ZA200306817B - Method of synchronizing fin fold-out on a fin-stabilized artillery shell, and an artillery shell designed in accordance therewith. - Google Patents

Method of synchronizing fin fold-out on a fin-stabilized artillery shell, and an artillery shell designed in accordance therewith. Download PDF

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Publication number
ZA200306817B
ZA200306817B ZA200306817A ZA200306817A ZA200306817B ZA 200306817 B ZA200306817 B ZA 200306817B ZA 200306817 A ZA200306817 A ZA 200306817A ZA 200306817 A ZA200306817 A ZA 200306817A ZA 200306817 B ZA200306817 B ZA 200306817B
Authority
ZA
South Africa
Prior art keywords
shell
fins
fin
fold
folded
Prior art date
Application number
ZA200306817A
Other languages
English (en)
Inventor
Stig Johnsson
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 ZA200306817B publication Critical patent/ZA200306817B/en

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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
    • F42B10/16—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
    • F42B10/02—Stabilising arrangements
    • F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
  • Magnetic Bearings And Hydrostatic Bearings (AREA)
  • Prostheses (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Powder Metallurgy (AREA)
ZA200306817A 2001-03-20 2003-09-01 Method of synchronizing fin fold-out on a fin-stabilized artillery shell, and an artillery shell designed in accordance therewith. ZA200306817B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE0100956A SE521445C2 (sv) 2001-03-20 2001-03-20 Sätt att synkronisera fenutfällningen vid en fenstabiliserad artillerigranat samt en i enlighet därmed utformad artillerigranat

Publications (1)

Publication Number Publication Date
ZA200306817B true ZA200306817B (en) 2004-09-01

Family

ID=20283429

Family Applications (1)

Application Number Title Priority Date Filing Date
ZA200306817A ZA200306817B (en) 2001-03-20 2003-09-01 Method of synchronizing fin fold-out on a fin-stabilized artillery shell, and an artillery shell designed in accordance therewith.

Country Status (8)

Country Link
US (2) US7104497B2 (fr)
EP (1) EP1370824B1 (fr)
CA (1) CA2441277C (fr)
IL (3) IL157972A0 (fr)
NO (1) NO327496B1 (fr)
SE (1) SE521445C2 (fr)
WO (1) WO2002079716A1 (fr)
ZA (1) ZA200306817B (fr)

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RU2704381C1 (ru) * 2019-02-12 2019-10-28 Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Способ аэродинамического управления летательным аппаратом
US11573069B1 (en) 2020-07-02 2023-02-07 Northrop Grumman Systems Corporation Axial flux machine for use with projectiles

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Also Published As

Publication number Publication date
CA2441277C (fr) 2009-06-09
US20070114323A1 (en) 2007-05-24
US7104497B2 (en) 2006-09-12
EP1370824A1 (fr) 2003-12-17
SE0100956L (sv) 2002-09-21
EP1370824B1 (fr) 2017-05-03
CA2441277A1 (fr) 2002-10-10
NO20034174D0 (no) 2003-09-19
US20050229806A1 (en) 2005-10-20
IL157972A0 (en) 2004-03-28
IL157972A (en) 2009-07-20
NO327496B1 (no) 2009-07-20
US7487934B2 (en) 2009-02-10
IL181105A0 (en) 2007-07-04
SE521445C2 (sv) 2003-11-04
WO2002079716A1 (fr) 2002-10-10
IL181105A (en) 2009-07-20
SE0100956D0 (sv) 2001-03-20
NO20034174L (no) 2003-11-10

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