CA1175241A - Mechanical and insulating connection between a nozzle and the filament-wound casing of the combustion chamber of a rocket motor - Google Patents

Mechanical and insulating connection between a nozzle and the filament-wound casing of the combustion chamber of a rocket motor

Info

Publication number
CA1175241A
CA1175241A CA000377798A CA377798A CA1175241A CA 1175241 A CA1175241 A CA 1175241A CA 000377798 A CA000377798 A CA 000377798A CA 377798 A CA377798 A CA 377798A CA 1175241 A CA1175241 A CA 1175241A
Authority
CA
Canada
Prior art keywords
nozzle
connecting ring
connection
casing
heat
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
CA000377798A
Other languages
English (en)
French (fr)
Inventor
Paul Donguy
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.)
EUOPEENNE DE PROPULSION Ste
Original Assignee
EUOPEENNE DE PROPULSION Ste
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 EUOPEENNE DE PROPULSION Ste filed Critical EUOPEENNE DE PROPULSION Ste
Application granted granted Critical
Publication of CA1175241A publication Critical patent/CA1175241A/en
Expired legal-status Critical Current

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
    • F02K9/08Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32Constructional parts; Details not otherwise provided for
    • 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
    • F02K9/08Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32Constructional parts; Details not otherwise provided for
    • F02K9/34Casings; Combustion chambers; Liners thereof
    • F02K9/343Joints, connections, seals therefor
    • 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
    • F02K9/97Rocket nozzles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Thermal Insulation (AREA)
  • Ceramic Products (AREA)
CA000377798A 1980-05-19 1981-05-19 Mechanical and insulating connection between a nozzle and the filament-wound casing of the combustion chamber of a rocket motor Expired CA1175241A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR8011127 1980-05-19
FR8011127A FR2482666B1 (fr) 1980-05-19 1980-05-19 Liaison mecanique et isolante entre une tuyere et l'enveloppe bobinee de la chambre de combustion d'un propulseur

Publications (1)

Publication Number Publication Date
CA1175241A true CA1175241A (en) 1984-10-02

Family

ID=9242102

Family Applications (1)

Application Number Title Priority Date Filing Date
CA000377798A Expired CA1175241A (en) 1980-05-19 1981-05-19 Mechanical and insulating connection between a nozzle and the filament-wound casing of the combustion chamber of a rocket motor

Country Status (6)

Country Link
JP (1) JPS5716239A (enrdf_load_stackoverflow)
CA (1) CA1175241A (enrdf_load_stackoverflow)
DE (1) DE3119712A1 (enrdf_load_stackoverflow)
FR (1) FR2482666B1 (enrdf_load_stackoverflow)
GB (1) GB2076061B (enrdf_load_stackoverflow)
IT (1) IT1135847B (enrdf_load_stackoverflow)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2706183B1 (fr) * 1993-06-07 1995-09-01 Europ Propulsion Dispositif de purge de résidus de combustion.
RU2108476C1 (ru) * 1996-01-24 1998-04-10 Акционерное общество "Центральный научно-исследовательский институт специального машиностроения" Корпус рдтт из композиционных материалов
DE19915082C1 (de) * 1999-04-01 2000-07-13 Daimler Chrysler Ag Verfahren zur Herstellung einer gekühlten Düse für ein Raketentriebwerk
RU2153092C1 (ru) * 1999-04-19 2000-07-20 Государственное унитарное предприятие Конструкторское бюро приборостроения Ракетный двигатель твердого топлива
RU2166660C1 (ru) * 2000-08-11 2001-05-10 Федеральное государственное унитарное предприятие "Пермский завод им. С.М. Кирова" Заряд ракетного твердого топлива
RU2174619C1 (ru) * 2000-11-09 2001-10-10 Федеральный центр двойных технологий "Союз" Корпус ракетного двигателя твердого топлива типа "кокон"
RU2189483C2 (ru) * 2000-11-22 2002-09-20 Государственное унитарное предприятие "Конструкторское бюро приборостроения" Ракетный двигатель твердого топлива
RU2192554C1 (ru) * 2001-06-06 2002-11-10 Федеральный центр двойных технологий "Союз" Заряд, скрепленный с корпусом ракетного двигателя твердого топлива
RU2239083C1 (ru) * 2003-01-09 2004-10-27 Государственное унитарное предприятие "Конструкторское бюро приборостроения" Ракетный двигатель твердого топлива
US11028802B2 (en) * 2016-11-14 2021-06-08 Northrop Grumman Systems Corporation Liquid rocket engine assemblies and related methods
RU2746081C1 (ru) * 2020-02-11 2021-04-06 Акционерное общество "Опытное конструкторское бюро "Новатор" Вкладыш соплового блока ракетного двигателя твердого топлива из углерод-кремнеземного композиционного материала
CN113250858A (zh) * 2021-04-21 2021-08-13 西安英利科电气科技有限公司 一种大开口固体火箭燃烧室的缠绕结构及方法

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3228186A (en) * 1962-08-27 1966-01-11 Thiokol Chemical Corp Combination self-restraining nozzle and exit cone for solid propellant rocket motors
US3212257A (en) * 1964-10-23 1965-10-19 Hercules Powder Co Ltd Rocket motor
US3648461A (en) * 1970-05-13 1972-03-14 Nasa Solid propellent rocket motor nozzle
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

Also Published As

Publication number Publication date
GB2076061B (en) 1983-09-07
DE3119712A1 (de) 1982-03-04
FR2482666A1 (fr) 1981-11-20
IT1135847B (it) 1986-08-27
JPS5716239A (en) 1982-01-27
GB2076061A (en) 1981-11-25
IT8121782A0 (it) 1981-05-18
JPS64586B2 (enrdf_load_stackoverflow) 1989-01-06
DE3119712C2 (enrdf_load_stackoverflow) 1992-02-06
FR2482666B1 (fr) 1985-06-21

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Legal Events

Date Code Title Description
MKEX Expiry