FR2684723B1 - Propulseur a propergol solide a poussee modulable et missile equipe. - Google Patents

Propulseur a propergol solide a poussee modulable et missile equipe.

Info

Publication number
FR2684723B1
FR2684723B1 FR9115271A FR9115271A FR2684723B1 FR 2684723 B1 FR2684723 B1 FR 2684723B1 FR 9115271 A FR9115271 A FR 9115271A FR 9115271 A FR9115271 A FR 9115271A FR 2684723 B1 FR2684723 B1 FR 2684723B1
Authority
FR
France
Prior art keywords
propeller
missile equipped
modular push
solid propergol
propergol
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 - Fee Related
Application number
FR9115271A
Other languages
English (en)
Other versions
FR2684723A1 (fr
Inventor
Dominique Cahuzac
Jacques Perrin
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.)
Thales SA
Original Assignee
Thomson CSF 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 Thomson CSF SA filed Critical Thomson CSF SA
Priority to FR9115271A priority Critical patent/FR2684723B1/fr
Publication of FR2684723A1 publication Critical patent/FR2684723A1/fr
Application granted granted Critical
Publication of FR2684723B1 publication Critical patent/FR2684723B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F02K9/80Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/88Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using auxiliary rocket nozzles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/60Steering arrangements
    • F42B10/66Steering by varying intensity or direction of thrust
    • F42B10/663Steering by varying intensity or direction of thrust using a plurality of transversally acting auxiliary nozzles, which are opened or closed by valves
FR9115271A 1991-12-10 1991-12-10 Propulseur a propergol solide a poussee modulable et missile equipe. Expired - Fee Related FR2684723B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR9115271A FR2684723B1 (fr) 1991-12-10 1991-12-10 Propulseur a propergol solide a poussee modulable et missile equipe.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9115271A FR2684723B1 (fr) 1991-12-10 1991-12-10 Propulseur a propergol solide a poussee modulable et missile equipe.

Publications (2)

Publication Number Publication Date
FR2684723A1 FR2684723A1 (fr) 1993-06-11
FR2684723B1 true FR2684723B1 (fr) 1995-05-19

Family

ID=9419853

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9115271A Expired - Fee Related FR2684723B1 (fr) 1991-12-10 1991-12-10 Propulseur a propergol solide a poussee modulable et missile equipe.

Country Status (1)

Country Link
FR (1) FR2684723B1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2914021B1 (fr) * 2007-03-23 2010-10-22 Snpe Materiaux Energetiques Procede et dispositif de propulsion pyrotechnique avec modulation de poussee.
DE102014004251A1 (de) 2013-11-20 2015-06-25 Mbda Deutschland Gmbh Lenkflugkörper und Verfahren zum Lenken eines Lenkflugkörpers

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3139725A (en) * 1961-10-31 1964-07-07 James E Webb Steerable solid propellant rocket motor
DE2846372C2 (de) * 1978-10-25 1985-11-21 Rheinmetall GmbH, 4000 Düsseldorf Geschoß mit radialgerichteten Steuerdüsen zur Endphasenlenkung
FR2517818A1 (fr) * 1981-12-09 1983-06-10 Thomson Brandt Methode de guidage terminal et missile guide operant selon cette methode
DE3531686A1 (de) * 1985-09-05 1987-03-12 Rheinmetall Gmbh Steuerblock
DE3546269C1 (de) * 1985-12-28 1987-08-13 Deutsche Forsch Luft Raumfahrt Flugkoerper
GB8803164D0 (en) * 1988-02-11 1988-08-24 British Aerospace Reaction control system

Also Published As

Publication number Publication date
FR2684723A1 (fr) 1993-06-11

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Legal Events

Date Code Title Description
CD Change of name or company name
ST Notification of lapse
AU Other act affecting the ownership or exploitation of an industrial property right
CL Concession to grant licenses