DE50204329D1 - ARTILLERY PROJECTILE WITH EXCHANGEABLE LOAD LOAD - Google Patents

ARTILLERY PROJECTILE WITH EXCHANGEABLE LOAD LOAD

Info

Publication number
DE50204329D1
DE50204329D1 DE50204329T DE50204329T DE50204329D1 DE 50204329 D1 DE50204329 D1 DE 50204329D1 DE 50204329 T DE50204329 T DE 50204329T DE 50204329 T DE50204329 T DE 50204329T DE 50204329 D1 DE50204329 D1 DE 50204329D1
Authority
DE
Germany
Prior art keywords
load
section
exchangeable
standardized
artillery projectile
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 - Lifetime
Application number
DE50204329T
Other languages
German (de)
Inventor
Karl Kautzsch
Klaus Baer
Juergen Bohl
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.)
Diehl BGT Defence GmbH and Co KG
Original Assignee
Diehl BGT Defence GmbH and Co KG
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 Diehl BGT Defence GmbH and Co KG filed Critical Diehl BGT Defence GmbH and Co KG
Priority to DE50204329T priority Critical patent/DE50204329D1/en
Application granted granted Critical
Publication of DE50204329D1 publication Critical patent/DE50204329D1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • F42B10/04—Stabilising arrangements using fixed fins
    • F42B10/06—Tail fins
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B14/00—Projectiles or missiles characterised by arrangements for guiding or sealing them inside barrels, or for lubricating or cleaning barrels
    • F42B14/02—Driving bands; Rotating bands
    • 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
    • F42B10/16—Wrap-around fins
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
    • F42B12/56—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing discrete solid bodies
    • F42B12/58—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles
    • F42B12/62—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected parallel to the longitudinal axis of the projectile

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Braking Arrangements (AREA)
  • Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)

Abstract

An inexpensive artillery munition of great range and acquisition accuracy for universal use while maintaining the external-ballistic coefficients is afforded when inserted between a standardized tail section (12) and also standardized tip section (13) is a load section (14) which connects the two contours of said sections together and which can be equipped with very different warheads which in particular are optimized against hard targets. For launch into an aerodynamically stabilized ballistic trajectory the tail section (12) is provided with super-calibre stabilization fins (17).
DE50204329T 2001-06-23 2002-06-15 ARTILLERY PROJECTILE WITH EXCHANGEABLE LOAD LOAD Expired - Lifetime DE50204329D1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE50204329T DE50204329D1 (en) 2001-06-23 2002-06-15 ARTILLERY PROJECTILE WITH EXCHANGEABLE LOAD LOAD

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE10130383A DE10130383A1 (en) 2001-06-23 2001-06-23 Artillery projectile with interchangeable payload
DE50204329T DE50204329D1 (en) 2001-06-23 2002-06-15 ARTILLERY PROJECTILE WITH EXCHANGEABLE LOAD LOAD
PCT/EP2002/006623 WO2003001141A1 (en) 2001-06-23 2002-06-15 Artillery projectile comprising an interchangeable payload

Publications (1)

Publication Number Publication Date
DE50204329D1 true DE50204329D1 (en) 2006-02-02

Family

ID=7689238

Family Applications (2)

Application Number Title Priority Date Filing Date
DE10130383A Withdrawn DE10130383A1 (en) 2001-06-23 2001-06-23 Artillery projectile with interchangeable payload
DE50204329T Expired - Lifetime DE50204329D1 (en) 2001-06-23 2002-06-15 ARTILLERY PROJECTILE WITH EXCHANGEABLE LOAD LOAD

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE10130383A Withdrawn DE10130383A1 (en) 2001-06-23 2001-06-23 Artillery projectile with interchangeable payload

Country Status (7)

Country Link
US (1) US20040200375A1 (en)
EP (1) EP1399706B1 (en)
KR (1) KR100796706B1 (en)
AT (1) ATE305128T1 (en)
DE (2) DE10130383A1 (en)
IL (1) IL159502A0 (en)
WO (1) WO2003001141A1 (en)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6978967B1 (en) * 2003-04-25 2005-12-27 The United States Of America As Represented By The Secretary Of The Army Space saving fin deployment system for munitions and missiles
WO2006088687A1 (en) * 2005-02-07 2006-08-24 Bae Systems Information And Electronic Systems Integration Inc. Optically guided munition
SE528624C2 (en) 2005-11-15 2007-01-09 Bae Systems Bofors Ab Increasing a range of trajectory shells for explosive substances by utilizing folding/fixed rear guide fins with specified radial extent range and folding/fixed front steerable so-called canard fins with aerodynamic bearing surfaces
FR2910122B1 (en) * 2006-12-15 2009-03-06 Thales Sa DEPLOYABLE CARRIER EMPLOYING DEVICE FOR OBUS
EP2109752B1 (en) 2007-01-12 2014-03-05 Raytheon Company Methods and apparatus for weapon fuze
US7506587B1 (en) 2007-02-20 2009-03-24 The United States Of Americas As Represented By The Secretary Of The Navy Modular projectile system
EP3789725A1 (en) 2009-02-02 2021-03-10 Aerovironment Multimode unmanned aerial vehicle
EP2433084B1 (en) * 2009-05-19 2013-05-08 Raytheon Company Guided missile
KR101098114B1 (en) * 2009-07-06 2011-12-26 주식회사 풍산 Dual Warhead Bombshell
CN102574575B (en) 2009-09-09 2015-09-30 威罗门飞行公司 A kind of aviation aircraft
CA3041106C (en) 2009-09-09 2020-11-10 Aerovironment, Inc. Reinforced unmanned aerial vehicle launch tube
US8671839B2 (en) 2011-11-04 2014-03-18 Joseph M. Bunczk Projectile and munition including projectile
US9593922B2 (en) 2013-03-14 2017-03-14 Bae Systems Land & Armaments L.P. Fin deployment system
US9194677B1 (en) * 2013-03-26 2015-11-24 Raytheon Company Projectile with aft obturating device
DE102017105565A1 (en) * 2017-03-15 2018-09-20 Rheinmetall Waffe Munition Gmbh Ammunition and logistics concept for in particular artillery projectiles
FR3080912B1 (en) 2018-05-02 2020-04-03 Nexter Munitions PROJECTILE POWERED BY STATOREACTOR
KR102081885B1 (en) 2018-06-19 2020-02-26 주식회사 풍산 Unfolding wings apparatus of folding blade
JP7456371B2 (en) 2020-12-23 2024-03-27 三菱電機株式会社 Radome for flying objects, manufacturing method of radome for flying objects

Family Cites Families (19)

* 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
US4364530A (en) * 1980-09-08 1982-12-21 The United States Of America As Represented By The Secretary Of The Navy Propulsion/control modular booster
DE3334023A1 (en) * 1983-09-21 1985-04-04 Mauser-Werke Oberndorf Gmbh, 7238 Oberndorf BULLET BODY WITH PLASTIC GUIDE BAND
FR2654822B1 (en) * 1987-03-17 1993-04-23 Thomson Brandt Armements DISPENSER OF SUB-PROJECTILES.
US4899956A (en) 1988-07-20 1990-02-13 Teleflex, Incorporated Self-contained supplemental guidance module for projectile weapons
GB9225589D0 (en) * 1992-12-08 2003-04-16 Royal Ordnance Plc Improvements in or relating to general purpose bombs
DE59704496D1 (en) * 1996-03-08 2001-10-11 Diehl Stiftung & Co Method and device for moving a large-caliber payload over a site
US6126109A (en) * 1997-04-11 2000-10-03 Raytheon Company Unlocking tail fin assembly for guided projectiles
DE19740888C2 (en) * 1997-09-17 1999-09-02 Rheinmetall W & M Gmbh Method for autonomously steering a spin-stabilized artillery projectile and autonomously guided artillery projectile for carrying out the method
US6408762B1 (en) * 1997-12-11 2002-06-25 Lockheed Martin Corporation Clamp assembly for shrouded aerial bomb
US6227119B1 (en) * 1998-10-30 2001-05-08 Lockheed Martin Corporation Lightweight warhead assembly
DE19917189A1 (en) * 1999-04-16 2000-10-19 Diehl Stiftung & Co Warhead comprises submunition stacked in a chamber, and an expulsion system located between the submunition chambers.
US6227096B1 (en) * 1999-06-22 2001-05-08 The Boeing Company Universal warhead adapter, and missile and method incorporating same
DE19944379B4 (en) * 1999-09-16 2007-05-16 Rheinmetall Waffe Munition cartridge
SE518665C2 (en) * 2000-03-21 2002-11-05 Bofors Weapon Sys Ab Fine stabilized artillery grenade
SE518656C2 (en) * 2000-07-03 2002-11-05 Bofors Defence Ab Fine stabilized artillery grenade
SE518654C2 (en) * 2000-07-03 2002-11-05 Bofors Defence Ab Methods and apparatus for artillery projectiles
SE519757C2 (en) * 2000-08-15 2003-04-08 Bofors Defence Ab Controllable artillery projectile with extremely long range
US6502786B2 (en) * 2001-02-01 2003-01-07 United Defense, L.P. 2-D projectile trajectory corrector

Also Published As

Publication number Publication date
IL159502A0 (en) 2004-06-01
EP1399706A1 (en) 2004-03-24
KR20040011552A (en) 2004-02-05
WO2003001141A1 (en) 2003-01-03
DE10130383A1 (en) 2003-01-09
EP1399706B1 (en) 2005-09-21
ATE305128T1 (en) 2005-10-15
KR100796706B1 (en) 2008-01-21
US20040200375A1 (en) 2004-10-14

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition