NO874599L - Fremgangsmaate for fremstilling av et forbrenningskammer for rakettmotor med fast drivstoff. - Google Patents

Fremgangsmaate for fremstilling av et forbrenningskammer for rakettmotor med fast drivstoff.

Info

Publication number
NO874599L
NO874599L NO874599A NO874599A NO874599L NO 874599 L NO874599 L NO 874599L NO 874599 A NO874599 A NO 874599A NO 874599 A NO874599 A NO 874599A NO 874599 L NO874599 L NO 874599L
Authority
NO
Norway
Prior art keywords
procedure
preparation
solid fuel
rocket engine
combustion combustor
Prior art date
Application number
NO874599A
Other languages
English (en)
Other versions
NO171648C (no
NO171648B (no
NO874599D0 (no
Inventor
Dino Crapiz
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 NO874599D0 publication Critical patent/NO874599D0/no
Publication of NO874599L publication Critical patent/NO874599L/no
Publication of NO171648B publication Critical patent/NO171648B/no
Publication of NO171648C publication Critical patent/NO171648C/no

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
    • F02K9/34—Casings; Combustion chambers; Liners thereof

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
  • Solid Fuels And Fuel-Associated Substances (AREA)
NO874599A 1986-11-05 1987-11-04 Fremgangsmaate for fremstilling av et forbrenningskammer for rakettmotor med fast drivstoff NO171648C (no)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8615426A FR2606082B1 (fr) 1986-11-05 1986-11-05 Chambre de combustion de propulseur a propergol solide, et procede pour sa fabrication

Publications (4)

Publication Number Publication Date
NO874599D0 NO874599D0 (no) 1987-11-04
NO874599L true NO874599L (no) 1988-05-06
NO171648B NO171648B (no) 1993-01-04
NO171648C NO171648C (no) 1993-04-14

Family

ID=9340554

Family Applications (1)

Application Number Title Priority Date Filing Date
NO874599A NO171648C (no) 1986-11-05 1987-11-04 Fremgangsmaate for fremstilling av et forbrenningskammer for rakettmotor med fast drivstoff

Country Status (8)

Country Link
US (1) US5032201A (no)
EP (1) EP0270412B1 (no)
JP (1) JPH0724899B2 (no)
DE (1) DE3770421D1 (no)
ES (1) ES2023428B3 (no)
FR (1) FR2606082B1 (no)
IL (1) IL84378A (no)
NO (1) NO171648C (no)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2863665B1 (fr) * 1988-10-12 2007-03-30 Aerospatiale Statoreacteur a structure tubulaire et missile propulse par un tel statoreacteur
DE4016220A1 (de) * 1990-05-19 1991-11-21 Dynamit Nobel Ag Feststoffraketenmotor
US5341638A (en) * 1992-03-09 1994-08-30 Thiokol Corporation Low cost segmented structure for pressure vessels, rocket motors, piping
RU2117811C1 (ru) * 1996-11-21 1998-08-20 Акционерное общество "Станкомаш" Способ защиты внутренней поверхности корпуса ракетного двигателя
FR2764646B1 (fr) * 1997-06-16 1999-07-16 Celerg Moteur, a propergol solide, de faible vulnerabilite
US6425172B1 (en) * 1999-04-23 2002-07-30 Dynetek Industries Ltd. Homogenizing process for fiber-wrapped structural composites
DE10043303B4 (de) * 2000-09-02 2004-06-09 Astrium Gmbh Raketentriebwerk in Segmentbauweise
RU2174619C1 (ru) * 2000-11-09 2001-10-10 Федеральный центр двойных технологий "Союз" Корпус ракетного двигателя твердого топлива типа "кокон"
RU2183758C1 (ru) * 2001-02-05 2002-06-20 Государственное унитарное предприятие "Научно-исследовательский институт полимерных материалов" Способ сборки ракетного двигателя твердого топлива
RU2256813C2 (ru) * 2003-08-28 2005-07-20 Открытое акционерное общество Научно-производственное объединение "Искра" Способ нанесения эластичного покрытия на внутреннюю поверхность корпуса
RU2274760C2 (ru) * 2004-06-30 2006-04-20 Федеральное государственное унитарное предприятие "Научно-исследовательский институт полимерных материалов" Способ снаряжения ракетного двигателя многошашечным зарядом твердого топлива
RU2322605C1 (ru) * 2006-08-16 2008-04-20 Государственное унитарное предприятие "Конструкторское бюро приборостроения" Ракетный двигатель
RU2322603C1 (ru) * 2007-04-02 2008-04-20 Федеральное казенное предприятие "Комбинат "Каменский" Заряд ракетного твердого топлива
KR101097787B1 (ko) * 2009-08-20 2011-12-23 국방과학연구소 추진제용 압력용기, 그 폭발 방지 방법 및 제조 방법
FR3011902B1 (fr) * 2013-10-16 2015-11-27 Herakles Procede de liaison d'une jupette a une enveloppe d'un corps de propulseur
CN109186375B (zh) * 2018-07-26 2020-12-11 西安航天动力技术研究所 一种复合材料固体火箭发动机中裙连接机构及成型方法

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE22661C (de) * W. E. WOODBRIDGE in Washington, V. St. A Konstruktion für Geschützrohre
FR921153A (fr) * 1945-10-31 1947-04-29 Controles Ind Et Tubes-moteurs pour projectiles-fusées et propulseurs de décollage d'avions
US2995011A (en) * 1959-09-17 1961-08-08 Phillips Petroleum Co Solid propellant rocket motor
US3224317A (en) * 1961-09-22 1965-12-21 Mb Assoc Method of constructing a miniature solid propellant rocket
US3188802A (en) * 1961-11-29 1965-06-15 Thiokol Chemical Corp Solid propellant grain
FR1356673A (fr) * 1962-05-10 1964-03-27 Thiokol Chemical Corp Moteur de roquette et méthode de construction
US3224191A (en) * 1963-05-20 1965-12-21 Thiokol Chemical Corp Rocket motor construction
US3301924A (en) * 1964-07-16 1967-01-31 Bryant Robert William Manufacture of rocket motors
US3426528A (en) * 1966-12-27 1969-02-11 Thiokol Chemical Corp Liner configuration for solid propellant rocket motors
FR2123036B1 (no) * 1969-11-24 1975-07-04 Neyrpic Creusot Loire
US4118928A (en) * 1973-07-12 1978-10-10 Thiokol Corporation Means for mounting solid propellant in a rocket motor
US3952506A (en) * 1973-11-07 1976-04-27 Thiokol Corporation Rocket motor construction
JPS5844518B2 (ja) * 1976-09-03 1983-10-04 ダイセル化学工業株式会社 ロケツトの外殻体
US4495764A (en) * 1983-05-26 1985-01-29 The United States Of America As Represented By The Secretary Of The Air Force Integrated insulation wall assembly
FR2552494B1 (fr) * 1983-09-26 1985-12-20 Europ Propulsion Procede de preparation de corps de propulseurs fusees
FR2593238B1 (fr) * 1986-01-22 1990-11-02 Europ Propulsion Chambre de combustion de propulseur et son procede d'assemblage

Also Published As

Publication number Publication date
EP0270412A1 (fr) 1988-06-08
DE3770421D1 (de) 1991-07-04
EP0270412B1 (fr) 1991-05-29
US5032201A (en) 1991-07-16
JPH0724899B2 (ja) 1995-03-22
NO171648C (no) 1993-04-14
NO171648B (no) 1993-01-04
ES2023428B3 (es) 1992-01-16
FR2606082A1 (fr) 1988-05-06
FR2606082B1 (fr) 1991-04-05
IL84378A0 (en) 1988-04-29
JPS6487035A (en) 1989-03-31
IL84378A (en) 1993-02-21
NO874599D0 (no) 1987-11-04

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