EG20054A - Allumeur fixable dans la tuyere d'un propulseur - Google Patents

Allumeur fixable dans la tuyere d'un propulseur

Info

Publication number
EG20054A
EG20054A EG8287A EG8287A EG20054A EG 20054 A EG20054 A EG 20054A EG 8287 A EG8287 A EG 8287A EG 8287 A EG8287 A EG 8287A EG 20054 A EG20054 A EG 20054A
Authority
EG
Egypt
Prior art keywords
thruster nozzle
igniter
fixed
fixed igniter
thruster
Prior art date
Application number
EG8287A
Other languages
English (en)
French (fr)
Original Assignee
Poudres & Explosifs Ste Nale
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 Poudres & Explosifs Ste Nale filed Critical Poudres & Explosifs Ste Nale
Application granted granted Critical
Publication of EG20054A publication Critical patent/EG20054A/xx

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B3/00—Blasting cartridges, i.e. case and explosive
    • F42B3/26—Arrangements for mounting initiators; Accessories therefor, e.g. tools
    • 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
    • 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
    • F02K9/978—Closures for nozzles; Nozzles comprising ejectable or discardable elements

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Air Bags (AREA)
  • Lighters Containing Fuel (AREA)
  • Portable Nailing Machines And Staplers (AREA)
EG8287A 1986-02-21 1987-02-16 Allumeur fixable dans la tuyere d'un propulseur EG20054A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8602378A FR2594891B1 (fr) 1986-02-21 1986-02-21 Allumeur fixable dans la tuyere d'un propulseur

Publications (1)

Publication Number Publication Date
EG20054A true EG20054A (fr) 1997-05-31

Family

ID=9332372

Family Applications (1)

Application Number Title Priority Date Filing Date
EG8287A EG20054A (fr) 1986-02-21 1987-02-16 Allumeur fixable dans la tuyere d'un propulseur

Country Status (5)

Country Link
US (1) US4751881A (xx)
EP (1) EP0235028B1 (xx)
DE (1) DE3762367D1 (xx)
EG (1) EG20054A (xx)
FR (1) FR2594891B1 (xx)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5062206A (en) * 1987-10-26 1991-11-05 Thiokol Corporation Removable rocket motor igniter
US5007236A (en) * 1987-10-26 1991-04-16 Morton Thiokol, Inc. Removable rocket motor igniter
US5410966A (en) * 1992-03-26 1995-05-02 Centuri Corporation High reliability model rocket engine igniter system
US5509354A (en) * 1992-03-26 1996-04-23 Centuri Corporation Igniter holder
DE29608194U1 (de) * 1996-05-06 1996-10-02 Trw Repa Gmbh Elektrischer Zünder eines pyrotechnischen Gasgenerators
US6481198B1 (en) 1999-07-09 2002-11-19 Alliant Techsystems Inc. Multi-stage rocket motor assembly including jettisonable launch motor integrated with flight igniter
US7284487B2 (en) * 2004-07-06 2007-10-23 United States Of America As Represented By The Secretary Of The Army Single-piece stereolithographically-produced missile igniter
US7784404B2 (en) * 2007-11-01 2010-08-31 Alliant Techsystems Inc. Dual fault safe and arm device, adaptive structures therewith and safety and reliability features therefor
CN104712458B (zh) * 2013-12-13 2016-07-06 航宇救生装备有限公司 能尾部点火的固体燃料火箭发动机
KR101878552B1 (ko) * 2016-06-15 2018-07-13 주식회사 한화 노즐 마개형 점화기 마운트 및 그 설치 방법
KR101872587B1 (ko) * 2016-06-15 2018-06-28 주식회사 한화 디스크형 점화기 마운트 조립체 및 그 설치 방법

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
LU31272A1 (xx) *
US2776623A (en) * 1949-08-06 1957-01-08 Hercules Powder Co Ltd Closure device
US2720749A (en) * 1950-01-31 1955-10-18 Hughes Aircraft Co Nozzle closure assembly
US3221495A (en) * 1960-03-28 1965-12-07 United Aircraft Corp Thrust cut-off and thrust reversal system
US3304865A (en) * 1965-04-21 1967-02-21 Robert L Gungle Self-sealing, unbonded, rocket motor nozzle closure
US3583162A (en) * 1969-03-07 1971-06-08 Thiokol Chemical Corp Closure and solid propellant grain support for a solid propellant rocket motor
US3910191A (en) * 1974-05-07 1975-10-07 Us Army Variable pressure nozzle closure
CA1036419A (en) * 1975-08-25 1978-08-15 Fred A. Christie Aft-end ignition system for rocket motor
FR2353040A1 (fr) * 1976-05-25 1977-12-23 Europ Propulsion Allumeur pour bloc de poudres propulsives
CA1079078A (en) * 1977-05-25 1980-06-10 Michael N. Clark Rocket nozzle assembly
CA1217944A (en) * 1983-03-16 1987-02-17 Christian J.L. Carrier Integrated weatherseal/igniter for solid rocket motor

Also Published As

Publication number Publication date
EP0235028A1 (fr) 1987-09-02
DE3762367D1 (de) 1990-05-23
US4751881A (en) 1988-06-21
FR2594891A1 (fr) 1987-08-28
FR2594891B1 (fr) 1989-10-13
EP0235028B1 (fr) 1990-04-18

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