ATE301816T1 - Einrichtung zur veränderung der flugrichtung eines rotationsstabilisierten lenkgeschosses - Google Patents

Einrichtung zur veränderung der flugrichtung eines rotationsstabilisierten lenkgeschosses

Info

Publication number
ATE301816T1
ATE301816T1 AT00402839T AT00402839T ATE301816T1 AT E301816 T1 ATE301816 T1 AT E301816T1 AT 00402839 T AT00402839 T AT 00402839T AT 00402839 T AT00402839 T AT 00402839T AT E301816 T1 ATE301816 T1 AT E301816T1
Authority
AT
Austria
Prior art keywords
flight
changing
rotation
guided missile
shell
Prior art date
Application number
AT00402839T
Other languages
German (de)
English (en)
Inventor
Pascal Tarayre
Jean-Paul Labroche
Dominique Broussoux
Original Assignee
Tda Armements 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 Tda Armements Sas filed Critical Tda Armements Sas
Application granted granted Critical
Publication of ATE301816T1 publication Critical patent/ATE301816T1/de

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
    • F42B10/02—Stabilising arrangements
    • F42B10/22—Projectiles of cannelured type
    • F42B10/24—Projectiles of cannelured type with inclined grooves
    • 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
    • F42B10/02—Stabilising arrangements
    • F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • 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
    • F42B10/62—Steering by movement of flight surfaces
    • F42B10/64—Steering by movement of flight surfaces of fins

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Toys (AREA)
  • Steering Controls (AREA)
AT00402839T 1999-10-15 2000-10-13 Einrichtung zur veränderung der flugrichtung eines rotationsstabilisierten lenkgeschosses ATE301816T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9912915A FR2799833B1 (fr) 1999-10-15 1999-10-15 Dispositif de correction de trajectoire pour projectiles guides gyroscopes

Publications (1)

Publication Number Publication Date
ATE301816T1 true ATE301816T1 (de) 2005-08-15

Family

ID=9551000

Family Applications (1)

Application Number Title Priority Date Filing Date
AT00402839T ATE301816T1 (de) 1999-10-15 2000-10-13 Einrichtung zur veränderung der flugrichtung eines rotationsstabilisierten lenkgeschosses

Country Status (4)

Country Link
EP (1) EP1092941B1 (fr)
AT (1) ATE301816T1 (fr)
DE (1) DE60021822T2 (fr)
FR (1) FR2799833B1 (fr)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2829593B1 (fr) * 2001-09-07 2003-11-21 Tda Armements Sas Procede de guidage d'un engin, notamment d'une munition
DE102007052938B3 (de) * 2007-11-02 2009-04-16 Jallcom Holdings Ltd. Geschoss mit einen Drall erzeugenden Strömungskanälen
DE102008007435B4 (de) 2008-02-01 2010-04-15 Deutsch Französisches Forschungsinstitut Saint Louis Drallstabilisiertes, lenkbares Geschoss und Verfahren zu seiner Lenkung
SE534614C2 (sv) * 2010-02-25 2011-10-25 Bae Systems Bofors Ab Granat anordnad med utfällbara vingar och styranordning
JP5626768B2 (ja) * 2010-05-28 2014-11-19 株式会社Ｉｈｉエアロスペース 飛翔体
ES2709655T3 (es) 2011-05-13 2019-04-17 Leigh Aerosystems Corp Sistema de guiado de proyectil terrestre
WO2017035126A1 (fr) * 2015-08-24 2017-03-02 Leigh Aerosystems Corporation Système de guidage de projectile au sol
US10280786B2 (en) 2015-10-08 2019-05-07 Leigh Aerosystems Corporation Ground-projectile system
DE102015013913A1 (de) * 2015-10-27 2017-04-27 Deutsch Französisches Forschungsinstitut Saint Louis Vollkalibriges, drallstabilisiertes Lenkgeschoss mit einer hohen Reichweite
US11624594B1 (en) 2020-03-31 2023-04-11 Barron Associates, Inc. Device, method and system for extending range and improving tracking precision of mortar rounds
KR102324184B1 (ko) * 2020-06-26 2021-11-09 국방과학연구소 초소형 웨어러블 유도탄 구동장치
DE102022002231A1 (de) 2021-08-21 2023-05-25 Kastriot Merlaku Leucht-System für Militärzwecke, das punktuell oder breitflächig ein Gegenstand oder Bodenbereich beleuchten soll

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5439188A (en) * 1964-09-04 1995-08-08 Hughes Missile Systems Company Control system
DE2141744C3 (de) * 1971-08-20 1978-09-14 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Flugkörper mit Schubvektor- und aerodynamischer Steuerung
US4565340A (en) * 1984-08-15 1986-01-21 Ford Aerospace & Communications Corporation Guided projectile flight control fin system
DE8620702U1 (de) * 1986-08-01 1987-01-08 Böhm, Walter, 7000 Stuttgart Weichprojektil
US5505408A (en) * 1993-10-19 1996-04-09 Versatron Corporation Differential yoke-aerofin thrust vector control system
US5775636A (en) * 1996-09-30 1998-07-07 The United States Of America As Represented By The Secretary Of The Army Guided artillery projectile and method
US6126109A (en) * 1997-04-11 2000-10-03 Raytheon Company Unlocking tail fin assembly for guided projectiles

Also Published As

Publication number Publication date
EP1092941B1 (fr) 2005-08-10
FR2799833A1 (fr) 2001-04-20
EP1092941A1 (fr) 2001-04-18
DE60021822D1 (de) 2005-09-15
FR2799833B1 (fr) 2002-10-25
DE60021822T2 (de) 2006-06-08

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Legal Events

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