FR2832762B1 - Rallonge de tuyere pour moteur de fusee - Google Patents

Rallonge de tuyere pour moteur de fusee

Info

Publication number
FR2832762B1
FR2832762B1 FR0214852A FR0214852A FR2832762B1 FR 2832762 B1 FR2832762 B1 FR 2832762B1 FR 0214852 A FR0214852 A FR 0214852A FR 0214852 A FR0214852 A FR 0214852A FR 2832762 B1 FR2832762 B1 FR 2832762B1
Authority
FR
France
Prior art keywords
tuyere
extension
rotor motor
rotor
motor
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
FR0214852A
Other languages
English (en)
Other versions
FR2832762A1 (fr
Inventor
Josef Grober
Peter Hampl
Herbert Linner
Karl Brey
Bernhard Stahn
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 FR2832762A1 publication Critical patent/FR2832762A1/fr
Application granted granted Critical
Publication of FR2832762B1 publication Critical patent/FR2832762B1/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
    • F02K9/97—Rocket nozzles
    • F02K9/976—Deployable nozzles
    • 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
    • F02K9/97—Rocket nozzles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Inorganic Fibers (AREA)
  • Ceramic Products (AREA)
  • Nozzles (AREA)
FR0214852A 2001-11-27 2002-11-27 Rallonge de tuyere pour moteur de fusee Expired - Fee Related FR2832762B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE10157752A DE10157752B4 (de) 2001-11-27 2001-11-27 Düsenverlängerung

Publications (2)

Publication Number Publication Date
FR2832762A1 FR2832762A1 (fr) 2003-05-30
FR2832762B1 true FR2832762B1 (fr) 2007-11-02

Family

ID=7706890

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0214852A Expired - Fee Related FR2832762B1 (fr) 2001-11-27 2002-11-27 Rallonge de tuyere pour moteur de fusee

Country Status (5)

Country Link
US (1) US6817184B2 (fr)
DE (1) DE10157752B4 (fr)
FR (1) FR2832762B1 (fr)
IT (1) ITMI20022423A1 (fr)
SE (1) SE523633C2 (fr)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2840030B1 (fr) * 2002-05-21 2005-03-04 Eads Launch Vehicles Moteur a tuyere a noyau central pour lanceur spatial
FR2916018B1 (fr) * 2007-05-10 2009-08-21 Snecma Propulsion Solide Sa Systeme d'echappement pour turbine a gaz
DE102008020198B8 (de) * 2008-04-15 2015-05-13 Astrium Gmbh Düsenerweiterung für ein Triebwerk und Verfahren zur Herstellung und Kühlung einer Düsenerweiterung
FR2934014B1 (fr) * 2008-07-17 2011-05-13 Snecma Propulsion Solide Procede de realisation d'une tuyere ou d'un divergent de tuyere en materiau composite.
US8281603B2 (en) * 2008-08-11 2012-10-09 United Technologies Corporation Fastener assembly for connecting rocket engine nozzles
FR2949821B1 (fr) * 2009-09-10 2011-09-30 Snecma Moteur fusee a divergent deployable
DE102011011220A1 (de) * 2011-02-15 2012-08-16 Astrium Gmbh Raketentriebwerk mit einer ausfahrbaren Düsenerweiterung
FR3008139B1 (fr) * 2013-07-04 2015-07-24 Snecma Dispositif et procede de liaison
CN104696104B (zh) * 2013-12-10 2016-08-31 上海新力动力设备研究所 固体火箭发动机挡环连接结构
JP6909242B2 (ja) * 2016-06-21 2021-07-28 エアロジェット ロケットダイン インコーポレイテッド 受動的凝縮物冷却を有する液体推進剤ロケットエンジン
FR3053403B1 (fr) * 2016-06-29 2018-07-27 Arianegroup Sas Moteur-fusee a divergent composite
FR3056256B1 (fr) * 2016-09-20 2020-11-06 Airbus Safran Launchers Moteur-fusee a divergent segmente
US11028802B2 (en) * 2016-11-14 2021-06-08 Northrop Grumman Systems Corporation Liquid rocket engine assemblies and related methods
US10471542B1 (en) * 2017-06-27 2019-11-12 United States Of America As Represented By The Administrator Of Nasa Cladding and freeform deposition for coolant channel closeout
FR3094414B1 (fr) * 2019-03-27 2021-04-09 Arianegroup Sas Tuyère équipée d’une couronne thermo-régulée
CN112523902A (zh) * 2020-11-30 2021-03-19 内蒙动力机械研究所 一种基于3d打印的喷管用复合材料固定壳体

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3596465A (en) * 1970-03-12 1971-08-03 Nasa Inflatable transpiration cooled nozzle
US3648461A (en) * 1970-05-13 1972-03-14 Nasa Solid propellent rocket motor nozzle
US3866792A (en) * 1973-03-02 1975-02-18 Hercules Inc Integral filament reinforced composite-rocket chamber/adapter
US4063684A (en) * 1975-11-25 1977-12-20 The United States Of America As Represented By The Secretary Of The Air Force Composite rocket nozzle structure
US4182495A (en) * 1978-12-04 1980-01-08 The United States Of America As Represented By The Secretary Of The Navy Graphite or carbon fiber composite structure, low temperature cure
US4967599A (en) * 1980-05-19 1990-11-06 Societe Europeenne De Propulsion Mechanical and insulating connection between a nozzle and the filament-wound casing of the combustion chamber of a solid propellant rocket motor
US4383407A (en) * 1981-02-02 1983-05-17 Thiokol Corporation Extendible thrust nozzle for rockets
US4477024A (en) * 1983-04-05 1984-10-16 The United States Of America As Represented By The Secretary Of The Air Force Carbon/carbon rocket motor exit cone reinforcement
US5540949A (en) * 1986-04-24 1996-07-30 The United States Of America As Represented By The Secretary Of The Air Force Method for cutting threads in a carbon-carbon structure
FR2652615B1 (fr) * 1989-10-04 1992-02-07 Europ Propulsion Chambre de combustion de propulseur.
US6324833B1 (en) * 1990-04-24 2001-12-04 Cordant Technologies, Inc. Reinforced composite articles and method of making same
US5113540A (en) * 1991-07-03 1992-05-19 Sereboff Joel L Fluid cushion with passages for ischial spines
DE19632893C2 (de) * 1996-08-16 2001-02-08 Industrieanlagen Betr Sgmbh Ia Verfahren zur Herstellung von Flugkörperkomponenten aus faserverstärkter Keramik
DE19730674A1 (de) * 1997-07-17 1999-01-21 Deutsch Zentr Luft & Raumfahrt Brennkammer und Verfahren zur Herstellung einer Brennkammer
DE19858197B4 (de) * 1998-12-17 2005-05-04 Eads Space Transportation Gmbh Triebwerk

Also Published As

Publication number Publication date
SE523633C2 (sv) 2004-05-04
SE0203504D0 (sv) 2002-11-26
US20030136128A1 (en) 2003-07-24
SE0203504L (sv) 2003-05-28
ITMI20022423A1 (it) 2003-05-28
DE10157752A1 (de) 2003-06-18
FR2832762A1 (fr) 2003-05-30
DE10157752B4 (de) 2006-04-06
US6817184B2 (en) 2004-11-16

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Legal Events

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Year of fee payment: 14

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Year of fee payment: 15

ST Notification of lapse

Effective date: 20180731