DE60114066D1 - Mehrstufenraketenmotor mit einer Interstufen-Schutzvorrichtung - Google Patents

Mehrstufenraketenmotor mit einer Interstufen-Schutzvorrichtung

Info

Publication number
DE60114066D1
DE60114066D1 DE60114066T DE60114066T DE60114066D1 DE 60114066 D1 DE60114066 D1 DE 60114066D1 DE 60114066 T DE60114066 T DE 60114066T DE 60114066 T DE60114066 T DE 60114066T DE 60114066 D1 DE60114066 D1 DE 60114066D1
Authority
DE
Germany
Prior art keywords
interstage
protection device
rocket motor
stage rocket
pyrotechnic
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 - Lifetime
Application number
DE60114066T
Other languages
English (en)
Other versions
DE60114066T2 (de
Inventor
Claude Guillet
Christophe Hermez
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.)
Roxel France SA
Original Assignee
Roxel France SA
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 Roxel France SA filed Critical Roxel France SA
Application granted granted Critical
Publication of DE60114066D1 publication Critical patent/DE60114066D1/de
Publication of DE60114066T2 publication Critical patent/DE60114066T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F02K9/28—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants having two or more propellant charges with the propulsion gases exhausting through a common nozzle
    • 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
    • F02K9/95—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by starting or ignition means or arrangements

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Air Bags (AREA)
  • Feeding, Discharge, Calcimining, Fusing, And Gas-Generation Devices (AREA)
  • Component Parts Of Construction Machinery (AREA)
  • Control Of Turbines (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Ignition Installations For Internal Combustion Engines (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
DE60114066T 2000-03-01 2001-02-23 Mehrstufenraketenmotor mit einer Interstufen-Schutzvorrichtung Expired - Lifetime DE60114066T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0002634 2000-03-01
FR0002634A FR2805855B1 (fr) 2000-03-01 2000-03-01 Moteur autopropulse a plusieurs etages et systeme de separation situe entre deux etages consecutifs

Publications (2)

Publication Number Publication Date
DE60114066D1 true DE60114066D1 (de) 2006-03-02
DE60114066T2 DE60114066T2 (de) 2006-07-13

Family

ID=8847598

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60114066T Expired - Lifetime DE60114066T2 (de) 2000-03-01 2001-02-23 Mehrstufenraketenmotor mit einer Interstufen-Schutzvorrichtung

Country Status (4)

Country Link
EP (1) EP1138923B1 (de)
AT (1) ATE307282T1 (de)
DE (1) DE60114066T2 (de)
FR (1) FR2805855B1 (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8291691B2 (en) 2007-08-02 2012-10-23 Aerojet-General Corporation Multi-functional pulse-divided rocket
CN108060990A (zh) * 2016-11-07 2018-05-22 贾海亮 一种串联单机固体发动机
CN107529585B (zh) * 2017-03-30 2023-05-05 内蒙动力机械研究所 一种适用于多脉冲固体火箭发动机的熔膜式隔板
FR3087227A1 (fr) * 2018-10-12 2020-04-17 Roxel France Fond intermediaire pour enceinte sous pression
RU2704058C9 (ru) * 2018-11-20 2019-12-18 Акционерное общество "Машиностроительное конструкторское бюро "Искра" имени Ивана Ивановича Картукова" (АО "МКБ "Искра") Разделительное днище многоимпульсного ракетного двигателя на твердом топливе
RU2715453C1 (ru) * 2019-05-23 2020-02-28 Акционерное общество "Машиностроительное конструкторское бюро "Искра" имени Ивана Ивановича Картукова" (АО "МКБ "Искра") Многорежимный ракетный двигатель твердого топлива
RU2715450C1 (ru) * 2019-05-24 2020-02-28 Акционерное общество "Машиностроительное конструкторское бюро "Искра" имени Ивана Ивановича Картукова" (АО "МКБ "Искра") Многорежимный ракетный двигатель
CN111022217B (zh) * 2019-11-01 2021-05-14 湖北三江航天红林探控有限公司 一种用于双脉冲燃发器的级间隔离导通装置
US11988172B2 (en) 2020-11-19 2024-05-21 Raytheon Company Ignition safety device for a multi-pulse or multi-stage rocket motor system
RU208720U1 (ru) * 2021-06-15 2022-01-11 Федеральное государственное бюджетное учреждение "Центральный научно-исследовательский испытательный институт инженерных войск имени Героя Советского Союза генерал-лейтенанта инженерных войск Д.М. Карбышева" Министерства обороны Российской Федерации Ракетный двигатель твердого топлива с отсекателем пороховых газов
CN113638822B (zh) * 2021-06-30 2023-12-29 西安航天动力测控技术研究所 一种固体火箭发动机后裙连接机械臂式级间分离试验装置

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3568448A (en) * 1969-04-01 1971-03-09 Thiokol Chemical Corp Ignition system for igniting a gas generator by the use of combustion gases from a solid propellant rocket motor having selective zoning capabilities
US4864817A (en) * 1983-05-26 1989-09-12 Morton Thiokol, Inc. Membrane seal for application to pulsed rocket motor
CA1235582A (en) * 1984-10-29 1988-04-26 Donald L. Smith Solid rocket motor with dual interrrupted thrust
US5613358A (en) 1990-09-26 1997-03-25 Thiokol Corporation Reduced cost membrane seal assembly for pulsed rocket motor
US5419118A (en) * 1994-01-19 1995-05-30 Universal Propulsion Company, Inc. Multi-stage rocket motors
DE69517689T2 (de) * 1994-04-29 2000-10-19 Cordant Technologies Inc., Ogden Zweiphasiger feststoffraketenmotor

Also Published As

Publication number Publication date
FR2805855B1 (fr) 2002-09-13
DE60114066T2 (de) 2006-07-13
EP1138923B1 (de) 2005-10-19
FR2805855A1 (fr) 2001-09-07
EP1138923A1 (de) 2001-10-04
ATE307282T1 (de) 2005-11-15

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