигатель
RU2497012C1 (ru) * 2012-06-27 2013-10-27 Владимир Викторович Черниченко Камера жидкостного ракетного двигателя
RU2490506C1 (ru) * 2012-06-27 2013-08-20 Владимир Викторович Черниченко Жидкостный ракетный двигатель
RU2494274C1 (ru) * 2012-06-27 2013-09-27 Владимир Викторович Черниченко Жидкостный ракетный двигатель
US9777674B2 (en) * 2014-02-26 2017-10-03 Deepak Atyam Injector plate for a rocket engine
CN103775246B (zh) * 2014-03-03 2015-08-05 葛明龙 过氧化氢/液氢气体发生器和推力室
DE102015001271A1 (de) * 2015-02-04 2016-08-04 Airbus Ds Gmbh Turbopumpe für ein Raketentriebwerk mit einer Radialstufe
CN106939850B (zh) * 2017-03-09 2018-10-30 上海空间推进研究所 单组元发动机用防回火喷注装置
CN106837608A (zh) * 2017-04-01 2017-06-13 北京航空航天大学 一种分段装药端燃变推力固液火箭发动机结构
CN107178437B (zh) * 2017-06-05 2019-01-08 上海空间推进研究所 微型气和气双组元推进剂的燃烧器
WO2018227317A1 (fr) * 2017-06-15 2018-12-20 葛明龙 Chambre de poussée de fusée super-grande et grande pour l'exploration lunaire par l'homme ou l'exploration de mars
FR3071554B1 (fr) * 2017-09-27 2022-04-15 Arianegroup Sas Paroi d'injection pour une chambre de combustion de moteur-fusee
RU2703889C1 (ru) * 2018-08-09 2019-10-22 Акционерное общество "Конструкторское бюро химавтоматики" Смесительная головка камеры сгорания жрд
US11661907B2 (en) 2018-10-11 2023-05-30 Sierra Space Corporation Vortex hybrid rocket motor
CN109630318B (zh) * 2018-10-23 2019-12-27 陕西蓝箭航天技术有限公司 用于液体发动机的喷注器及液体发动机
US11378040B2 (en) * 2018-11-15 2022-07-05 Stratolaunch, Llc Swirl preburner system and method
US20210148307A1 (en) 2019-01-30 2021-05-20 Laboratoire Reaction Dynamics Inc. Rocket engine with integrated oxidizer catalyst in manifold and injector assembly
US11572851B2 (en) 2019-06-21 2023-02-07 Sierra Space Corporation Reaction control vortex thruster system
CN113389658B (zh) * 2021-07-21 2022-08-26 北京航空航天大学 针栓式自适应变推力固液火箭发动机头部结构
US11952967B2 (en) 2021-08-19 2024-04-09 Sierra Space Corporation Liquid propellant injector for vortex hybrid rocket motor
US11879414B2 (en) 2022-04-12 2024-01-23 Sierra Space Corporation Hybrid rocket oxidizer flow control system including regression rate sensors
WO2023221250A1 (fr) * 2022-05-18 2023-11-23 卢驭龙 Moteur de fusée à propergol liquide coaxial utilisant un cycle de combustion étagée à flux complet
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Also Published As

Publication number Publication date
DE4341376B4 (de) 2004-06-17
FR2698914A1 (fr) 1994-06-10
US5404715A (en) 1995-04-11
DE4341376A1 (de) 1994-06-16
JP3310078B2 (ja) 2002-07-29
JPH06213076A (ja) 1994-08-02

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Legal Events

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TP Transmission of property
CD Change of name or company name
TP Transmission of property
CD Change of name or company name
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Effective date: 20090831