JPS64586B2 - - Google Patents

Info

Publication number
JPS64586B2
JPS64586B2 JP56074343A JP7434381A JPS64586B2 JP S64586 B2 JPS64586 B2 JP S64586B2 JP 56074343 A JP56074343 A JP 56074343A JP 7434381 A JP7434381 A JP 7434381A JP S64586 B2 JPS64586 B2 JP S64586B2
Authority
JP
Japan
Prior art keywords
nozzle
casing
coupling
ring
coupling ring
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
JP56074343A
Other languages
English (en)
Japanese (ja)
Other versions
JPS5716239A (en
Inventor
Dangii Hooru
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.)
YUUROPEENU DO PUROPUYURUSHION SOC
Original Assignee
YUUROPEENU DO PUROPUYURUSHION SOC
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 YUUROPEENU DO PUROPUYURUSHION SOC filed Critical YUUROPEENU DO PUROPUYURUSHION SOC
Publication of JPS5716239A publication Critical patent/JPS5716239A/ja
Publication of JPS64586B2 publication Critical patent/JPS64586B2/ja
Granted 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
    • F02K9/08—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)
JP7434381A 1980-05-19 1981-05-19 Casing nozzle combination structure Granted JPS5716239A (en)

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
JPS5716239A JPS5716239A (en) 1982-01-27
JPS64586B2 true JPS64586B2 (enrdf_load_stackoverflow) 1989-01-06

Family

ID=9242102

Family Applications (1)

Application Number Title Priority Date Filing Date
JP7434381A Granted JPS5716239A (en) 1980-05-19 1981-05-19 Casing nozzle combination structure

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
DE3119712C2 (enrdf_load_stackoverflow) 1992-02-06
CA1175241A (en) 1984-10-02
FR2482666B1 (fr) 1985-06-21

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