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FR2987081B1 - Ensemble et procede propulsifs - Google Patents

Ensemble et procede propulsifs

Info

Publication number
FR2987081B1
FR2987081B1 FR1251575A FR1251575A FR2987081B1 FR 2987081 B1 FR2987081 B1 FR 2987081B1 FR 1251575 A FR1251575 A FR 1251575A FR 1251575 A FR1251575 A FR 1251575A FR 2987081 B1 FR2987081 B1 FR 2987081B1
Authority
FR
France
Prior art keywords
propellant assembly
propellant
assembly
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
FR1251575A
Other languages
English (en)
Other versions
FR2987081A1 (fr
Inventor
Jean Marie Conrardy
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR1251575A priority Critical patent/FR2987081B1/fr
Priority to US13/771,562 priority patent/US9249758B2/en
Publication of FR2987081A1 publication Critical patent/FR2987081A1/fr
Application granted granted Critical
Publication of FR2987081B1 publication Critical patent/FR2987081B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44Feeding propellants
    • F02K9/46Feeding propellants using pumps
    • F02K9/48Feeding propellants using pumps driven by a gas turbine fed by propellant combustion gases or fed by vaporized propellants or other gases
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K7/00Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/18Composite ram-jet/rocket engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44Feeding propellants
    • F02K9/52Injectors

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Jet Pumps And Other Pumps (AREA)
FR1251575A 2012-02-21 2012-02-21 Ensemble et procede propulsifs Active FR2987081B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1251575A FR2987081B1 (fr) 2012-02-21 2012-02-21 Ensemble et procede propulsifs
US13/771,562 US9249758B2 (en) 2012-02-21 2013-02-20 Propulsion assembly and method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1251575A FR2987081B1 (fr) 2012-02-21 2012-02-21 Ensemble et procede propulsifs

Publications (2)

Publication Number Publication Date
FR2987081A1 FR2987081A1 (fr) 2013-08-23
FR2987081B1 true FR2987081B1 (fr) 2017-03-31

Family

ID=46704737

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1251575A Active FR2987081B1 (fr) 2012-02-21 2012-02-21 Ensemble et procede propulsifs

Country Status (2)

Country Link
US (1) US9249758B2 (fr)
FR (1) FR2987081B1 (fr)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106014683B (zh) * 2016-05-30 2018-04-06 西北工业大学 一种带增压流动控制装置的tbcc用sern结构
DE102017106758A1 (de) 2017-03-15 2018-09-20 Deutsches Zentrum für Luft- und Raumfahrt e.V. Schubkammervorrichtung und Verfahren zum Betreiben einer Schubkammervorrichtung
CN106968835B (zh) * 2017-04-14 2018-07-06 西北工业大学 一种宽范围工作的火箭冲压组合全流道
US11346306B1 (en) 2019-01-03 2022-05-31 Ball Aerospace & Technologies Corp. Chemical and cold gas propellant systems and methods
US11391247B1 (en) 2019-01-24 2022-07-19 Firefly Aerospace Inc. Liquid rocket engine cooling channels
US11333104B1 (en) 2019-01-24 2022-05-17 Firefly Aerospace Inc. Liquid rocket engine cross impinged propellant injection
US11498705B1 (en) 2019-05-09 2022-11-15 Ball Aerospace & Technology Corp. On orbit fluid propellant dispensing systems and methods
US11008977B1 (en) 2019-09-26 2021-05-18 Firefly Aerospace Inc. Liquid rocket engine tap-off power source
US11846251B1 (en) * 2020-04-24 2023-12-19 Firefly Aerospace Inc. Liquid rocket engine booster engine with combustion gas fuel source
US11512669B2 (en) 2020-06-24 2022-11-29 Raytheon Company Distributed airfoil aerospike rocket nozzle
EP4180649A4 (fr) * 2020-07-13 2023-11-15 Rafael MARTÍNEZ-VILANOVA PIÑÓN Moteur à réaction pour aéronefs
CN112922744B (zh) * 2021-03-05 2023-01-06 中国空气动力研究与发展中心空天技术研究所 一种壁面嵌入式的飞行器燃料输送装置
US12012233B2 (en) 2021-05-10 2024-06-18 Ball Aerospace & Technologies Corp. Active on orbit fluid propellant management and refueling systems and methods
US11945606B1 (en) 2021-10-19 2024-04-02 Ball Aerospace & Technologies Corp. Electric propulsion based spacecraft propulsion systems and methods utilizing multiple propellants
CN114109650B (zh) * 2021-10-27 2023-02-28 厦门大学 一种整体式液体火箭冲压组合动力装置
US11970995B2 (en) * 2022-05-31 2024-04-30 Venus Aerospace Corp. Oblique detonation rocket engine

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3085393A (en) * 1958-06-03 1963-04-16 North American Aviation Inc Rocket engine starting method
US3176464A (en) * 1960-05-24 1965-04-06 Martin Marietta Corp Ducted rocket engine
DE1571248B1 (de) * 1966-10-18 1970-06-04 Messerschmitt Boelkow Blohm Zweistufiges Verfahren zur Erzeugung von brennbaren,unter Druck stehenden Gasen fuer Triebwerke,insbesondere Raketen- und Staustrahltriebwerke
US6293091B1 (en) * 1999-04-22 2001-09-25 Trw Inc. Axisymmetrical annular plug propulsion system for integrated rocket/ramjet or rocket/scramjet
FR2836699B1 (fr) * 2002-03-04 2005-02-11 Eads Launch Vehicles Moteur de fusee
US6981364B2 (en) * 2003-07-22 2006-01-03 National Aerospace Laboratory Of Japan Combine engine for single-stage spacecraft
US20090113873A1 (en) * 2005-03-16 2009-05-07 Erik Henry Tweeton Continously air breathing assisted jet engine linear aerospkie rocket
FR2933744B1 (fr) 2008-07-11 2011-06-03 Snecma Moteur-fusee et reacteur comportant une pluralite de tels moteurs-fusees.

Also Published As

Publication number Publication date
FR2987081A1 (fr) 2013-08-23
US20140325958A1 (en) 2014-11-06
US9249758B2 (en) 2016-02-02

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