AU2001274733A1 - Fin-stabilized shell - Google Patents

Fin-stabilized shell

Info

Publication number
AU2001274733A1
AU2001274733A1 AU2001274733A AU7473301A AU2001274733A1 AU 2001274733 A1 AU2001274733 A1 AU 2001274733A1 AU 2001274733 A AU2001274733 A AU 2001274733A AU 7473301 A AU7473301 A AU 7473301A AU 2001274733 A1 AU2001274733 A1 AU 2001274733A1
Authority
AU
Australia
Prior art keywords
fin
stabilized shell
stabilized
shell
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
AU2001274733A
Inventor
Ulf Hellman
Ulf Holmqvist
Stig Johnsson
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.)
BAE Systems Bofors AB
Original Assignee
Bofors Defence AB
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 Bofors Defence AB filed Critical Bofors Defence AB
Publication of AU2001274733A1 publication Critical patent/AU2001274733A1/en
Abandoned 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
    • F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F42B10/18—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel using a longitudinally slidable support member
    • 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
    • F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/38—Range-increasing arrangements
    • F42B10/40—Range-increasing arrangements with combustion of a slow-burning charge, e.g. fumers, base-bleed projectiles
AU2001274733A 2000-07-03 2001-06-13 Fin-stabilized shell Abandoned AU2001274733A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
SE0002487 2000-07-03
SE0002487A SE518656C2 (en) 2000-07-03 2000-07-03 Fine stabilized artillery grenade
PCT/SE2001/001332 WO2002006760A1 (en) 2000-07-03 2001-06-13 Fin-stabilized shell

Publications (1)

Publication Number Publication Date
AU2001274733A1 true AU2001274733A1 (en) 2002-01-30

Family

ID=20280335

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2001274733A Abandoned AU2001274733A1 (en) 2000-07-03 2001-06-13 Fin-stabilized shell

Country Status (11)

Country Link
US (1) US6886775B2 (en)
EP (1) EP1297293B1 (en)
AU (1) AU2001274733A1 (en)
CA (1) CA2415090C (en)
DE (1) DE60140540D1 (en)
ES (1) ES2336541T3 (en)
IL (2) IL153628A0 (en)
NO (1) NO20030004L (en)
SE (1) SE518656C2 (en)
WO (1) WO2002006760A1 (en)
ZA (1) ZA200210384B (en)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0111171D0 (en) * 2001-05-08 2001-06-27 Special Cartridge Company Ltd Projictile
DE10130383A1 (en) * 2001-06-23 2003-01-09 Diehl Munitionssysteme Gmbh Artillery projectile with interchangeable payload
US7415931B2 (en) * 2005-07-20 2008-08-26 Textron Systems Corporation Methods and apparatus for active deployment of a samara wing
SE0502509L (en) * 2005-11-15 2007-01-09 Bae Systems Bofors Ab Under-calibrated grenade with long range
US7829830B1 (en) * 2007-10-19 2010-11-09 Woodward Hrt, Inc. Techniques for controlling access through a slot on a projectile
US8193476B2 (en) * 2008-06-13 2012-06-05 Raytheon Company Solid-fuel pellet thrust and control actuation system to maneuver a flight vehicle
US8158915B2 (en) * 2008-10-02 2012-04-17 Raytheon Company Canard-centric missile support
WO2011014806A1 (en) * 2009-07-31 2011-02-03 Raytheon Company Deployable fairing and method for reducing aerodynamic drag on a gun-launched artillery shell
CN102574575B (en) * 2009-09-09 2015-09-30 威罗门飞行公司 A kind of aviation aircraft
DE102009057682A1 (en) 2009-12-04 2011-06-09 Frank Lehnen Kinetic energy projectile i.e. caseless munition, has drive and resistance stabilizer for firing of smooth or profiled gun tubes, where projectile exhibits rotation symmetric tail-shape at longitudinal axis
DE202009016713U1 (en) 2009-12-04 2010-04-08 Lehnen, Frank Resistance-stabilized, wingless and powered balancing projectile
US8933383B2 (en) * 2010-09-01 2015-01-13 The United States Of America As Represented By The Secretary Of The Army Method and apparatus for correcting the trajectory of a fin-stabilized, ballistic projectile using canards
US9759535B2 (en) * 2014-04-30 2017-09-12 Bae Systems Land & Armaments L.P. Gun launched munition with strakes
US10184762B2 (en) 2015-12-01 2019-01-22 Raytheon Company Base drag reduction fairing using shape memory materials
US11796291B2 (en) * 2022-01-11 2023-10-24 Raytheon Company Effector having morphing airframe and method
FI130317B (en) * 2022-06-02 2023-06-16 Moviator Oy Projectile
IL294415B2 (en) 2022-06-29 2023-10-01 Israel Aerospace Ind Ltd Air intake module for a projectile

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2264338A1 (en) * 1972-12-30 1974-07-04 Dynamit Nobel Ag FOLD-OUT TAIL, ESPECIALLY FOR MISSILE
US3819132A (en) * 1973-02-21 1974-06-25 Sarmac Sa Self propelled projectile with fins
SE428058B (en) 1981-10-08 1983-05-30 Foerenade Fabriksverken PROJECTIL WORKS
DE3344402A1 (en) 1983-12-08 1985-06-13 Diehl GmbH & Co, 8500 Nürnberg Missile
GB2265443B (en) 1988-04-14 1994-03-23 British Aerospace Fin assembly for a projectile
US4944226A (en) * 1988-08-19 1990-07-31 General Dynamics Corp., Pomona Div. Expandable telescoped missile airframe
USH905H (en) * 1990-09-13 1991-04-02 The United States Of America As Represented By The Secretary Of The Army Fin assembly
US6126109A (en) * 1997-04-11 2000-10-03 Raytheon Company Unlocking tail fin assembly for guided projectiles
DE10015514B4 (en) * 2000-03-30 2007-10-04 Rheinmetall Waffe Munition Gmbh Wing stabilized projectile
US6571715B1 (en) * 2002-03-11 2003-06-03 Raytheon Company Boot mechanism for complex projectile base survival

Also Published As

Publication number Publication date
DE60140540D1 (en) 2009-12-31
ES2336541T3 (en) 2010-04-14
ZA200210384B (en) 2004-02-10
NO20030004D0 (en) 2003-01-02
WO2002006760A1 (en) 2002-01-24
IL153628A0 (en) 2003-07-06
US20040011919A1 (en) 2004-01-22
NO20030004L (en) 2003-02-11
EP1297293A1 (en) 2003-04-02
CA2415090C (en) 2009-02-10
EP1297293B1 (en) 2009-11-18
SE518656C2 (en) 2002-11-05
SE0002487L (en) 2002-01-04
IL153628A (en) 2013-05-30
SE0002487D0 (en) 2000-07-03
US6886775B2 (en) 2005-05-03
CA2415090A1 (en) 2002-01-24

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