ZA200210384B - Fin-stabilized shell. - Google Patents

Fin-stabilized shell. Download PDF

Info

Publication number
ZA200210384B
ZA200210384B ZA200210384A ZA200210384A ZA200210384B ZA 200210384 B ZA200210384 B ZA 200210384B ZA 200210384 A ZA200210384 A ZA 200210384A ZA 200210384 A ZA200210384 A ZA 200210384A ZA 200210384 B ZA200210384 B ZA 200210384B
Authority
ZA
South Africa
Prior art keywords
shell
fins
body part
fin
retracted
Prior art date
Application number
ZA200210384A
Other languages
English (en)
Inventor
Stig Johnsson
Ulf Hellman
Ulf Holmqvist
Original Assignee
Bofors Defence Aktiebolag
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 Aktiebolag filed Critical Bofors Defence Aktiebolag
Publication of ZA200210384B publication Critical patent/ZA200210384B/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/02Stabilising arrangements
    • F42B10/14Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F42B10/18Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel using a longitudinally slidable support member
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/02Stabilising arrangements
    • F42B10/14Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F42B10/16Wrap-around fins
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/32Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/38Range-increasing arrangements
    • F42B10/40Range-increasing arrangements with combustion of a slow-burning charge, e.g. fumers, base-bleed projectiles

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Automotive Seat Belt Assembly (AREA)
  • Toys (AREA)
  • Prostheses (AREA)
  • Braking Systems And Boosters (AREA)
  • Air Bags (AREA)
ZA200210384A 2000-07-03 2002-12-20 Fin-stabilized shell. ZA200210384B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE0002487A SE518656C2 (sv) 2000-07-03 2000-07-03 Fenstabiliserad artillerigranat

Publications (1)

Publication Number Publication Date
ZA200210384B true ZA200210384B (en) 2004-02-10

Family

ID=20280335

Family Applications (1)

Application Number Title Priority Date Filing Date
ZA200210384A ZA200210384B (en) 2000-07-03 2002-12-20 Fin-stabilized shell.

Country Status (11)

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

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 (de) * 2001-06-23 2003-01-09 Diehl Munitionssysteme Gmbh Artillerie-Projektil mit austauschbarer Nutzlast
US7415931B2 (en) * 2005-07-20 2008-08-26 Textron Systems Corporation Methods and apparatus for active deployment of a samara wing
SE0502509L (sv) * 2005-11-15 2007-01-09 Bae Systems Bofors Ab Underkalibrerad granat med lång räckvidd
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
EP2459956B1 (de) * 2009-07-31 2014-12-24 Raytheon Company Einsetzbare verkleidung und verfahren zur verringerung des luftwiderstandes bei einer waffenabgefeuerten granate
EP2475575B1 (de) * 2009-09-09 2017-11-01 AeroVironment, Inc. UAV mit ausfahrbaren Flügeln und Flugsteuerungsverfahren
DE202009016713U1 (de) 2009-12-04 2010-04-08 Lehnen, Frank Widerstandsstabilisiertes, flügelloses und angetriebenes Wuchtgeschoss
DE102009057682A1 (de) 2009-12-04 2011-06-09 Frank Lehnen Widerstandsstabilisiertes, flügelloses und angetriebenes Wuchtgeschoss
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 (fi) * 2022-06-02 2023-06-16 Moviator Oy Ammus
IL294415B2 (en) 2022-06-29 2023-10-01 Israel Aerospace Ind Ltd Air receiver module for the missile

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2264338A1 (de) * 1972-12-30 1974-07-04 Dynamit Nobel Ag Ausklappbares leitwerk, insbesondere fuer raketen
US3819132A (en) * 1973-02-21 1974-06-25 Sarmac Sa Self propelled projectile with fins
SE428058B (sv) 1981-10-08 1983-05-30 Foerenade Fabriksverken Styrverk for projektil
DE3344402A1 (de) 1983-12-08 1985-06-13 Diehl GmbH & Co, 8500 Nürnberg Flugkoerper
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 (de) * 2000-03-30 2007-10-04 Rheinmetall Waffe Munition Gmbh Flügelstabilisiertes Geschoß
US6571715B1 (en) * 2002-03-11 2003-06-03 Raytheon Company Boot mechanism for complex projectile base survival

Also Published As

Publication number Publication date
SE518656C2 (sv) 2002-11-05
IL153628A (en) 2013-05-30
IL153628A0 (en) 2003-07-06
NO20030004D0 (no) 2003-01-02
NO20030004L (no) 2003-02-11
CA2415090A1 (en) 2002-01-24
SE0002487L (sv) 2002-01-04
CA2415090C (en) 2009-02-10
ES2336541T3 (es) 2010-04-14
EP1297293B1 (de) 2009-11-18
US20040011919A1 (en) 2004-01-22
DE60140540D1 (de) 2009-12-31
EP1297293A1 (de) 2003-04-02
SE0002487D0 (sv) 2000-07-03
AU2001274733A1 (en) 2002-01-30
WO2002006760A1 (en) 2002-01-24
US6886775B2 (en) 2005-05-03

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