ES2128005T3 - INSTALLATION TO FIRE FILOGUIDED AMMUNITION FROM A MOBILE LAUNCHER. - Google Patents

INSTALLATION TO FIRE FILOGUIDED AMMUNITION FROM A MOBILE LAUNCHER.

Info

Publication number
ES2128005T3
ES2128005T3 ES95400899T ES95400899T ES2128005T3 ES 2128005 T3 ES2128005 T3 ES 2128005T3 ES 95400899 T ES95400899 T ES 95400899T ES 95400899 T ES95400899 T ES 95400899T ES 2128005 T3 ES2128005 T3 ES 2128005T3
Authority
ES
Spain
Prior art keywords
ammunition
coil
filoguided
fire
installation
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 - Lifetime
Application number
ES95400899T
Other languages
Spanish (es)
Inventor
Frederick 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
Application granted granted Critical
Publication of ES2128005T3 publication Critical patent/ES2128005T3/en
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • 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

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)

Abstract

UN ORGANO DE CONEXION FILIFORME TAL COMO UNA FIBRA OPTICA, QUE CONECTA UNA MUNICION GUIADA POR HILO (16) CON UN TUBO DE LANZAMIENTO (14) EMBARCADO EN UN LANZADOR MOVIL, ES RECIBIDO SOBRE UNA PRIMERA BOBINA (20) LLEVADA POR LA MUNICION Y SOBRE UNA SEGUNDA BOBINA (22) MONADA EN EL TUBO DE LANZAMIENTO (14), ENTRE LA MUNICION (16) Y UNA PUERTA DELANTERA (24) DEL TUBO. EL ORGANO DE CONEXION, ASI COMO LA MUNICION ESTAN TOTALMENTE PROTEGIDOS POR EL TUBO DE LANZAMIENTO DURANTE EL ALMACENAMIENTO Y EL TRANSPORTE. JUSTO ANTES DEL ENCENDIDO DE LA MUNICION (16), LA SEGUNDA BOBINA (22) BASCULA AL EXTERIOR DEL TUBO DE LANZAMIENTO (14) PARA PERMITIR EL PASO DE LA MUNICION. EL ORGANO DE CONEXION SE DESENROLLA ENTONCES HACIA LA PARTE TRASERA DEL LANZADOR, LO QUE PERMITE A ESTE ULTIMO ALEJARSE DEL BLANCO.A FILIFORM CONNECTING ORGAN SUCH AS AN OPTICAL FIBER, WHICH CONNECTS A THREAD-GUIDED AMMUNITION (16) WITH A LAUNCH TUBE (14) BOARD IN A MOBILE LAUNCHER, IS RECEIVED ON A FIRST COIL (20) CARRIED BY THE AMMUNITION AND ON A SECOND COIL (22) MOUNTED ON THE LAUNCH PIPE (14), BETWEEN THE AMMUNITION (16) AND A FRONT DOOR (24) OF THE PIPE. THE CONNECTION BODY, AS WELL AS THE MUNICIPALITY, ARE FULLY PROTECTED BY THE LAUNCH PIPE DURING STORAGE AND TRANSPORT. JUST BEFORE THE AMMUNITION IS STARTED (16), THE SECOND COIL (22) SCALES OUTSIDE THE LAUNCH TUBE (14) TO ALLOW THE PASSAGE OF THE AMMUNITION. THEN THE CONNECTING ORGAN IS DEVELOPED TOWARDS THE BACK OF THE PITCHER, WHICH ALLOWS THE LAST ONE TO GET AWAY FROM THE TARGET.

ES95400899T 1994-04-25 1995-04-21 INSTALLATION TO FIRE FILOGUIDED AMMUNITION FROM A MOBILE LAUNCHER. Expired - Lifetime ES2128005T3 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9404947A FR2719111B1 (en) 1994-04-25 1994-04-25 Installation of fired ammunition firing from a mobile launcher.

Publications (1)

Publication Number Publication Date
ES2128005T3 true ES2128005T3 (en) 1999-05-01

Family

ID=9462472

Family Applications (1)

Application Number Title Priority Date Filing Date
ES95400899T Expired - Lifetime ES2128005T3 (en) 1994-04-25 1995-04-21 INSTALLATION TO FIRE FILOGUIDED AMMUNITION FROM A MOBILE LAUNCHER.

Country Status (4)

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

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007005254B4 (en) 2007-02-02 2009-01-29 Lfk-Lenkflugkörpersysteme Gmbh Dropping device and dropping method for a missile
DE102009011447B9 (en) * 2009-03-03 2012-08-16 Diehl Bgt Defence Gmbh & Co. Kg Method for igniting a warhead of a grenade and vehicle
FR3022881B1 (en) * 2014-06-30 2016-11-04 Dcns SUBMARINE ENGINE HAVING MEANS FOR LAUNCHING A SUBMARINE VEHICLE
DE102018207712A1 (en) * 2018-05-17 2019-11-21 Thyssenkrupp Ag Weapon tube module for ejecting two guided weapons arranged one behind the other
DE102022001553B4 (en) 2022-05-04 2024-07-18 Bundesrepublik Deutschland, vertr. durch das Bundesministerium der Verteidigung, vertr. durch das Bundesamt für Ausrüstung, Informationstechnik und Nutzung der Bundeswehr Measuring method and device for controlling the safe use of missiles on helicopters

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4860968A (en) * 1988-04-15 1989-08-29 The Boeing Company Communication link between moving bodies
US5005930A (en) * 1990-02-23 1991-04-09 Hughes Aircraft Company Multi-directional payout fiber optic canister
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

Also Published As

Publication number Publication date
DE69506940T2 (en) 1999-07-01
EP0679861A1 (en) 1995-11-02
FR2719111B1 (en) 1996-07-12
FR2719111A1 (en) 1995-10-27
DE69506940D1 (en) 1999-02-11
EP0679861B1 (en) 1998-12-30

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