NO20023970L - Artillerirakett - Google Patents

Artillerirakett

Info

Publication number
NO20023970L
NO20023970L NO20023970A NO20023970A NO20023970L NO 20023970 L NO20023970 L NO 20023970L NO 20023970 A NO20023970 A NO 20023970A NO 20023970 A NO20023970 A NO 20023970A NO 20023970 L NO20023970 L NO 20023970L
Authority
NO
Norway
Prior art keywords
artillery rocket
artillery
rocket
Prior art date
Application number
NO20023970A
Other languages
English (en)
Other versions
NO329849B1 (no
NO20023970D0 (no
Inventor
Bernhard Trosky
Harald Wich
Lutz Lehmann
Original Assignee
Diehl Munitionssysteme 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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=7696264&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=NO20023970(L) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Diehl Munitionssysteme Gmbh filed Critical Diehl Munitionssysteme Gmbh
Publication of NO20023970D0 publication Critical patent/NO20023970D0/no
Publication of NO20023970L publication Critical patent/NO20023970L/no
Publication of NO329849B1 publication Critical patent/NO329849B1/no

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
    • F42B10/661—Steering by varying intensity or direction of thrust using several transversally acting rocket motors, each motor containing an individual propellant charge, e.g. solid charge
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/34—Direction control systems for self-propelled missiles based on predetermined target position data

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Carbon And Carbon Compounds (AREA)
  • Powder Metallurgy (AREA)
  • Toys (AREA)
NO20023970A 2001-08-22 2002-08-21 Artillerirakett NO329849B1 (no)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE10141169A DE10141169A1 (de) 2001-08-22 2001-08-22 Artillerierakete

Publications (3)

Publication Number Publication Date
NO20023970D0 NO20023970D0 (no) 2002-08-21
NO20023970L true NO20023970L (no) 2003-02-24
NO329849B1 NO329849B1 (no) 2011-01-10

Family

ID=7696264

Family Applications (1)

Application Number Title Priority Date Filing Date
NO20023970A NO329849B1 (no) 2001-08-22 2002-08-21 Artillerirakett

Country Status (4)

Country Link
US (1) US6685134B2 (no)
EP (1) EP1286128B2 (no)
DE (2) DE10141169A1 (no)
NO (1) NO329849B1 (no)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10354098A1 (de) * 2003-11-19 2005-06-23 Rheinmetall Waffe Munition Gmbh Querschub-Steuervorrichtung
IL178840A0 (en) * 2006-10-24 2007-09-20 Rafael Advanced Defense Sys System
US8546736B2 (en) 2007-03-15 2013-10-01 Raytheon Company Modular guided projectile
US7947938B2 (en) * 2007-03-15 2011-05-24 Raytheon Company Methods and apparatus for projectile guidance
DE102007059397A1 (de) 2007-12-10 2009-06-18 Diehl Bgt Defence Gmbh & Co. Kg Taumelzünder

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2140538A (en) * 1983-05-17 1984-11-28 Ferranti Plc Projectile guidance system
DE3332415A1 (de) * 1983-09-08 1985-03-28 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Steuerbares stroemungsumlenksystem
DE3739370A1 (de) 1987-11-20 1989-06-01 Diehl Gmbh & Co Bomblet-gefechtskopf
DE59004020D1 (de) * 1989-09-19 1994-02-10 Diehl Gmbh & Co Bahnkorrigierbares Projektil.
DE4325218C2 (de) * 1993-07-28 1998-10-22 Diehl Stiftung & Co Artillerie-Rakete und Verfahren zur Leistungssteigerung einer Artillerie-Rakete
US6460801B1 (en) * 1993-11-18 2002-10-08 Lockheed Martin Corp. Precision guidance system for aircraft launched bombs
US5379968A (en) * 1993-12-29 1995-01-10 Raytheon Company Modular aerodynamic gyrodynamic intelligent controlled projectile and method of operating same
DE4401315B4 (de) * 1994-01-19 2006-03-09 Oerlikon Contraves Gmbh Vorrichtung zur Flugbahnkorrektur
US6254031B1 (en) * 1994-08-24 2001-07-03 Lockhead Martin Corporation Precision guidance system for aircraft launched bombs
US6138945A (en) * 1997-01-09 2000-10-31 Biggers; James E. Neural network controller for a pulsed rocket motor tactical missile system
DE19735452C2 (de) * 1997-08-16 1999-07-22 Bodenseewerk Geraetetech Rohrverbindung, insbesondere zum Verbinden zweier rohrförmiger Rumpfteile eines Flugkörpers
DE19824288C2 (de) * 1998-05-29 2002-11-14 Rheinmetall W & M Gmbh Artilleriegeschoß
WO2000052414A1 (en) * 1999-03-03 2000-09-08 Linick James M Impulse motor to improve trajectory correctable munitions
US6502785B1 (en) * 1999-11-17 2003-01-07 Lockheed Martin Corporation Three axis flap control system

Also Published As

Publication number Publication date
US20030038211A1 (en) 2003-02-27
NO329849B1 (no) 2011-01-10
NO20023970D0 (no) 2002-08-21
EP1286128B1 (de) 2006-06-28
EP1286128B2 (de) 2009-07-29
US6685134B2 (en) 2004-02-03
DE50207367D1 (de) 2006-08-10
DE10141169A1 (de) 2003-03-13
EP1286128A1 (de) 2003-02-26

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