DE69923944D1 - Flüssigtreibstoffrakete - Google Patents

Flüssigtreibstoffrakete

Info

Publication number
DE69923944D1
DE69923944D1 DE69923944T DE69923944T DE69923944D1 DE 69923944 D1 DE69923944 D1 DE 69923944D1 DE 69923944 T DE69923944 T DE 69923944T DE 69923944 T DE69923944 T DE 69923944T DE 69923944 D1 DE69923944 D1 DE 69923944D1
Authority
DE
Germany
Prior art keywords
liquid propellant
propellant rocket
rocket
liquid
propellant
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 - Lifetime
Application number
DE69923944T
Other languages
English (en)
Other versions
DE69923944T2 (de
Inventor
Boris Ivanovich Katorgin
Vladimir Konstantinovi Chvanov
Gennady Grogorievich Derkach
Jury Vasilievich Movchan
Felix Jurievich Chelkis
Vadim Lliich Semenov
Leonid Alexeevich Tolstikov
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.)
Nauchno Proizvodstvennoe Obiedinenie Energomas OAO
Borovichsky Kombinat Ogneuporov OAO
Original Assignee
Nauchno Proizvodstvennoe Obiedinenie Energomas OAO
Borovichsky Kombinat Ogneuporov OAO
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 Nauchno Proizvodstvennoe Obiedinenie Energomas OAO, Borovichsky Kombinat Ogneuporov OAO filed Critical Nauchno Proizvodstvennoe Obiedinenie Energomas OAO
Application granted granted Critical
Publication of DE69923944D1 publication Critical patent/DE69923944D1/de
Publication of DE69923944T2 publication Critical patent/DE69923944T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F02K9/95—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by starting or ignition means or arrangements

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
DE69923944T 1999-01-21 1999-12-15 Flüssigtreibstoffrakete Expired - Lifetime DE69923944T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
RU99100839/06A RU2158839C2 (ru) 1999-01-21 1999-01-21 Жидкостный ракетный двигатель с дожиганием турбогаза
RU99100839 1999-01-21

Publications (2)

Publication Number Publication Date
DE69923944D1 true DE69923944D1 (de) 2005-04-07
DE69923944T2 DE69923944T2 (de) 2006-04-06

Family

ID=20214719

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69923944T Expired - Lifetime DE69923944T2 (de) 1999-01-21 1999-12-15 Flüssigtreibstoffrakete

Country Status (4)

Country Link
US (1) US6226980B1 (de)
EP (1) EP1022454B1 (de)
DE (1) DE69923944T2 (de)
RU (1) RU2158839C2 (de)

Families Citing this family (57)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19958310C2 (de) * 1999-12-03 2002-01-17 Daimler Chrysler Ag Raketentriebwerk für Flüssigtreibstoffe mit einem geschlossenen Triebwerkskreislauf
RU2200866C2 (ru) * 2000-12-04 2003-03-20 ОАО "НПО Энергомаш им. акад. В.П.Глушко" Регулируемый жидкостный ракетный двигатель
FR2825135A1 (fr) 2001-05-22 2002-11-29 Lockheed Corp Systeme embarque de stockage de gaz et d'alimentation en gaz
DE10141108B4 (de) * 2001-08-22 2005-06-30 Eads Space Transportation Gmbh Raketentriebwerk mit geschlossenen Triebwerkskreislauf mit modularer Zuführung der Turbinenabgase
US6769242B1 (en) * 2001-11-21 2004-08-03 Mse Technology Applications, Inc. Rocket engine
US6684625B2 (en) 2002-01-22 2004-02-03 Hy Pat Corporation Hybrid rocket motor using a turbopump to pressurize a liquid propellant constituent
US6679049B2 (en) 2002-01-22 2004-01-20 Hy Pat Corporation Hybrid rocket motor having a precombustion chamber
US6640536B2 (en) 2002-01-22 2003-11-04 Hy Pat Corporation Hybrid rocket motor using a turbopump to pressurize a liquid propellant constituent
US6739121B2 (en) 2002-01-22 2004-05-25 Environmental Areoscience Corp. Flame holder for a hybrid rocket motor
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
US6968673B1 (en) * 2003-11-14 2005-11-29 Knight Andrew F Cool gas generator and ultra-safe rocket engine
US7477966B1 (en) * 2004-02-20 2009-01-13 Lockheed Martin Corporation Propellant management system and method for multiple booster rockets
US8127527B2 (en) * 2004-11-22 2012-03-06 General Electric Company Methods and systems for operating oxidizer systems
US7418814B1 (en) 2005-06-30 2008-09-02 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Dual expander cycle rocket engine with an intermediate, closed-cycle heat exchanger
US7389636B2 (en) * 2005-07-06 2008-06-24 United Technologies Corporation Booster rocket engine using gaseous hydrocarbon in catalytically enhanced gas generator cycle
US7565795B1 (en) * 2006-01-17 2009-07-28 Pratt & Whitney Rocketdyne, Inc. Piezo-resonance igniter and ignition method for propellant liquid rocket engine
US8122703B2 (en) 2006-04-28 2012-02-28 United Technologies Corporation Coaxial ignition assembly
US20080299504A1 (en) * 2007-06-01 2008-12-04 Mark David Horn Resonance driven glow plug torch igniter and ignition method
US8814562B2 (en) * 2008-06-02 2014-08-26 Aerojet Rocketdyne Of De, Inc. Igniter/thruster with catalytic decomposition chamber
US8731745B2 (en) * 2008-07-01 2014-05-20 Aerojet Rocketdyne Of De, Inc. Sequence diagram system
US8161725B2 (en) 2008-09-22 2012-04-24 Pratt & Whitney Rocketdyne, Inc. Compact cyclone combustion torch igniter
US8407981B1 (en) * 2010-02-05 2013-04-02 Florida Turbine Technologies, Inc. Johnson Sexton cycle rocket engine
US8671687B2 (en) * 2011-02-18 2014-03-18 Chris Gudmundson Hydrogen based combined steam cycle apparatus
RU2466292C1 (ru) * 2011-08-23 2012-11-10 Николай Борисович Болотин Жидкостный ракетный двигатель
FR2985804B1 (fr) * 2012-01-17 2014-02-07 Snecma Moteur pour fusee a alimentation optimisee
RU2506444C1 (ru) * 2012-05-22 2014-02-10 Александр Фролович Ефимочкин Жидкостный ракетный двигатель
RU2513023C2 (ru) * 2012-07-31 2014-04-20 Открытое акционерное общество "НПО Энергомаш имени академика В.П. Глушко" Способ обеспечения бессрывной работы турбонасосного агрегата многорежимного жидкостного ракетного двигателя на режимах глубокого дросселирования
RU2520771C1 (ru) * 2012-11-14 2014-06-27 Открытое акционерное общество "НПО Энергомаш имени академика В.П. Глушко" Жидкостный ракетный двигатель по схеме с дожиганием генераторного газа
DE102013105526B4 (de) * 2013-05-29 2021-02-25 Deutsches Zentrum für Luft- und Raumfahrt e.V. Raumfahrtantrieb und Verfahren zum Starten eines Raumfahrtantriebs
FR3009587B1 (fr) * 2013-08-06 2015-08-28 Snecma Dispositif de pressurisation de reservoirs d'ergol d'un moteur de fusee
RU2545613C1 (ru) * 2014-03-11 2015-04-10 Николай Борисович Болотин Жидкостный ракетный двигатель
RU2545615C1 (ru) * 2014-03-18 2015-04-10 Николай Борисович Болотин Турбонасосный агрегат жидкостного ракетного двигателя
RU2560656C1 (ru) * 2014-11-11 2015-08-20 Николай Борисович Болотин Турбонасосный агрегат жидкостного ракетного двигателя
DE102015001271A1 (de) 2015-02-04 2016-08-04 Airbus Ds Gmbh Turbopumpe für ein Raketentriebwerk mit einer Radialstufe
ITUB20151139A1 (it) * 2015-05-26 2016-11-26 Avio Spa Motore a propellente liquido
EP3318745B1 (de) * 2015-09-14 2020-03-11 Korea Aerospace Research Institute Flüssigkeitsraketenmotor mit elektromotorisch angetriebener boosterpumpe
US11084605B2 (en) * 2016-02-05 2021-08-10 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Device and system for controlling missiles and kill vehicles operated with gel-like fuels
RU2671449C2 (ru) * 2016-12-28 2018-10-31 Акционерное общество "НПО Энергомаш имени академика В.П. Глушко" Ампула с пусковым горючим для зажигания компонентов топлива жидкостного ракетного двигателя
RU2647937C1 (ru) * 2017-07-18 2018-03-21 Владислав Юрьевич Климов Жидкостный ракетный двигатель
CN108953003B (zh) * 2018-06-28 2021-03-23 西安航天动力研究所 一种实现补燃循环发动机系统及推力深度调节方法
US11149691B2 (en) 2018-08-29 2021-10-19 Special Aerospace Services, LLC Staged combustion liquid rocket engine cycle with the turbopump unit and preburner integrated into the structure of the combustion chamber
US11970996B2 (en) 2018-08-29 2024-04-30 Special Aerospace Services, LLC Staged combustion liquid rocket engine cycle with the turbopump unit and preburner integrated into the structure of the combustion chamber
CN109372657B (zh) * 2018-08-31 2021-09-07 西安航天动力研究所 一种新型预冷空气组合发动机
CN110005546A (zh) * 2019-03-14 2019-07-12 北京星际荣耀空间科技有限公司 一种多次起动火箭发动机及起动方法
CN109973246B (zh) * 2019-03-22 2020-06-30 西安航天动力研究所 一种气液复合驱动预压涡轮泵结构及预压涡轮泵驱动方法
CN111720238B (zh) * 2019-07-03 2021-08-10 西安航天动力研究所 基于液氧膨胀循环的深度变推多次起动液体火箭发动机
WO2021091613A2 (en) * 2019-09-06 2021-05-14 Special Aerospace Services, LLC Staged combustion liquid rocket engine cycle with the turbopump unit and preburner integrated into the structure of the combustion chamber
FR3104647B1 (fr) * 2019-12-12 2022-08-05 Centre Nat Etd Spatiales Dispositif d’allumage pour moteur-fusée
CN111927648B (zh) * 2020-07-31 2021-09-03 西安航天动力研究所 一种基于无毒环保推进剂的轨姿控集成动力系统
CN111963337B (zh) * 2020-08-21 2022-07-19 西安航天动力研究所 一种富氧补燃发动机推力室直连热试系统及热试方法
CN112196702B (zh) * 2020-10-19 2022-01-04 北京天兵科技有限公司 一种液体火箭发动机起动器及其设计方法
CN112555056B (zh) * 2020-12-02 2022-05-10 西安航天动力研究所 补燃循环液体发动机核心系统热试验装置及参数协调方法
CN114458476A (zh) * 2020-12-28 2022-05-10 北京天兵科技有限公司 一种液体火箭发动机冷气驱动强迫起动系统和方法
CN112377331B (zh) * 2021-01-18 2021-04-06 北京星际荣耀空间科技股份有限公司 一种火箭发动机多次点火起动装置及具有其的火箭发动机
RU2771473C1 (ru) * 2021-07-21 2022-05-04 Акционерное общество "Конструкторское бюро химавтоматики" Жидкостный ракетный двигатель, работающий по схеме с дожиганием восстановительного генераторного газа
CN113958425B (zh) * 2021-12-20 2022-05-10 西安航天动力研究所 一种开式循环液氧煤油发动机系统及其使用方法

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US3623329A (en) * 1960-04-12 1971-11-30 United Aircraft Corp Control system for liquid rocket
US4171615A (en) * 1966-04-21 1979-10-23 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Supercharged topping rocket propellant feed system
FR2232685A1 (en) * 1973-06-09 1975-01-03 Messerschmitt Boelkow Blohm Fluid drive system for rockets - with pre-combustion chamber to raise oxydator-rich gas mixture, and based on main drive electrical system
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
US5873241A (en) * 1991-05-23 1999-02-23 United Technologies Corporation Rocket engine auxiliary power system
US5444973A (en) * 1993-12-13 1995-08-29 United Technologies Corporation Pressure-fed rocket booster system
US5551230A (en) * 1994-03-14 1996-09-03 Rockwell International Corporation Heat induced high pressure lox pump rocket engine cycle

Also Published As

Publication number Publication date
EP1022454A3 (de) 2002-07-17
DE69923944T2 (de) 2006-04-06
RU2158839C2 (ru) 2000-11-10
EP1022454B1 (de) 2005-03-02
EP1022454A2 (de) 2000-07-26
US6226980B1 (en) 2001-05-08

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition