FR2503794B1 - Chambre de combustion de propulseur-fusee a divergent multiple - Google Patents

Chambre de combustion de propulseur-fusee a divergent multiple

Info

Publication number
FR2503794B1
FR2503794B1 FR8107366A FR8107366A FR2503794B1 FR 2503794 B1 FR2503794 B1 FR 2503794B1 FR 8107366 A FR8107366 A FR 8107366A FR 8107366 A FR8107366 A FR 8107366A FR 2503794 B1 FR2503794 B1 FR 2503794B1
Authority
FR
France
Prior art keywords
combustion chamber
rocket combustion
multiple divergent
divergent rocket
chamber
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
Application number
FR8107366A
Other languages
English (en)
Other versions
FR2503794A1 (fr
Inventor
George Gill
Alain Souchier
Georges Dorville
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.)
Societe Europeenne de Propulsion SEP SA
Original Assignee
Societe Europeenne de Propulsion SEP SA
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 Societe Europeenne de Propulsion SEP SA filed Critical Societe Europeenne de Propulsion SEP SA
Priority to FR8107366A priority Critical patent/FR2503794B1/fr
Priority to DE19823213161 priority patent/DE3213161A1/de
Priority to US06/366,985 priority patent/US4434614A/en
Priority to SE8202303A priority patent/SE450787B/sv
Publication of FR2503794A1 publication Critical patent/FR2503794A1/fr
Application granted granted Critical
Publication of FR2503794B1 publication Critical patent/FR2503794B1/fr
Expired 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
    • F02K9/978—Closures for nozzles; Nozzles comprising ejectable or discardable elements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • F05D2250/32—Arrangement of components according to their shape
    • F05D2250/324—Arrangement of components according to their shape divergent

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Engines (AREA)
  • Toys (AREA)
  • Infusion, Injection, And Reservoir Apparatuses (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
FR8107366A 1981-04-13 1981-04-13 Chambre de combustion de propulseur-fusee a divergent multiple Expired FR2503794B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR8107366A FR2503794B1 (fr) 1981-04-13 1981-04-13 Chambre de combustion de propulseur-fusee a divergent multiple
DE19823213161 DE3213161A1 (de) 1981-04-13 1982-04-08 Brennkammer fuer raketentriebwerk
US06/366,985 US4434614A (en) 1981-04-13 1982-04-09 Combustion chamber in a rocket propulsion system with multiple divergent portion
SE8202303A SE450787B (sv) 1981-04-13 1982-04-13 Forbrenningskammare i en raketmotor med ett flerdelat trattformigt parti

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8107366A FR2503794B1 (fr) 1981-04-13 1981-04-13 Chambre de combustion de propulseur-fusee a divergent multiple

Publications (2)

Publication Number Publication Date
FR2503794A1 FR2503794A1 (fr) 1982-10-15
FR2503794B1 true FR2503794B1 (fr) 1986-04-25

Family

ID=9257325

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8107366A Expired FR2503794B1 (fr) 1981-04-13 1981-04-13 Chambre de combustion de propulseur-fusee a divergent multiple

Country Status (4)

Country Link
US (1) US4434614A (fr)
DE (1) DE3213161A1 (fr)
FR (1) FR2503794B1 (fr)
SE (1) SE450787B (fr)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2602275B1 (fr) * 1986-08-04 1990-08-10 Onera (Off Nat Aerospatiale) Perfectionnements aux tuyeres de propulseurs pour reduction d'efforts lateraux
FR2705738B1 (fr) * 1993-05-28 1995-08-18 Europ Propulsion Tuyère de moteur-fusée à diffuseur éjectable.
FR2705739B1 (fr) * 1993-05-28 1995-08-18 Europ Propulsion Tuyère de moteur-fusée à section de sortie sélectivement réduite.
FR2705737B1 (fr) * 1993-05-28 1995-08-18 Europ Propulsion Tuyère de moteur-fusée à divergent échancré.
FR2724979A1 (fr) * 1994-09-26 1996-03-29 Europ Propulsion Dispositif de protection contre l'effet bouchon d'eau lors de la mise a feu d'un missile lance en immersion
US5779151A (en) * 1996-05-28 1998-07-14 Regents Of The University Of California Stepped nozzle
DE69621638T2 (de) * 1996-09-23 2002-11-07 Volvo Aero Corp Temperaturgeregelte raketendüse
FR2754566B1 (fr) * 1996-10-11 1999-02-05 Europ Propulsion Tuyere de moteur-fusee a inserts ejectables
FR2757571B1 (fr) * 1996-12-24 2003-03-28 Europ Propulsion Divergent deployable pour propulseur
SE519561C2 (sv) * 2000-07-03 2003-03-11 Bofors Carl Gustaf Ab Anordning vid raketmotorer för att förhindra att raketmotor bringas att explodera vid utvändig brand
FR2816990B1 (fr) 2000-11-22 2003-02-21 Snecma Moteurs Dispositif de reduction ou suppression de decollement de jet dans les tuyeres de moteur-fusee et tuyere comprenant le dispositif
FR2863666B1 (fr) * 2003-12-10 2006-03-24 Snecma Propulsion Solide Dispositif d'adaptation pour tuyere de moteur fusee a divergent mobile
US20060016551A1 (en) * 2004-07-23 2006-01-26 Christensen Donald J Phenolic lamination process for hot gas components
KR100851889B1 (ko) 2007-06-29 2008-08-13 국방과학연구소 강제 박리장치를 구비한 로켓용 노즐
JP5736827B2 (ja) * 2011-02-18 2015-06-17 株式会社Ihi ノズルエクステンション
WO2016149075A1 (fr) * 2015-03-15 2016-09-22 Aerojet Rocketdyne, Inc. Tuyère de poussée de fusée ayant des raccords et un étançon
FR3094414B1 (fr) 2019-03-27 2021-04-09 Arianegroup Sas Tuyère équipée d’une couronne thermo-régulée
CN117532131B (zh) * 2024-01-09 2024-03-26 北京智创联合科技股份有限公司 火箭发动机燃烧室及其制作方法

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1071421B (de) * 1956-11-09 1959-12-17 Armstrong Siddeley Motors Ltd., Coventry, Warwickshire (Großbritannien) Brennkammer für Gasturbinen oder Raketenmotoren
US3079752A (en) * 1961-02-23 1963-03-05 Thompson Ramo Wooldridge Inc Variable expansion ratio nozzle
US3237402A (en) * 1963-11-14 1966-03-01 Steverding Bernard Variable thrust nozzle
US3372548A (en) * 1965-06-17 1968-03-12 Thiokol Chemical Corp Rocket nozzle
US4022129A (en) * 1976-01-16 1977-05-10 The United States Of America As Represented By The Secretary Of The Air Force Nozzle ejection system

Also Published As

Publication number Publication date
US4434614A (en) 1984-03-06
DE3213161A1 (de) 1982-11-25
DE3213161C2 (fr) 1991-05-08
SE450787B (sv) 1987-07-27
SE8202303L (sv) 1982-10-14
FR2503794A1 (fr) 1982-10-15

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Legal Events

Date Code Title Description
ST Notification of lapse