FR2801936B1 - Moteur de fusee pour combustible liquide a circuit moteur ferme - Google Patents

Moteur de fusee pour combustible liquide a circuit moteur ferme

Info

Publication number
FR2801936B1
FR2801936B1 FR0015567A FR0015567A FR2801936B1 FR 2801936 B1 FR2801936 B1 FR 2801936B1 FR 0015567 A FR0015567 A FR 0015567A FR 0015567 A FR0015567 A FR 0015567A FR 2801936 B1 FR2801936 B1 FR 2801936B1
Authority
FR
France
Prior art keywords
engine
liquid fuel
closed
circuit
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.)
Expired - Fee Related
Application number
FR0015567A
Other languages
English (en)
Other versions
FR2801936A1 (fr
Inventor
Chris Udo Mading
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 DS GmbH
Original Assignee
Astrium 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 Astrium GmbH filed Critical Astrium GmbH
Publication of FR2801936A1 publication Critical patent/FR2801936A1/fr
Application granted granted Critical
Publication of FR2801936B1 publication Critical patent/FR2801936B1/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

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)
  • Supercharger (AREA)
  • Jet Pumps And Other Pumps (AREA)
FR0015567A 1999-12-03 2000-12-01 Moteur de fusee pour combustible liquide a circuit moteur ferme Expired - Fee Related FR2801936B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19958310A DE19958310C2 (de) 1999-12-03 1999-12-03 Raketentriebwerk für Flüssigtreibstoffe mit einem geschlossenen Triebwerkskreislauf

Publications (2)

Publication Number Publication Date
FR2801936A1 FR2801936A1 (fr) 2001-06-08
FR2801936B1 true FR2801936B1 (fr) 2004-07-02

Family

ID=7931295

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0015567A Expired - Fee Related FR2801936B1 (fr) 1999-12-03 2000-12-01 Moteur de fusee pour combustible liquide a circuit moteur ferme

Country Status (4)

Country Link
US (1) US6470670B2 (fr)
JP (1) JP4430226B2 (fr)
DE (1) DE19958310C2 (fr)
FR (1) FR2801936B1 (fr)

Families Citing this family (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3870252B2 (ja) * 2001-07-19 2007-01-17 独立行政法人 宇宙航空研究開発機構 キャビテーション抑制ポンプシステム
US6769242B1 (en) * 2001-11-21 2004-08-03 Mse Technology Applications, Inc. Rocket engine
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
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
WO2007041773A1 (fr) * 2005-10-07 2007-04-19 Biopharmica Ltd Agent de contrôle de sumoylation et applications
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
US7685807B2 (en) * 2006-09-06 2010-03-30 United Technologies Corporation Three component injector for kerosene-oxygen rocket engine
US20080264372A1 (en) * 2007-03-19 2008-10-30 Sisk David B Two-stage ignition system
US20080299504A1 (en) * 2007-06-01 2008-12-04 Mark David Horn Resonance driven glow plug torch igniter and ignition method
FR2921979B1 (fr) 2007-10-08 2014-06-13 Astrium Sas Dispositif et procede de motorisation de pompe pour moteur fusee par moteur a combustion interne
US8814562B2 (en) * 2008-06-02 2014-08-26 Aerojet Rocketdyne Of De, Inc. Igniter/thruster with catalytic decomposition chamber
US8161725B2 (en) 2008-09-22 2012-04-24 Pratt & Whitney Rocketdyne, Inc. Compact cyclone combustion torch igniter
US8381508B2 (en) * 2009-05-28 2013-02-26 Alliant Techsystems Inc. Closed-cycle rocket engine assemblies and methods of operating such rocket engine assemblies
JP5762093B2 (ja) 2011-03-31 2015-08-12 三菱重工業株式会社 航空機・宇宙機用流体冷却システム及び航空機・宇宙機用流体冷却方法
RU2476706C1 (ru) * 2011-09-21 2013-02-27 Николай Борисович Болотин Жидкостный ракетный двигатель
RU2476708C1 (ru) * 2011-11-25 2013-02-27 Николай Борисович Болотин Жидкостный ракетный двигатель
RU2476709C1 (ru) * 2011-11-25 2013-02-27 Николай Борисович Болотин Жидкостный ракетный двигатель
US9200596B2 (en) 2011-12-13 2015-12-01 Aerojet Rocketdyne, Inc. Catalytically enhanced gas generator system for rocket applications
FR2985804B1 (fr) * 2012-01-17 2014-02-07 Snecma Moteur pour fusee a alimentation optimisee
RU2481550C1 (ru) * 2012-03-07 2013-05-10 Николай Борисович Болотин Жидкостный ракетный двигатель (варианты)
EP2806138B1 (fr) * 2013-05-22 2015-09-02 Astrium GmbH Système de génération de gaz
FR3009586B1 (fr) * 2013-08-06 2015-08-28 Snecma Dispositif d'alimentation en ergol de moteur-fusee
US9695786B2 (en) * 2015-01-13 2017-07-04 Caterpillar Inc. Engine intake system and method for operating same
WO2018022723A1 (fr) * 2016-07-29 2018-02-01 Aerojet Rocketdyne, Inc. Drain de turbopompe de moteur-fusée à propergol liquide
RU2711887C1 (ru) * 2016-09-14 2020-01-23 АйЭйчАй КОРПОРЕЙШН Жидкостная ракетная двигательная установка со вспомогательной элктрической мощностью
RU2692598C1 (ru) * 2018-07-31 2019-06-25 Акционерное общество "НПО Энергомаш имени академика В.П.Глушко" Жидкостный ракетный двигатель
EP3847365A4 (fr) * 2018-09-06 2022-05-18 Oqab Dietrich Induction Inc. Moteur pour produire une poussée
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
FR3115838A1 (fr) 2020-10-29 2022-05-06 Marc Grosman Moteur-fusée à antimatière.
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

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1626082B1 (de) * 1967-07-26 1970-06-25 Erno Raumfahrttechnik Gmbh Raketentriebwerk fuer fluessige treibstoffe
DE2241383C3 (de) * 1972-08-23 1978-07-27 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Flüssigkeitsraketentriebwerk der Hauptstrombauart
US4831818A (en) * 1988-03-09 1989-05-23 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Dual-fuel, dual-mode rocket engine
GB8811126D0 (en) * 1988-05-11 1988-12-14 Royal Ordnance Plc Bipropellant rocket engines
FR2698914B1 (fr) * 1992-12-09 1995-03-03 Europ Propulsion Moteur-fusée à ergols liquides à flux dérivé et générateur de gaz intégré.
US5551230A (en) * 1994-03-14 1996-09-03 Rockwell International Corporation Heat induced high pressure lox pump rocket engine cycle
RU2095607C1 (ru) * 1995-07-19 1997-11-10 Ракетно-космическая корпорация "Энергия" им.С.П.Королева Жидкостный ракетный двигатель на криогенном топливе
RU2158839C2 (ru) * 1999-01-21 2000-11-10 Открытое акционерное общество "НПО Энергомаш им. акад. В.П. Глушко" Жидкостный ракетный двигатель с дожиганием турбогаза

Also Published As

Publication number Publication date
US20010015063A1 (en) 2001-08-23
JP2001193565A (ja) 2001-07-17
JP4430226B2 (ja) 2010-03-10
FR2801936A1 (fr) 2001-06-08
DE19958310C2 (de) 2002-01-17
DE19958310A1 (de) 2001-06-28
US6470670B2 (en) 2002-10-29

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