DE69014795D1 - Brennbarer Anzünder für einen Raketenmotor mit festem Treibstoff. - Google Patents

Brennbarer Anzünder für einen Raketenmotor mit festem Treibstoff.

Info

Publication number: DE69014795D1
Authority: DE; Germany
Prior art keywords: solid fuel; rocket engine; flammable; lighter; flammable lighter
Prior art date: 1989-09-19
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 - Fee Related

Application number

DE69014795T

Other languages

English (en)

Other versions

DE69014795T2 (de

Inventor

Herman Fedde Rein Schoeyer

Guido Borso

Salvatore Gibilisco

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.)

Agence Spatiale Europeenne

Original Assignee

Agence Spatiale Europeenne

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.)

1989-09-19

Filing date

1990-09-11

Publication date

1995-01-19

1990-09-11 Application filed by Agence Spatiale Europeenne filed Critical Agence Spatiale Europeenne

1995-01-19 Publication of DE69014795D1 publication Critical patent/DE69014795D1/de

1995-04-13 Application granted granted Critical

1995-04-13 Publication of DE69014795T2 publication Critical patent/DE69014795T2/de

2010-09-12 Anticipated expiration legal-status Critical

Status Expired - Fee Related legal-status Critical Current

Classifications

- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C19/00—Details of fuzes
- F42C19/08—Primers; Detonators
- F42C19/0819—Primers or igniters for the initiation of rocket motors, i.e. pyrotechnical aspects thereof
- 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)
General Engineering & Computer Science (AREA)
Chemical & Material Sciences (AREA)
Combustion & Propulsion (AREA)
Mechanical Engineering (AREA)
Air Bags (AREA)
Testing Of Engines (AREA)

DE69014795T 1989-09-19 1990-09-11 Brennbarer Anzünder für einen Raketenmotor mit festem Treibstoff. Expired - Fee Related DE69014795T2 (de)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
FR8912255A FR2652125B1 (fr)	1989-09-19	1989-09-19	Allumeur consumable pour moteur-fusee a perpergol solide.

Publications (2)

Publication Number	Publication Date
DE69014795D1 true DE69014795D1 (de)	1995-01-19
DE69014795T2 DE69014795T2 (de)	1995-04-13

Family

ID=9385624

Family Applications (2)

Application Number	Title	Priority Date	Filing Date
DE69014795T Expired - Fee Related DE69014795T2 (de)	1989-09-19	1990-09-11	Brennbarer Anzünder für einen Raketenmotor mit festem Treibstoff.
DE199090402490T Pending DE419319T1 (de)	1989-09-19	1990-09-11	Brennbarer anzuender fuer einen raketenmotor mit festem treibstoff.

Family Applications After (1)

Application Number	Title	Priority Date	Filing Date
DE199090402490T Pending DE419319T1 (de)	1989-09-19	1990-09-11	Brennbarer anzuender fuer einen raketenmotor mit festem treibstoff.

Country Status (6)

Country	Link
US (1)	US5113763A (de)
EP (1)	EP0419319B1 (de)
JP (1)	JP2927922B2 (de)
CA (1)	CA2024520C (de)
DE (2)	DE69014795T2 (de)
FR (1)	FR2652125B1 (de)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
FR2733314B1 (fr) *	1995-04-20	1997-06-06	Aerospatiale	Dispositif d'allumage pyrotechnique pour un generateur de gaz
US5845933A (en) *	1996-12-24	1998-12-08	Autoliv Asp, Inc.	Airbag inflator with consumable igniter tube
JP3329695B2 (ja)	1997-06-10	2002-09-30	松下電送システム株式会社	同報通信方法及び通信装置
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
US8671840B2 (en) *	2011-01-28	2014-03-18	The United States Of America As Represented By The Secretary Of The Navy	Flexible fragmentation sleeve
US10995578B2 (en) *	2015-10-21	2021-05-04	Schlumberger Technology Corporation	Shearable deployment bar with ballistic transfer

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US2693757A (en) *	1950-10-10	1954-11-09	Energa	Safety device for self-propelled projectiles
US2952876A (en) *	1957-12-26	1960-09-20	Phillips Petroleum Co	Extrusion of solid rocket grains
US3048968A (en) *	1958-01-02	1962-08-14	Phillips Petroleum Co	Rocket motor
US3148505A (en) *	1960-01-04	1964-09-15	North American Aviation Inc	Radially firing pyrotechnic igniter
US3103784A (en) *	1960-11-15	1963-09-17	Ronald F Vetter	Plastic internal rocket nozzle
US3570364A (en) *	1961-11-08	1971-03-16	Joseph G Thibodaux Jr	Method of making a solid propellant rocket motor
US3392673A (en) *	1967-05-29	1968-07-16	Navy Usa	Consumable pyrogen igniter
US3855789A (en) *	1968-04-05	1974-12-24	Us Navy	Explosive coupling assembly
US4080901A (en) *	1976-04-20	1978-03-28	The United States Of America As Represented By The Aministrator Of The National Aeronautics And Space Administration	Molded composite pyrogen igniter for rocket motors
US4311005A (en) *	1979-05-11	1982-01-19	Raytheon Company	Rocket motor
US4503773A (en) *	1982-12-27	1985-03-12	Thiokol Corporation	Aft end igniter for full, head-end web solid propellant rocket motors
US4498292A (en) *	1983-02-02	1985-02-12	Thiokol Corporation	Igniter for rocket motors
JPS6019951A (ja) *	1983-07-14	1985-02-01	Nissan Motor Co Ltd	ロケツトモ−タの点火装置
US4574699A (en) *	1983-11-17	1986-03-11	Thiokol Corporation	Extendible wafer igniter with perforations adjacent the foot portion
JPS62299531A (ja) *	1986-06-11	1987-12-26	旭化成株式会社	低旋回性被覆弾性糸及びその製造方法
JPS62299532A (ja) *	1986-06-11	1987-12-26	旭化成株式会社	低旋回性の被覆弾性糸及びその製造方法
US4911795A (en) *	1987-08-14	1990-03-27	Morton Thiokol, Inc.	Method of preserving a composite material cased solid propellant rocket motor
US4901642A (en) *	1988-10-27	1990-02-20	Morton Thiokol, Inc.	Consumable wafer igniter

1989
- 1989-09-19 FR FR8912255A patent/FR2652125B1/fr not_active Expired - Lifetime
1990
- 1990-09-04 CA CA002024520A patent/CA2024520C/fr not_active Expired - Lifetime
- 1990-09-11 DE DE69014795T patent/DE69014795T2/de not_active Expired - Fee Related
- 1990-09-11 EP EP90402490A patent/EP0419319B1/de not_active Expired - Lifetime
- 1990-09-11 DE DE199090402490T patent/DE419319T1/de active Pending
- 1990-09-17 US US07/583,836 patent/US5113763A/en not_active Expired - Lifetime
- 1990-09-18 JP JP2249900A patent/JP2927922B2/ja not_active Expired - Lifetime

Also Published As

Publication number	Publication date
FR2652125A1 (fr)	1991-03-22
FR2652125B1 (fr)	1992-01-10
CA2024520A1 (fr)	1991-03-20
DE69014795T2 (de)	1995-04-13
DE419319T1 (de)	1991-09-05
JP2927922B2 (ja)	1999-07-28
CA2024520C (fr)	1998-08-11
EP0419319B1 (de)	1994-12-07
EP0419319A1 (de)	1991-03-27
JPH03130566A (ja)	1991-06-04
US5113763A (en)	1992-05-19

Similar Documents

Publication	Publication Date	Title
GB2206159B (en)	1992-02-19	A gas turbine engine having a dual manifold fuel system.
DE69004636D1 (de)	1993-12-23	Schubumkehrvorrichtung für ein Strahltriebwerk.
DE68912401D1 (de)	1994-03-03	Brenner für staubförmigen Brennstoff.
DE58901419D1 (de)	1992-06-17	Kraftstoffe fuer verbrennungsmaschinen.
DE3876971D1 (de)	1993-02-04	Kraftstoffeinspritzventil fuer einen motor.
DE69010061D1 (de)	1994-07-28	Brennstoffeinspritzeinrichtung für Dieselmotoren.
DE68901357D1 (de)	1992-06-04	Kombinationstriebwerk, rakete mit luftatmendem turbinenstrahltriebwerk.
DE69007899D1 (de)	1994-05-11	Brennraum für Diesel-Brennkraftmaschine.
DE69014121D1 (de)	1994-12-15	Brennstoffschiene für motortyp-v.
DE3872003D1 (de)	1992-07-23	Einspritzsystem fuer einen zweibrennstoffmotor.
BR8100370A (pt)	1981-08-11	Conjunto para injecao de combustivel de ignicao, por um lado, e combustivel principal, de dificil ignicao, por outro lado, destinado a motores diesel
DE69724179D1 (de)	2003-09-25	Schubumkehrvorrichtung für ein Zweikreistriebwerk mit Klappen am Triebwerksgehäuse
DE68902346D1 (de)	1992-09-10	Kraftstoffeinspritzventil fuer einspritzmotoren.
DE68901086D1 (de)	1992-04-30	Anlasser fuer einen verbrennungsmotor.
DE68905502D1 (de)	1993-04-29	Brennstoffeinspritzventil.
DE3751675D1 (de)	1996-02-22	Brennstoffeinspritzung für d.i.-dieselmotor mit mehreren düsen
DE68912995D1 (de)	1994-03-24	Kraftstoffeinspritzventil.
DE69204075D1 (de)	1995-09-14	Kraftstoffeinspritzventil für verbrennungsmotoren.
DE58907476D1 (de)	1994-05-19	Brennelementabzug für einen kugelhaufenkernreaktor.
DE69505899D1 (de)	1998-12-17	Schubumkehrvorrichtung für ein Zweikreistriebwerk mit Klappen am Triebwerksgehäuse
ES548810A0 (es)	1987-06-01	Un aparato para la combustion de combustible carbonoso.
DE69014795D1 (de)	1995-01-19	Brennbarer Anzünder für einen Raketenmotor mit festem Treibstoff.
DE68915621D1 (de)	1994-07-07	Gasfeuerzeug mit innerer Verbrennung.
DE69006939D1 (de)	1994-04-07	Kraftstoffeinspritzregelsystem für einen Dieselmotor.
DE69100985D1 (de)	1994-02-24	Brennstoffversorgungssystem für einen Turbomotor.

Legal Events

Date	Code	Title	Description
1996-01-11	8364	No opposition during term of opposition
2001-10-11	8339	Ceased/non-payment of the annual fee