DE3764633D1 - Bremsmechanismus fuer entfaltbare fluegel und fernlenkgeschoss mit diesem mechanismus. - Google Patents

Bremsmechanismus fuer entfaltbare fluegel und fernlenkgeschoss mit diesem mechanismus.

Info

Publication number
DE3764633D1
DE3764633D1 DE8787402911T DE3764633T DE3764633D1 DE 3764633 D1 DE3764633 D1 DE 3764633D1 DE 8787402911 T DE8787402911 T DE 8787402911T DE 3764633 T DE3764633 T DE 3764633T DE 3764633 D1 DE3764633 D1 DE 3764633D1
Authority
DE
Germany
Prior art keywords
remote steering
foldable wings
bullet
brake mechanism
brake
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
DE8787402911T
Other languages
German (de)
English (en)
Inventor
Etienne Lamarque
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.)
TDA Armements SAS
Thomson Brandt Armements SA
Original Assignee
TDA Armements SAS
Thomson Brandt Armements 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 TDA Armements SAS, Thomson Brandt Armements SA filed Critical TDA Armements SAS
Application granted granted Critical
Publication of DE3764633D1 publication Critical patent/DE3764633D1/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means 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
    • F42B10/02—Stabilising arrangements
    • F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Vibration Dampers (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
DE8787402911T 1986-12-23 1987-12-18 Bremsmechanismus fuer entfaltbare fluegel und fernlenkgeschoss mit diesem mechanismus. Expired - Fee Related DE3764633D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8618084A FR2608750A1 (fr) 1986-12-23 1986-12-23 Dispositif de freinage du deploiement d'une aile et projectile guide equipe d'un tel dispositif

Publications (1)

Publication Number Publication Date
DE3764633D1 true DE3764633D1 (de) 1990-10-04

Family

ID=9342240

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8787402911T Expired - Fee Related DE3764633D1 (de) 1986-12-23 1987-12-18 Bremsmechanismus fuer entfaltbare fluegel und fernlenkgeschoss mit diesem mechanismus.

Country Status (4)

Country Link
US (1) US4852828A (enExample)
EP (1) EP0275766B1 (enExample)
DE (1) DE3764633D1 (enExample)
FR (1) FR2608750A1 (enExample)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2237362B (en) * 1989-10-24 1994-01-19 British Aerospace Retardation and arming mechanism for a projectile
FR2657703B1 (fr) * 1990-01-26 1992-04-10 Thomson Brandt Armements Dispositif pour la commande d'attitude en roulis d'un projectile stabilise par empennage.
DE4119613C2 (de) * 1991-06-14 1997-03-27 Diehl Gmbh & Co Flugkörper mit ausklappbaren Leiteinrichtungen
SE544263C2 (en) * 2020-07-03 2022-03-22 Saab Ab A wing arrangement, a projectile, a method for deploying a wing blade, a use and a method for assembly

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3785290A (en) * 1971-03-01 1974-01-15 Us Navy Bomb fin shock absorber assembly
US3819132A (en) * 1973-02-21 1974-06-25 Sarmac Sa Self propelled projectile with fins
US4143838A (en) * 1977-08-22 1979-03-13 The United States Of America As Represented By The Secretary Of The Navy Folding fin assembly detent
US4175720A (en) * 1978-04-05 1979-11-27 The United States Of America As Represented By The Secretary Of The Navy Retainer/release mechanism for use on fin stabilized gun fired projectiles
US4323208A (en) * 1980-02-01 1982-04-06 British Aerospace Folding fins

Also Published As

Publication number Publication date
US4852828A (en) 1989-08-01
FR2608750B1 (enExample) 1993-02-26
EP0275766A1 (fr) 1988-07-27
EP0275766B1 (fr) 1990-08-29
FR2608750A1 (fr) 1988-06-24

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee