IT1135847B - Dispositivo di collegamento meccanico e isolante fra un ugello e l'involucro avvolto della camera di combustione di un propulsore - Google Patents

Dispositivo di collegamento meccanico e isolante fra un ugello e l'involucro avvolto della camera di combustione di un propulsore

Info

Publication number
IT1135847B
IT1135847B IT21782/81A IT2178281A IT1135847B IT 1135847 B IT1135847 B IT 1135847B IT 21782/81 A IT21782/81 A IT 21782/81A IT 2178281 A IT2178281 A IT 2178281A IT 1135847 B IT1135847 B IT 1135847B
Authority
IT
Italy
Prior art keywords
propulsor
nozzle
mechanical
combustion chamber
connection device
Prior art date
Application number
IT21782/81A
Other languages
English (en)
Italian (it)
Other versions
IT8121782A0 (it
Inventor
Paul Donguy
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 IT8121782A0 publication Critical patent/IT8121782A0/it
Application granted granted Critical
Publication of IT1135847B publication Critical patent/IT1135847B/it

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
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32—Constructional parts; Details not otherwise provided for
    • 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
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32—Constructional parts; Details not otherwise provided for
    • F02K9/34—Casings; Combustion chambers; Liners thereof
    • F02K9/343—Joints, connections, seals therefor
    • 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)
  • Thermal Insulation (AREA)
  • Ceramic Products (AREA)
IT21782/81A 1980-05-19 1981-05-18 Dispositivo di collegamento meccanico e isolante fra un ugello e l'involucro avvolto della camera di combustione di un propulsore IT1135847B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
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 (2)

Publication Number Publication Date
IT8121782A0 IT8121782A0 (it) 1981-05-18
IT1135847B true IT1135847B (it) 1986-08-27

Family

ID=9242102

Family Applications (1)

Application Number Title Priority Date Filing Date
IT21782/81A IT1135847B (it) 1980-05-19 1981-05-18 Dispositivo di collegamento meccanico e isolante fra un ugello e l'involucro avvolto della camera di combustione di un propulsore

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
DE3119712A1 (de) 1982-03-04
FR2482666B1 (fr) 1985-06-21
DE3119712C2 (enrdf_load_stackoverflow) 1992-02-06
GB2076061A (en) 1981-11-25
GB2076061B (en) 1983-09-07
CA1175241A (en) 1984-10-02
JPS64586B2 (enrdf_load_stackoverflow) 1989-01-06
IT8121782A0 (it) 1981-05-18
FR2482666A1 (fr) 1981-11-20
JPS5716239A (en) 1982-01-27

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