DE602005010933D1 - Raketensuchkopf - Google Patents

Raketensuchkopf

Info

Publication number
DE602005010933D1
DE602005010933D1 DE602005010933T DE602005010933T DE602005010933D1 DE 602005010933 D1 DE602005010933 D1 DE 602005010933D1 DE 602005010933 T DE602005010933 T DE 602005010933T DE 602005010933 T DE602005010933 T DE 602005010933T DE 602005010933 D1 DE602005010933 D1 DE 602005010933D1
Authority
DE
Germany
Prior art keywords
projectile
light sensor
light
opening
hollow
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
DE602005010933T
Other languages
English (en)
Inventor
Ehud Chishinski
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.)
Rafael Advanced Defense Systems Ltd
Original Assignee
Rafael Advanced Defense Systems Ltd
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 Rafael Advanced Defense Systems Ltd filed Critical Rafael Advanced Defense Systems Ltd
Publication of DE602005010933D1 publication Critical patent/DE602005010933D1/de
Expired - Fee Related 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
    • 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
    • F42B10/60—Steering arrangements
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F42B10/663—Steering by varying intensity or direction of thrust using a plurality of transversally acting auxiliary nozzles, which are opened or closed by valves
    • 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
    • F41G7/22—Homing guidance systems
    • F41G7/226—Semi-active homing systems, i.e. comprising a receiver and involving auxiliary illuminating means, e.g. using auxiliary guiding missiles
    • 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
    • F41G7/22—Homing guidance systems
    • F41G7/2273—Homing guidance systems characterised by the type of waves
    • F41G7/2293—Homing guidance systems characterised by the type of waves using electromagnetic waves other than radio waves
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S3/00—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received
    • G01S3/78—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received using electromagnetic waves other than radio waves
    • G01S3/782—Systems for determining direction or deviation from predetermined direction
    • G01S3/787—Systems for determining direction or deviation from predetermined direction using rotating reticles producing a direction-dependent modulation characteristic

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Engineering & Computer Science (AREA)
  • Electromagnetism (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Fluid Mechanics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Optical Radar Systems And Details Thereof (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Medicines Containing Antibodies Or Antigens For Use As Internal Diagnostic Agents (AREA)
DE602005010933T 2004-05-17 2005-05-12 Raketensuchkopf Expired - Fee Related DE602005010933D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IL162032A IL162032A (en) 2004-05-17 2004-05-17 Optical target search accessory for bullet

Publications (1)

Publication Number Publication Date
DE602005010933D1 true DE602005010933D1 (de) 2008-12-24

Family

ID=34936448

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005010933T Expired - Fee Related DE602005010933D1 (de) 2004-05-17 2005-05-12 Raketensuchkopf

Country Status (5)

Country Link
US (1) US7036767B2 (de)
EP (1) EP1598633B1 (de)
AT (1) ATE414255T1 (de)
DE (1) DE602005010933D1 (de)
IL (1) IL162032A (de)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7511253B2 (en) * 2006-11-13 2009-03-31 Lockheed Martin Corporation Apparatus for detecting radiation and munition incorporating same
US8319162B2 (en) 2008-12-08 2012-11-27 Raytheon Company Steerable spin-stabilized projectile and method
US8119958B2 (en) 2009-02-19 2012-02-21 Lockheed Martin Corporation Method and device for matrix of explosive cells
DE102014014906B3 (de) * 2014-10-08 2015-10-15 Mbda Deutschland Gmbh Flugkörper und Verfahren zum Betreiben eines Flugkörpers

Family Cites Families (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4105174A (en) * 1973-06-08 1978-08-08 Ab Bofors Device for receiving or transmitting radiation
US5259570A (en) * 1974-08-12 1993-11-09 The United States Of America As Represented By The Secretary Of The Navy Laser resistant optical detector arrangement
US4245890A (en) * 1979-01-02 1981-01-20 The United States Of America As Represented By The Secretary Of The Army Gradient index of refraction for missile seekers
US4717822A (en) * 1986-08-04 1988-01-05 Hughes Aircraft Company Rosette scanning surveillance sensor
DE3638847C1 (de) * 1986-11-13 1996-07-25 Bodenseewerk Geraetetech Flugkörperbaugruppe mit strahlungsdurchlässigem Abdeckkörper und Fassungsring
DE3830496C1 (de) * 1988-09-08 1996-09-19 Daimler Benz Aerospace Ag Vorrichtung zum Erkennen und Verfolgen von Objekten
GB8828680D0 (en) * 1988-12-08 2000-10-04 British Aerospace Underwater detection system
DE4112140A1 (de) * 1991-04-13 1992-10-15 Bodenseewerk Geraetetech Suchkopfabdeckung fuer lenkflugkoerper
DE4208516C2 (de) * 1992-03-17 1994-03-03 Deutsche Aerospace Bilderzeugendes Suchkopfsystem
US5368254A (en) * 1993-03-16 1994-11-29 Hughes Aircraft Company Optical imaging system including generally conical, transparent protective dome and optically refractive fixed corrector for reversing conical deformation created by viewing through the dome
DE4410326C2 (de) * 1994-03-25 1998-07-02 Rheinmetall Ind Ag Geschoß mit einer Vorrichtung zur Flugbahnkorrektur
DE4442134A1 (de) * 1994-11-26 1996-05-30 Bodenseewerk Geraetetech Lenkschleife für Flugkörper
DE4443134C2 (de) * 1994-12-03 2001-07-05 Diehl Stiftung & Co Sensoreinrichtung für einen Flugkörper
US5681009A (en) * 1996-09-27 1997-10-28 Lockheed Missiles And Space Company Missile having endoatmospheric and exoatmospheric seeker capability
AU5957898A (en) * 1997-01-02 1998-08-07 Tibor G. Horwath Reticle for use in a guidance seeker for a spinning projectile
US5791591A (en) * 1997-04-28 1998-08-11 The United States Of America As Represented By The Secretary Of The Navy Target seeking free gyro
US6310730B1 (en) * 1997-10-02 2001-10-30 Raytheon Company Optical system with asymmetric optical corrector
US6028712A (en) * 1997-10-02 2000-02-22 Raytheon Company Optical system and method for providing corrected optical images
US6180938B1 (en) * 1997-12-08 2001-01-30 Raytheon Company Optical system with a window having a conicoidal inner surface, and testing of the optical system
US6138944A (en) * 1999-04-16 2000-10-31 The United States Of America As Represented By The Secretary Of The Army Scatterider guidance system for a flying object based on maintenance of minimum distance between the designating laser beam and the longitudinal axis of the flying object
AUPR303501A0 (en) * 2001-02-09 2001-03-08 Kusic, Tom Spiralling missile
US6462889B1 (en) * 2000-06-22 2002-10-08 Raytheon Company Conformal-dome optical system with rotationally symmetric stationary optical baffles
US6525809B2 (en) * 2001-01-23 2003-02-25 Sikorsky Aircraft Corporation Alignment device for a guided missile seeker
US6606066B1 (en) * 2001-10-29 2003-08-12 Northrop Grumman Corporation Tri-mode seeker
US6851645B1 (en) * 2003-12-05 2005-02-08 Lockheed Martin Corporation Non-coherent fresnel direction finding method and apparatus

Also Published As

Publication number Publication date
EP1598633B1 (de) 2008-11-12
EP1598633A1 (de) 2005-11-23
IL162032A0 (en) 2005-11-20
IL162032A (en) 2009-05-04
US7036767B2 (en) 2006-05-02
ATE414255T1 (de) 2008-11-15
US20060054734A1 (en) 2006-03-16

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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