EP0679861A1 - Schiessvorrichtung für drahtgelenkte Munition aus einem mobilen Werfer - Google Patents

Schiessvorrichtung für drahtgelenkte Munition aus einem mobilen Werfer Download PDF

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Publication number
EP0679861A1
EP0679861A1 EP95400899A EP95400899A EP0679861A1 EP 0679861 A1 EP0679861 A1 EP 0679861A1 EP 95400899 A EP95400899 A EP 95400899A EP 95400899 A EP95400899 A EP 95400899A EP 0679861 A1 EP0679861 A1 EP 0679861A1
Authority
EP
European Patent Office
Prior art keywords
coil
tube
installation according
axis
ammunition
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
EP95400899A
Other languages
English (en)
French (fr)
Other versions
EP0679861B1 (de
Inventor
Frédérick Donnaint
Eric Droz-Bartholet
Isabelle Charruyer
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.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Publication of EP0679861A1 publication Critical patent/EP0679861A1/de
Application granted granted Critical
Publication of EP0679861B1 publication Critical patent/EP0679861B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • 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
    • F42B15/01—Arrangements thereon for guidance or control
    • F42B15/04—Arrangements thereon for guidance or control using wire, e.g. for guiding ground-to-ground rockets
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/30—Command link guidance systems
    • F41G7/32—Command link guidance systems for wire-guided missiles

Definitions

  • a section 18a of the optical fiber 18, corresponding for example to at least half of its total length, is wound up on a first coil 20 housed in the rear part of the missile 16. This arrangement is conventional and will therefore not be described in more detail.
  • the cover 32 extends beyond the end of the core 26 facing upwards in the normal storage position of the coil 22 and its diameter then decreases to present a circular opening 32a, centered on the axis of the core 26 and through which the fiber leaves the coil 22.
  • the diameter of this opening 32a is for example close to the outside diameter of the core 26.
  • the front end of the installation does not have any protuberance capable of preventing its stacking or increasing the master- couple.
  • reel 22 can be supported directly by the launch tube 14, instead of being fixed on the internal face of the front door 24. The release of the front door and the tilting towards the outside of the coil then intervene sequentially.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
EP19950400899 1994-04-25 1995-04-21 Schiessvorrichtung für drahtgelenkte Munition aus einem mobilen Werfer Expired - Lifetime EP0679861B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9404947A FR2719111B1 (fr) 1994-04-25 1994-04-25 Installation de tir de munition filoguidée depuis un lanceur mobile.
FR9404947 1994-04-25

Publications (2)

Publication Number Publication Date
EP0679861A1 true EP0679861A1 (de) 1995-11-02
EP0679861B1 EP0679861B1 (de) 1998-12-30

Family

ID=9462472

Family Applications (1)

Application Number Title Priority Date Filing Date
EP19950400899 Expired - Lifetime EP0679861B1 (de) 1994-04-25 1995-04-21 Schiessvorrichtung für drahtgelenkte Munition aus einem mobilen Werfer

Country Status (4)

Country Link
EP (1) EP0679861B1 (de)
DE (1) DE69506940T2 (de)
ES (1) ES2128005T3 (de)
FR (1) FR2719111B1 (de)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3022881A1 (fr) * 2014-06-30 2016-01-01 Dcns Engin sous-marin comportant des moyens de lancement d'un vehicule sous-marin
WO2019219476A1 (de) * 2018-05-17 2019-11-21 Thyssenkrupp Marine Systems Gmbh WAFFENROHRMODUL ZUM AUSSTOß VON ZWEI HINTEREINANDER ANGEORDNETEN GEFÜHRTEN WAFFEN

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007005254B4 (de) 2007-02-02 2009-01-29 Lfk-Lenkflugkörpersysteme Gmbh Abwurfvorrichtung und Abwurfverfahren für einen Flugkörper
DE102009011447B9 (de) * 2009-03-03 2012-08-16 Diehl Bgt Defence Gmbh & Co. Kg Verfahren zum Zünden eines Gefechtskopfs einer Granate und Fahrzeug
DE102022001553A1 (de) 2022-05-04 2023-11-09 Bundesrepublik Deutschland, vertr. durch das Bundesministerium der Verteidigung, vertr. durch das Bundesamt für Ausrüstung, Informationstechnik und Nutzung der Bundeswehr Verfahren und Vorrichtung zur Kontrolle des sicheren Einsatzes von Flugkörpern an Hubschraubern

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0337254A2 (de) * 1988-04-15 1989-10-18 The Boeing Company Nachrichtenverbindung zwischen Fahrzeugen
EP0443623A1 (de) * 1990-02-23 1991-08-28 Hughes Aircraft Company Behälter für multidirektionalen Abzug für Glasfaseroptik
DE4112016C1 (en) * 1991-04-12 1992-08-06 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De Flight path and/or actual speed detector - uses sensor at circular gap between fixed parts of missile to register speed of unwinding of guiding optical fibre

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0337254A2 (de) * 1988-04-15 1989-10-18 The Boeing Company Nachrichtenverbindung zwischen Fahrzeugen
EP0443623A1 (de) * 1990-02-23 1991-08-28 Hughes Aircraft Company Behälter für multidirektionalen Abzug für Glasfaseroptik
DE4112016C1 (en) * 1991-04-12 1992-08-06 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De Flight path and/or actual speed detector - uses sensor at circular gap between fixed parts of missile to register speed of unwinding of guiding optical fibre

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3022881A1 (fr) * 2014-06-30 2016-01-01 Dcns Engin sous-marin comportant des moyens de lancement d'un vehicule sous-marin
WO2019219476A1 (de) * 2018-05-17 2019-11-21 Thyssenkrupp Marine Systems Gmbh WAFFENROHRMODUL ZUM AUSSTOß VON ZWEI HINTEREINANDER ANGEORDNETEN GEFÜHRTEN WAFFEN
KR20210019011A (ko) * 2018-05-17 2021-02-19 티쎈크로프 마리네 지스템스 게엠베하 서로 잇달아 배열된 두개의 안내된 무기들의 방출을 위한 배럴 모듈
AU2019268994B2 (en) * 2018-05-17 2021-10-07 Thyssenkrupp Ag Barrel module for ejection of two guided weapons arranged one behind the other

Also Published As

Publication number Publication date
ES2128005T3 (es) 1999-05-01
FR2719111A1 (fr) 1995-10-27
FR2719111B1 (fr) 1996-07-12
DE69506940D1 (de) 1999-02-11
EP0679861B1 (de) 1998-12-30
DE69506940T2 (de) 1999-07-01

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