AU2245801A - Ring array projectile steering with optically-triggered diverter elements - Google Patents

Ring array projectile steering with optically-triggered diverter elements

Info

Publication number
AU2245801A
AU2245801A AU22458/01A AU2245801A AU2245801A AU 2245801 A AU2245801 A AU 2245801A AU 22458/01 A AU22458/01 A AU 22458/01A AU 2245801 A AU2245801 A AU 2245801A AU 2245801 A AU2245801 A AU 2245801A
Authority
AU
Australia
Prior art keywords
triggered
optically
ring array
diverter elements
projectile steering
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.)
Abandoned
Application number
AU22458/01A
Inventor
Tibor G. Horwath
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.)
General Dynamics Ordnance and Tactical Systems Inc
Original Assignee
Primex Technologies Inc
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 Primex Technologies Inc filed Critical Primex Technologies Inc
Publication of AU2245801A publication Critical patent/AU2245801A/en
Abandoned legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G7/00Direction control systems for self-propelled missiles
    • F41G7/20Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22Homing guidance systems
    • F41G7/226Semi-active homing systems, i.e. comprising a receiver and involving auxiliary illuminating means, e.g. using auxiliary guiding missiles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G7/00Direction control systems for self-propelled missiles
    • F41G7/20Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22Homing guidance systems
    • F41G7/2273Homing guidance systems characterised by the type of waves
    • F41G7/2293Homing guidance systems characterised by the type of waves using electromagnetic waves other than radio waves
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/60Steering arrangements
    • F42B10/66Steering by varying intensity or direction of thrust
    • F42B10/661Steering by varying intensity or direction of thrust using several transversally acting rocket motors, each motor containing an individual propellant charge, e.g. solid charge
AU22458/01A 1999-07-21 2000-07-20 Ring array projectile steering with optically-triggered diverter elements Abandoned AU2245801A (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US14491899P 1999-07-21 1999-07-21
US60144918 1999-07-21
PCT/US2000/019925 WO2001016547A2 (en) 1999-07-21 2000-07-20 Ring array projectile steering with optically-triggered diverter elements

Publications (1)

Publication Number Publication Date
AU2245801A true AU2245801A (en) 2001-03-26

Family

ID=22510742

Family Applications (1)

Application Number Title Priority Date Filing Date
AU22458/01A Abandoned AU2245801A (en) 1999-07-21 2000-07-20 Ring array projectile steering with optically-triggered diverter elements

Country Status (4)

Country Link
EP (1) EP1196733B1 (en)
AU (1) AU2245801A (en)
DE (1) DE60023007T2 (en)
WO (1) WO2001016547A2 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10147837A1 (en) 2001-09-27 2003-04-24 Rheinmetall Landsysteme Gmbh Warhead throwing system with a mine neutralizer
DE102004029343B4 (en) * 2004-06-17 2009-04-30 Diehl Bgt Defence Gmbh & Co. Kg Guidance device for an aircraft
DE202007018452U1 (en) * 2007-01-16 2008-10-02 Lfk-Lenkflugkörpersysteme Gmbh Search head for a guided missile for detecting and tracking a target
DE102009016147A1 (en) 2009-04-03 2010-10-07 Rheinmetall Soldier Electronics Gmbh Demountable projectile for use in weapon barrel of weapon system, is demounted into two projectile parts after firing target location, where projectile parts are connected with each other by multiple connecting elements
US8164037B2 (en) * 2009-09-26 2012-04-24 Raytheon Company Co-boresighted dual-mode SAL/IR seeker including a SAL spreader

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3000307A (en) * 1953-08-04 1961-09-19 Jr Herbert Trotter Device for correcting the course of a missile
US4006356A (en) * 1961-10-27 1977-02-01 Aeronutronic Ford Corporation Radiant energy tracking device
GB1605228A (en) * 1970-10-01 1985-03-20 British Aerospace Missiles
US4231533A (en) * 1975-07-09 1980-11-04 The United States Of America As Represented By The Secretary Of The Air Force Static self-contained laser seeker system for active missile guidance
US5102065A (en) 1988-02-17 1992-04-07 Thomson - Csf System to correct the trajectory of a projectile
US5127604A (en) * 1989-08-18 1992-07-07 Raytheon Company Optical system
DE4007712A1 (en) * 1990-03-10 1991-09-12 Tzn Forschung & Entwicklung FLOOR WITH AN IR DETECTING SYSTEM ARROWED ON THE BOW SIDE
US5529262A (en) 1993-06-23 1996-06-25 Horwath; Tibor G. Guidance seeker for small spinning projectiles
US5456429A (en) * 1993-08-02 1995-10-10 Loral Corp. Thrust maneuver system
DE4408085C2 (en) * 1994-03-10 1999-08-12 Rheinmetall W & M Gmbh Device for guiding a missile not rotating about its longitudinal axis
DE4410326C2 (en) * 1994-03-25 1998-07-02 Rheinmetall Ind Ag Projectile with a device for trajectory correction
DE4443134C2 (en) * 1994-12-03 2001-07-05 Diehl Stiftung & Co Sensor device for a missile
IL116438A (en) 1995-12-18 2000-01-31 Israel State Laser sensor
US5695152A (en) * 1996-09-18 1997-12-09 Israel Aircraft Industries Ltd. System for correcting flight trajectory of a projectile
US6076765A (en) 1997-01-02 2000-06-20 Primex Technologies, Inc. Reticle for use in a guidance seeker for a spinning projectile

Also Published As

Publication number Publication date
DE60023007T2 (en) 2006-07-13
EP1196733A2 (en) 2002-04-17
DE60023007D1 (en) 2006-02-16
EP1196733A4 (en) 2003-07-02
WO2001016547A2 (en) 2001-03-08
EP1196733B1 (en) 2005-10-05
WO2001016547A3 (en) 2001-06-21

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Legal Events

Date Code Title Description
MK6 Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase