NO20074123L - Device for a light bulb conductor at the start of an aircraft body - Google Patents

Device for a light bulb conductor at the start of an aircraft body

Info

Publication number
NO20074123L
NO20074123L NO20074123A NO20074123A NO20074123L NO 20074123 L NO20074123 L NO 20074123L NO 20074123 A NO20074123 A NO 20074123A NO 20074123 A NO20074123 A NO 20074123A NO 20074123 L NO20074123 L NO 20074123L
Authority
NO
Norway
Prior art keywords
missile
launcher
stern
secured
transmitter
Prior art date
Application number
NO20074123A
Other languages
Norwegian (no)
Other versions
NO339592B1 (en
Inventor
Horst Christof
Original Assignee
Lfk 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 Gmbh filed Critical Lfk Gmbh
Publication of NO20074123L publication Critical patent/NO20074123L/en
Publication of NO339592B1 publication Critical patent/NO339592B1/en

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)
  • Mechanical Light Control Or Optical Switches (AREA)
  • Optical Communication System (AREA)
  • Optical Couplings Of Light Guides (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.
NO20074123A 2006-08-10 2007-08-09 Device for a light waveguide at the start of an aircraft body NO339592B1 (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 (2)

Publication Number Publication Date
NO20074123L true NO20074123L (en) 2008-02-11
NO339592B1 NO339592B1 (en) 2017-01-09

Family

ID=38508820

Family Applications (1)

Application Number Title Priority Date Filing Date
NO20074123A NO339592B1 (en) 2006-08-10 2007-08-09 Device for a light waveguide at the start of an aircraft body

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
DE102022003485B4 (en) * 2022-09-21 2024-11-14 Diehl Defence Gmbh & Co. Kg coil unit for a guided missile

Family Cites Families (5)

* 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
FR2630202B1 (en) * 1988-04-14 1990-08-17 Aerospatiale PACKAGING AND LAUNCHING INSTALLATION OF A FILOGUIDE MISSILE
US4974793A (en) * 1989-12-15 1990-12-04 The Boeing Company Tapered chamber dispensing of optical fiber
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.

Also Published As

Publication number Publication date
ATE528611T1 (en) 2011-10-15
EP1887307A3 (en) 2010-02-10
DE102006037332A1 (en) 2008-02-14
DE202006020409U1 (en) 2008-07-17
EP1887307A2 (en) 2008-02-13
EP1887307B1 (en) 2011-10-12
NO339592B1 (en) 2017-01-09

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