FR2445508A1 - Generateur pyrotechnique de gaz a faible duree de combustion comportant des rondelles de propergol entretoisees - Google Patents

Generateur pyrotechnique de gaz a faible duree de combustion comportant des rondelles de propergol entretoisees

Info

Publication number
FR2445508A1
FR2445508A1 FR7836725A FR7836725A FR2445508A1 FR 2445508 A1 FR2445508 A1 FR 2445508A1 FR 7836725 A FR7836725 A FR 7836725A FR 7836725 A FR7836725 A FR 7836725A FR 2445508 A1 FR2445508 A1 FR 2445508A1
Authority
FR
France
Prior art keywords
washers
deflectors
sepd
aiming
solid fuel
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.)
Granted
Application number
FR7836725A
Other languages
English (en)
Other versions
FR2445508B1 (fr
Inventor
Francis Dalet
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 Nationale des Poudres et Explosifs
Original Assignee
Societe Nationale des Poudres et Explosifs
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 Nationale des Poudres et Explosifs filed Critical Societe Nationale des Poudres et Explosifs
Priority to FR7836725A priority Critical patent/FR2445508A1/fr
Publication of FR2445508A1 publication Critical patent/FR2445508A1/fr
Application granted granted Critical
Publication of FR2445508B1 publication Critical patent/FR2445508B1/fr
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/30Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants with the propulsion gases exhausting through a plurality of nozzles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/10Shape or structure of solid propellant charges
    • F02K9/14Shape or structure of solid propellant charges made from sheet-like materials, e.g. of carpet-roll type, of layered structure

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)

Abstract

Générateur pyrotechnique de gaz à faible durée de combustion, destiné notament à être utilisé comme propulseur d'accélération d'un engin autopropulsé. Le générateur est muni d'un chargement pyrotechnique constitué de rondelles de propergol solide disposées sensiblement parallèlement les unes aux autres et ménageant au moins un canal longitudinal d'évacuation des gaz de combustion en direction d'au moins une tuyère, et se caractérise en ce que le chargement pyrotechnique est constitué de plusieurs ensembles 11 à 14 de rondelles de propergol séparés par des déflecteurs 8, 9, 10 qui sont disposés sensiblement parallèlement aux plaques de propergol et dont le bord 8a, 9a, 10a situé vers le canal longitudinal d'évacuation des gaz est en dépassement.
FR7836725A 1978-12-28 1978-12-28 Generateur pyrotechnique de gaz a faible duree de combustion comportant des rondelles de propergol entretoisees Granted FR2445508A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7836725A FR2445508A1 (fr) 1978-12-28 1978-12-28 Generateur pyrotechnique de gaz a faible duree de combustion comportant des rondelles de propergol entretoisees

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7836725A FR2445508A1 (fr) 1978-12-28 1978-12-28 Generateur pyrotechnique de gaz a faible duree de combustion comportant des rondelles de propergol entretoisees

Publications (2)

Publication Number Publication Date
FR2445508A1 true FR2445508A1 (fr) 1980-07-25
FR2445508B1 FR2445508B1 (fr) 1982-01-15

Family

ID=9216682

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7836725A Granted FR2445508A1 (fr) 1978-12-28 1978-12-28 Generateur pyrotechnique de gaz a faible duree de combustion comportant des rondelles de propergol entretoisees

Country Status (1)

Country Link
FR (1) FR2445508A1 (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2489419A1 (fr) * 1980-09-01 1982-03-05 Nippon Oils & Fats Co Ltd Grain de generateur de gaz et son procede de fabrication
FR2567197A1 (fr) * 1984-07-06 1986-01-10 Brandt Armements Propulseur a poudre pour projectile tire dans un tube de lancement
DE4228696A1 (de) * 1992-08-28 1994-03-03 Hs Tech & Design Pyrotechnischer Gasgenerator

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2510147A (en) * 1945-03-07 1950-06-06 Leslie A Skinner Side venting rocket
FR1015763A (fr) * 1950-03-31 1952-10-23 Soc Tech De Rech Ind Propulseur
FR1180590A (fr) * 1957-06-22 1959-06-05 Prb Nv Charges propulsives améliorées pour engins auto-propulsés
DE1170714B (de) * 1959-11-26 1964-05-21 Rheinmetall Gmbh Treibladung fuer Pulverraketen
FR2074801A1 (fr) * 1970-01-29 1971-10-08 Onera (Off Nat Aerospatiale)
FR2359981A1 (fr) * 1976-07-27 1978-02-24 Messerschmitt Boelkow Blohm Moteur-fusee a propergol solide

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2510147A (en) * 1945-03-07 1950-06-06 Leslie A Skinner Side venting rocket
FR1015763A (fr) * 1950-03-31 1952-10-23 Soc Tech De Rech Ind Propulseur
FR1180590A (fr) * 1957-06-22 1959-06-05 Prb Nv Charges propulsives améliorées pour engins auto-propulsés
DE1170714B (de) * 1959-11-26 1964-05-21 Rheinmetall Gmbh Treibladung fuer Pulverraketen
FR2074801A1 (fr) * 1970-01-29 1971-10-08 Onera (Off Nat Aerospatiale)
FR2359981A1 (fr) * 1976-07-27 1978-02-24 Messerschmitt Boelkow Blohm Moteur-fusee a propergol solide

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2489419A1 (fr) * 1980-09-01 1982-03-05 Nippon Oils & Fats Co Ltd Grain de generateur de gaz et son procede de fabrication
FR2567197A1 (fr) * 1984-07-06 1986-01-10 Brandt Armements Propulseur a poudre pour projectile tire dans un tube de lancement
DE4228696A1 (de) * 1992-08-28 1994-03-03 Hs Tech & Design Pyrotechnischer Gasgenerator

Also Published As

Publication number Publication date
FR2445508B1 (fr) 1982-01-15

Similar Documents

Publication Publication Date Title
ES444603A1 (es) Senuelo emisor elemental y procedimiento para su uso.
GB1541066A (en) Aircraft gas turbine engine flight manoeuverable exhaust nozzle
JPS5289717A (en) Fuel injector for gas turbine engine
FR2445508A1 (fr) Generateur pyrotechnique de gaz a faible duree de combustion comportant des rondelles de propergol entretoisees
JPS51127912A (en) Fuel injector for gas turbine engine
GB953260A (en) Air-breathing solid propellant ducted rocket
JPS5251270A (en) Ignition device with timer for firing a lighter
ES2019138B3 (es) Explosivo para cabezas de combate y combustible para misiles.
GB927675A (en) Improvements relating to jet propelled missiles
JPS5245741A (en) Waste gas combustion burner
GB961001A (en) Improvements in propulsion units having a plurality of reaction propulsion nozzles
CA1000067A (en) Lighter assembly with ignition by admixture of primary and secondary fuel
JPS52100800A (en) Electric fuse
JPS54120305A (en) Solid rocket engine in two-stage thrust mode
WARD et al. Laser ignition of pyrotechnic compositions being tested as drag-reducing fumers(Laser ignition of pyrotechnic compositions being considered as drag reducing fumers)
FR2141004A5 (en) Solid propellant igniter - for rockets with slow burning propellants
JPS5229532A (en) Fuel injection nozzle
CA824880A (en) Gas turbine engine afterburner fuel control and ignition
JPS529128A (en) Gun type burner
JPS5210912A (en) Method of discharging gas from tank
LHUILLIER et al. A study of the erosive burning of solid propellants
JPS5253113A (en) Burner, gas turbine engine
JPS5237609A (en) Engine without crank
JPS5252048A (en) Internal engine ignition timing control unit
JPS5253111A (en) Fuel burning method in a diesel engine

Legal Events

Date Code Title Description
ST Notification of lapse