FR2433169A1 - Ejector-igniter for tactical missiles - incorporates several pyrotechnic compsns. stacked in tiers in receptacle each having appropriate function - Google Patents

Ejector-igniter for tactical missiles - incorporates several pyrotechnic compsns. stacked in tiers in receptacle each having appropriate function

Info

Publication number
FR2433169A1
FR2433169A1 FR7823380A FR7823380A FR2433169A1 FR 2433169 A1 FR2433169 A1 FR 2433169A1 FR 7823380 A FR7823380 A FR 7823380A FR 7823380 A FR7823380 A FR 7823380A FR 2433169 A1 FR2433169 A1 FR 2433169A1
Authority
FR
France
Prior art keywords
ejector
igniter
tiers
stacked
receptacle
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.)
Withdrawn
Application number
FR7823380A
Other languages
French (fr)
Inventor
Michel Reichard
Bernard Luscan
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.)
Societe Europeenne de Propulsion SEP SA
Original Assignee
Societe Europeenne de Propulsion SEP 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 Societe Europeenne de Propulsion SEP SA filed Critical Societe Europeenne de Propulsion SEP SA
Priority to FR7823380A priority Critical patent/FR2433169A1/en
Publication of FR2433169A1 publication Critical patent/FR2433169A1/en
Withdrawn legal-status Critical Current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
    • F02K9/97—Rocket nozzles
    • F02K9/978—Closures for nozzles; Nozzles comprising ejectable or discardable elements
    • 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
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/36—Means for interconnecting rocket-motor and body section; Multi-stage connectors; Disconnecting means

Abstract

A pyrotechnic ejector-igniter device includes means of ejecting a mass and means of igniting a charge placed in the mass. It comprises a unitary receptacle in which several pyrotechnic compsn. are stacked in tiers. Each realises an function. Allows the realisation of an ejector-igniter assembly which ensures the whole sequence of the propellant from the single order to fire the ejector. The invention also realises an ignition system which is easily incorporated in a tactical missile.
FR7823380A 1978-08-08 1978-08-08 Ejector-igniter for tactical missiles - incorporates several pyrotechnic compsns. stacked in tiers in receptacle each having appropriate function Withdrawn FR2433169A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7823380A FR2433169A1 (en) 1978-08-08 1978-08-08 Ejector-igniter for tactical missiles - incorporates several pyrotechnic compsns. stacked in tiers in receptacle each having appropriate function

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7823380A FR2433169A1 (en) 1978-08-08 1978-08-08 Ejector-igniter for tactical missiles - incorporates several pyrotechnic compsns. stacked in tiers in receptacle each having appropriate function

Publications (1)

Publication Number Publication Date
FR2433169A1 true FR2433169A1 (en) 1980-03-07

Family

ID=9211698

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7823380A Withdrawn FR2433169A1 (en) 1978-08-08 1978-08-08 Ejector-igniter for tactical missiles - incorporates several pyrotechnic compsns. stacked in tiers in receptacle each having appropriate function

Country Status (1)

Country Link
FR (1) FR2433169A1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2791130A1 (en) * 1999-03-19 2000-09-22 Celerg MACHINE PROVIDED WITH A WIDE PYROTECHNIC EJECTOR
RU2620613C1 (en) * 2016-04-19 2017-05-29 Федеральное государственное автономное образовательное учреждение высшего образования "Национальный исследовательский Томский государственный университет" (ТГУ) Rocket engine of rocket-assisted projectile
RU2647256C1 (en) * 2017-04-17 2018-03-15 Федеральное государственное автономное образовательное учреждение высшего образования "Национальный исследовательский Томский государственный университет" (НИ ТГУ) Method of increasing the distance of the rocket-propelled grenade

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1011030A (en) * 1948-11-24 1952-06-18 Self-regulating ignition relay for multi-stage powder rockets
DE1132471B (en) * 1958-02-03 1962-06-28 Hotchkiss Brandt Safety and delay device for terminating the propellant charge of a rocket
DE1200172B (en) * 1960-09-23 1965-09-02 Hotchkiss Brandt Missile projectile with ejectable delay device

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1011030A (en) * 1948-11-24 1952-06-18 Self-regulating ignition relay for multi-stage powder rockets
DE1132471B (en) * 1958-02-03 1962-06-28 Hotchkiss Brandt Safety and delay device for terminating the propellant charge of a rocket
DE1200172B (en) * 1960-09-23 1965-09-02 Hotchkiss Brandt Missile projectile with ejectable delay device

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2791130A1 (en) * 1999-03-19 2000-09-22 Celerg MACHINE PROVIDED WITH A WIDE PYROTECHNIC EJECTOR
DE10013745C2 (en) * 1999-03-19 2002-12-05 Celerg Immeuble Jura Ct D Affa Missile equipped with a detachable, pyrotechnic ejector
RU2620613C1 (en) * 2016-04-19 2017-05-29 Федеральное государственное автономное образовательное учреждение высшего образования "Национальный исследовательский Томский государственный университет" (ТГУ) Rocket engine of rocket-assisted projectile
RU2647256C1 (en) * 2017-04-17 2018-03-15 Федеральное государственное автономное образовательное учреждение высшего образования "Национальный исследовательский Томский государственный университет" (НИ ТГУ) Method of increasing the distance of the rocket-propelled grenade

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Legal Events

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