SE450787B - Forbrenningskammare i en raketmotor med ett flerdelat trattformigt parti - Google Patents

Forbrenningskammare i en raketmotor med ett flerdelat trattformigt parti

Info

Publication number
SE450787B
SE450787B SE8202303A SE8202303A SE450787B SE 450787 B SE450787 B SE 450787B SE 8202303 A SE8202303 A SE 8202303A SE 8202303 A SE8202303 A SE 8202303A SE 450787 B SE450787 B SE 450787B
Authority
SE
Sweden
Prior art keywords
funnel
shaped part
shaped
combustion chamber
nozzle
Prior art date
Application number
SE8202303A
Other languages
English (en)
Swedish (sv)
Other versions
SE8202303L (sv
Inventor
G Gill
A Souchier
G Dorville
Original Assignee
Europ Propulsion
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 Europ Propulsion filed Critical Europ Propulsion
Publication of SE8202303L publication Critical patent/SE8202303L/xx
Publication of SE450787B publication Critical patent/SE450787B/sv

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)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Infusion, Injection, And Reservoir Apparatuses (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
SE8202303A 1981-04-13 1982-04-13 Forbrenningskammare i en raketmotor med ett flerdelat trattformigt parti SE450787B (sv)

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
SE8202303L SE8202303L (sv) 1982-10-14
SE450787B true SE450787B (sv) 1987-07-27

Family

ID=9257325

Family Applications (1)

Application Number Title Priority Date Filing Date
SE8202303A SE450787B (sv) 1981-04-13 1982-04-13 Forbrenningskammare i en raketmotor med ett flerdelat trattformigt parti

Country Status (4)

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

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
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.
FR2705738B1 (fr) * 1993-05-28 1995-08-18 Europ Propulsion Tuyère de moteur-fusée à diffuseur éjectable.
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
US6318071B2 (en) * 1996-09-23 2001-11-20 Volvo Aero Corporation Controlled temperature rocket nozzle
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
EP3271567B1 (de) * 2015-03-15 2020-04-29 Aerojet Rocketdyne, Inc. Raketenschubdüse mit verbindern und strebe
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
FR2503794A1 (fr) 1982-10-15
FR2503794B1 (fr) 1986-04-25
DE3213161C2 (de) 1991-05-08
SE8202303L (sv) 1982-10-14
US4434614A (en) 1984-03-06
DE3213161A1 (de) 1982-11-25

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