EP1887307A3 - Device for an optical fiber when starting a missile - Google Patents

Device for an optical fiber when starting a missile Download PDF

Info

Publication number
EP1887307A3
EP1887307A3 EP07015057A EP07015057A EP1887307A3 EP 1887307 A3 EP1887307 A3 EP 1887307A3 EP 07015057 A EP07015057 A EP 07015057A EP 07015057 A EP07015057 A EP 07015057A EP 1887307 A3 EP1887307 A3 EP 1887307A3
Authority
EP
European Patent Office
Prior art keywords
missile
launcher
stern
secured
transmitter
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
EP07015057A
Other languages
German (de)
French (fr)
Other versions
EP1887307A2 (en
EP1887307B1 (en
Inventor
Horst Christof
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.)
LFK Lenkflugkoerpersysteme GmbH
Original Assignee
LFK Lenkflugkoerpersysteme GmbH
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 LFK Lenkflugkoerpersysteme GmbH filed Critical LFK Lenkflugkoerpersysteme GmbH
Publication of EP1887307A2 publication Critical patent/EP1887307A2/en
Publication of EP1887307A3 publication Critical patent/EP1887307A3/en
Application granted granted Critical
Publication of EP1887307B1 publication Critical patent/EP1887307B1/en
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

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

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Optical Communication System (AREA)
  • Optical Couplings Of Light Guides (AREA)
  • Mechanical Light Control Or Optical Switches (AREA)

Abstract

The device for optical transmitter of a missile for transmission of master signal, comprises a support mounted for the transmitter (5), which is surrounded within a launcher (2) by a telescope-like tubular device (6), whose first end completely surrounds a coil (3) secured on stern of the missile (1) and second end is secured to the stern of the missile by a separatable fastener. The transmitter is arranged in the launcher up to ignition of its engine. The tubular device has concentric tube sections lying with one another, and a flat spiral spring. The device for optical transmitter of a missile for transmission of master signal, comprises a support mounted for the transmitter (5), which is surrounded within a launcher (2) by a telescope-like tubular device (6), whose first end completely surrounds a coil (3) secured on stern of the missile (1) and second end is secured to the stern of the missile by a separatable fastener. The transmitter is arranged in the launcher up to ignition of its engine. The tubular device has concentric tube sections lying with one another, and a flat spiral spring, which is prestressed between the stern of the missile and rear end of the launcher. The tube sections are spring loaded and prestressed between the stern of the missile and rear end of the launcher and are arranged above the starting of the missile. The second end of the tubular device is secured to the stern of the missile by a separatable fastener. The length of the tubular device is larger or equal to the length of the interior area of the launcher.
EP07015057A 2006-08-10 2007-08-01 Device for an optical fiber when starting a missile Not-in-force EP1887307B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102006037332A DE102006037332A1 (en) 2006-08-10 2006-08-10 Device for an optical waveguide at the start of a missile

Publications (3)

Publication Number Publication Date
EP1887307A2 EP1887307A2 (en) 2008-02-13
EP1887307A3 true EP1887307A3 (en) 2010-02-10
EP1887307B1 EP1887307B1 (en) 2011-10-12

Family

ID=38508820

Family Applications (1)

Application Number Title Priority Date Filing Date
EP07015057A Not-in-force EP1887307B1 (en) 2006-08-10 2007-08-01 Device for an optical fiber when starting a missile

Country Status (4)

Country Link
EP (1) EP1887307B1 (en)
AT (1) ATE528611T1 (en)
DE (2) DE202006020409U1 (en)
NO (1) NO339592B1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102022003485A1 (en) * 2022-09-21 2024-03-21 Diehl Defence Gmbh & Co. Kg Coil unit for a guided missile

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1578073A1 (en) * 1966-06-18 1971-04-22 Messerschmitt Boelkow Blohm Device for protecting a wire connection used for signal transmission of a recoil-driven missile launched from a launch tube
US4974793A (en) * 1989-12-15 1990-12-04 The Boeing Company Tapered chamber dispensing of optical fiber
DE68907257T2 (en) * 1988-04-14 1993-12-16 Aerospatiale Storage and launch unit for a wire guided missile.

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5385319A (en) 1993-11-22 1995-01-31 Hughes Missile Systems Company Missile with inside payout optical fiber canister
FR2720822B1 (en) * 1994-06-02 1996-08-23 Aerospatiale Installation for conditioning and launching a guided missile.

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1578073A1 (en) * 1966-06-18 1971-04-22 Messerschmitt Boelkow Blohm Device for protecting a wire connection used for signal transmission of a recoil-driven missile launched from a launch tube
DE68907257T2 (en) * 1988-04-14 1993-12-16 Aerospatiale Storage and launch unit for a wire guided missile.
US4974793A (en) * 1989-12-15 1990-12-04 The Boeing Company Tapered chamber dispensing of optical fiber

Also Published As

Publication number Publication date
EP1887307A2 (en) 2008-02-13
NO20074123L (en) 2008-02-11
NO339592B1 (en) 2017-01-09
DE202006020409U1 (en) 2008-07-17
ATE528611T1 (en) 2011-10-15
EP1887307B1 (en) 2011-10-12
DE102006037332A1 (en) 2008-02-14

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