JPS6053650A - バイパス型ロケツトエンジンの運転方法およびこの方法を実施するためのバイパス型ロケツトエンジン - Google Patents

バイパス型ロケツトエンジンの運転方法およびこの方法を実施するためのバイパス型ロケツトエンジン

Info

Publication number
JPS6053650A
JPS6053650A JP16298784A JP16298784A JPS6053650A JP S6053650 A JPS6053650 A JP S6053650A JP 16298784 A JP16298784 A JP 16298784A JP 16298784 A JP16298784 A JP 16298784A JP S6053650 A JPS6053650 A JP S6053650A
Authority
JP
Japan
Prior art keywords
combustion chamber
oxygen
hydrogen
operating
main combustion
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.)
Granted
Application number
JP16298784A
Other languages
English (en)
Japanese (ja)
Other versions
JPH0370108B2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html
Inventor
ギユンテル・シユミツト
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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of JPS6053650A publication Critical patent/JPS6053650A/ja
Publication of JPH0370108B2 publication Critical patent/JPH0370108B2/ja
Granted 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
    • F02K9/56—Control
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Engines (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Transition And Organic Metals Composition Catalysts For Addition Polymerization (AREA)
  • Developing Agents For Electrophotography (AREA)
  • Medicines Containing Antibodies Or Antigens For Use As Internal Diagnostic Agents (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
JP16298784A 1983-08-04 1984-08-03 バイパス型ロケツトエンジンの運転方法およびこの方法を実施するためのバイパス型ロケツトエンジン Granted JPS6053650A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3328117.3 1983-08-04
DE19833328117 DE3328117A1 (de) 1983-08-04 1983-08-04 Verfahren zum betreiben eines nebenstrom-raketentriebwerkes

Publications (2)

Publication Number Publication Date
JPS6053650A true JPS6053650A (ja) 1985-03-27
JPH0370108B2 JPH0370108B2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1991-11-06

Family

ID=6205734

Family Applications (1)

Application Number Title Priority Date Filing Date
JP16298784A Granted JPS6053650A (ja) 1983-08-04 1984-08-03 バイパス型ロケツトエンジンの運転方法およびこの方法を実施するためのバイパス型ロケツトエンジン

Country Status (3)

Country Link
JP (1) JPS6053650A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
DE (1) DE3328117A1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
FR (1) FR2550277B1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01318752A (ja) * 1988-05-11 1989-12-25 Royal Ordnance Plc 二液型推進剤ロケットエンジンの構造体
JPH07174046A (ja) * 1993-07-26 1995-07-11 Shoichi Nomoto 酸素水素ロケット・エンジン

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3506826A1 (de) * 1985-02-27 1986-08-28 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Verfahren zum betreiben eines fluessigkeitsraketentriebwerks und raketentriebwerk zur durchfuehrung des verfahrens
US4771600A (en) * 1986-10-20 1988-09-20 United Technologies Corporation Tripropellant rocket engine
RU2125177C1 (ru) * 1998-02-12 1999-01-20 Федеральное государственное унитарное предприятие Конструкторское бюро химавтоматики Способ изменения режима работы жрд и жидкостный ракетный двигатель для реализации способа
RU2190114C2 (ru) * 2000-06-30 2002-09-27 ОАО "НПО Энергомаш им. акад. В.П.Глушко" Жидкостный ракетный двигатель на криогенных компонентах топлива с замкнутым контуром привода турбины турбонасосного агрегата
RU2278988C2 (ru) * 2003-12-25 2006-06-27 ОАО "НПО Энергомаш имени академика В.П. Глушко" Способ настройки и регулирования параметров жидкостного ракетного двигателя
RU2436989C2 (ru) * 2008-06-16 2011-12-20 Федеральное государственное унитарное предприятие "Научно-исследовательский институт машиностроения" (ФГУП "НИИМаш") Способ настройки жидкостного двигателя малой тяги с двухкомпонентной центробежной форсункой
RU2391544C1 (ru) * 2008-12-17 2010-06-10 Государственное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" Камера жидкостного ракетного двигателя
RU2422665C2 (ru) * 2008-12-17 2011-06-27 Государственное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" Способ установки трубы
RU2451202C1 (ru) * 2011-04-27 2012-05-20 Открытое акционерное общество "Конструкторское бюро химавтоматики" Способ форсирования по тяге жидкостного ракетного двигателя и жидкостный ракетный двигатель
RU2484286C1 (ru) * 2011-12-07 2013-06-10 Николай Борисович Болотин Кислородно-водородный жидкостный ракетный двигатель
RU2484285C1 (ru) * 2011-12-29 2013-06-10 Николай Борисович Болотин Кислородно-водородный жидкостный ракетный двигатель
CN115614185B (zh) * 2022-11-22 2023-05-16 东方空间(西安)宇航技术有限公司 一种火箭发动机热试车台气液供应系统
CN116480488A (zh) * 2023-06-19 2023-07-25 西安航天动力研究所 一种可自适应起动的补燃循环发动机系统及其起动方法

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3257800A (en) * 1963-02-01 1966-06-28 United Aircraft Corp Propellant flow control system
US3302406A (en) * 1963-10-14 1967-02-07 Curtiss Wright Corp Rocket engine throttling means
DE2155786A1 (de) * 1971-11-10 1973-05-17 Messerschmitt Boelkow Blohm Startverfahren fuer ein fluessigkeitsraketentriebwerk
DE2241383C3 (de) * 1972-08-23 1978-07-27 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Flüssigkeitsraketentriebwerk der Hauptstrombauart

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01318752A (ja) * 1988-05-11 1989-12-25 Royal Ordnance Plc 二液型推進剤ロケットエンジンの構造体
JPH07174046A (ja) * 1993-07-26 1995-07-11 Shoichi Nomoto 酸素水素ロケット・エンジン

Also Published As

Publication number Publication date
FR2550277B1 (fr) 1986-08-08
FR2550277A1 (fr) 1985-02-08
JPH0370108B2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1991-11-06
DE3328117A1 (de) 1985-02-14
DE3328117C2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1987-06-19

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