ATE305128T1 - ARTILLERY PROJECTILE WITH INTERCHANGEABLE PAYLOAD - Google Patents
ARTILLERY PROJECTILE WITH INTERCHANGEABLE PAYLOADInfo
- Publication number
- ATE305128T1 ATE305128T1 AT02754685T AT02754685T ATE305128T1 AT E305128 T1 ATE305128 T1 AT E305128T1 AT 02754685 T AT02754685 T AT 02754685T AT 02754685 T AT02754685 T AT 02754685T AT E305128 T1 ATE305128 T1 AT E305128T1
- Authority
- AT
- Austria
- Prior art keywords
- section
- standardized
- artillery projectile
- tail section
- interchangeable payload
- Prior art date
Links
- 239000004429 Calibre Substances 0.000 abstract 1
- 230000006641 stabilisation Effects 0.000 abstract 1
- 238000011105 stabilization Methods 0.000 abstract 1
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)
- Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
- Braking Arrangements (AREA)
- Pharmaceuticals Containing Other Organic And Inorganic Compounds (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).
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE10130383A DE10130383A1 (en) | 2001-06-23 | 2001-06-23 | Artillery projectile with interchangeable payload |
| PCT/EP2002/006623 WO2003001141A1 (en) | 2001-06-23 | 2002-06-15 | Artillery projectile comprising an interchangeable payload |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE305128T1 true ATE305128T1 (en) | 2005-10-15 |
Family
ID=7689238
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT02754685T ATE305128T1 (en) | 2001-06-23 | 2002-06-15 | 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 (20)
| 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 |
| US7533849B2 (en) * | 2005-02-07 | 2009-05-19 | Bae Systems Information And Electronic Systems Integration Inc. | Optically guided munition |
| SE528624C2 (en) * | 2005-11-15 | 2007-01-09 | Bae Systems Bofors Ab | Under-calibrated grenade with long range |
| 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 |
| KR101730664B1 (en) | 2009-02-02 | 2017-04-26 | 에어로바이론먼트, 인크. | Multimode unmanned aerial vehicle |
| US20120068002A1 (en) * | 2009-05-19 | 2012-03-22 | Unger Michael P | Guided missile |
| KR101098114B1 (en) * | 2009-07-06 | 2011-12-26 | 주식회사 풍산 | Dual Warhead Bombshell |
| JP5886201B2 (en) | 2009-09-09 | 2016-03-16 | エアロバイロメント, インコーポレイテッドAerovironment, Inc. | Elevon control system |
| DK3133019T3 (en) | 2009-09-09 | 2019-02-18 | Aerovironment Inc | NOISE DEVICE FOR A DRONE PROTECTION PIPE |
| 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 |
| US12392588B1 (en) * | 2024-04-09 | 2025-08-19 | United States Of America As Represented By The Secretary Of The Air Force | Expanding fin rocket with fin restraint |
| CN118224936A (en) * | 2024-04-25 | 2024-06-21 | 西北工业大学 | High-speed water entry stabilization device for missile and missile |
Family Cites Families (19)
| 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 |
| EP0794405B1 (en) * | 1996-03-08 | 2001-09-05 | Diehl Stiftung & Co. | Method and device for dispersing a large caliber payload above a target |
| 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 |
| SE518654C2 (en) * | 2000-07-03 | 2002-11-05 | Bofors Defence Ab | Methods and apparatus for artillery projectiles |
| SE518656C2 (en) * | 2000-07-03 | 2002-11-05 | Bofors Defence Ab | Fine stabilized artillery grenade |
| SE519757C2 (en) * | 2000-08-15 | 2003-04-08 | Bofors Defence Ab | Controllable artillery projectile with extremely long range |
| DE60233113D1 (en) * | 2001-02-01 | 2009-09-10 | Bae Systems Land & Armaments | TWO-DIMENSIONAL STORE FLIGHT GATE CORRECTION DEVICE |
-
2001
- 2001-06-23 DE DE10130383A patent/DE10130383A1/en not_active Withdrawn
-
2002
- 2002-06-15 EP EP02754685A patent/EP1399706B1/en not_active Expired - Lifetime
- 2002-06-15 IL IL15950202A patent/IL159502A0/en unknown
- 2002-06-15 AT AT02754685T patent/ATE305128T1/en not_active IP Right Cessation
- 2002-06-15 KR KR1020037016819A patent/KR100796706B1/en not_active Expired - Fee Related
- 2002-06-15 WO PCT/EP2002/006623 patent/WO2003001141A1/en not_active Ceased
- 2002-06-15 US US10/481,201 patent/US20040200375A1/en not_active Abandoned
- 2002-06-15 DE DE50204329T patent/DE50204329D1/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| KR20040011552A (en) | 2004-02-05 |
| EP1399706A1 (en) | 2004-03-24 |
| EP1399706B1 (en) | 2005-09-21 |
| US20040200375A1 (en) | 2004-10-14 |
| DE50204329D1 (en) | 2006-02-02 |
| KR100796706B1 (en) | 2008-01-21 |
| WO2003001141A1 (en) | 2003-01-03 |
| DE10130383A1 (en) | 2003-01-09 |
| IL159502A0 (en) | 2004-06-01 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| REN | Ceased due to non-payment of the annual fee |