IL157972A0 - Method of synchronizing fin fold-out on a fit-stabilized artillery shell, and an artillery shell designed in accordance therewith - Google Patents

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

Info

Publication number
IL157972A0
IL157972A0 IL15797202A IL15797202A IL157972A0 IL 157972 A0 IL157972 A0 IL 157972A0 IL 15797202 A IL15797202 A IL 15797202A IL 15797202 A IL15797202 A IL 15797202A IL 157972 A0 IL157972 A0 IL 157972A0
Authority
IL
Israel
Prior art keywords
artillery shell
synchronizing
fit
accordance therewith
stabilized
Prior art date
Application number
IL15797202A
Other languages
English (en)
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 IL157972A0 publication Critical patent/IL157972A0/xx

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
    • F42B10/16—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)
  • Radar Systems Or Details Thereof (AREA)
  • Prostheses (AREA)
  • Powder Metallurgy (AREA)
IL15797202A 2001-03-20 2002-03-20 Method of synchronizing fin fold-out on a fit-stabilized artillery shell, and an artillery shell designed in accordance therewith IL157972A0 (en)

Applications Claiming Priority (2)

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
PCT/SE2002/000550 WO2002079716A1 (en) 2001-03-20 2002-03-20 Method of synchronizing fin fold-out on a fin-stabilized artillery shell, and an artillery shell designed in accordance therewith

Publications (1)

Publication Number Publication Date
IL157972A0 true IL157972A0 (en) 2004-03-28

Family

ID=20283429

Family Applications (3)

Application Number Title Priority Date Filing Date
IL15797202A IL157972A0 (en) 2001-03-20 2002-03-20 Method of synchronizing fin fold-out on a fit-stabilized artillery shell, and an artillery shell designed in accordance therewith
IL157972A IL157972A (en) 2001-03-20 2003-09-17 Fin-stabilized artillery shell with synchronized fin fold-out
IL181105A IL181105A (en) 2001-03-20 2007-02-01 Method of synchronizing fin fold-out on a fin-stabilized artillery shell and an artillery shell designed in accordance therewith

Family Applications After (2)

Application Number Title Priority Date Filing Date
IL157972A IL157972A (en) 2001-03-20 2003-09-17 Fin-stabilized artillery shell with synchronized fin fold-out
IL181105A IL181105A (en) 2001-03-20 2007-02-01 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 (sv)
EP (1) EP1370824B1 (sv)
CA (1) CA2441277C (sv)
IL (3) IL157972A0 (sv)
NO (1) NO327496B1 (sv)
SE (1) SE521445C2 (sv)
WO (1) WO2002079716A1 (sv)
ZA (1) ZA200306817B (sv)

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US10184762B2 (en) * 2015-12-01 2019-01-22 Raytheon Company Base drag reduction fairing using shape memory materials
FR3054030B1 (fr) * 2016-07-18 2018-08-24 Nexter Munitions Projectile comprenant un dispositif de deploiement d'une voilure ou ailette
US11555679B1 (en) 2017-07-07 2023-01-17 Northrop Grumman Systems Corporation Active spin control
US11578956B1 (en) 2017-11-01 2023-02-14 Northrop Grumman Systems Corporation Detecting body spin on a projectile
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FR3089620B1 (fr) * 2018-12-11 2022-04-01 Nexter Munitions Projectile a plans de voilure deployables
DE102018133113A1 (de) * 2018-12-20 2020-06-25 Rheinmetall Air Defence Ag Lenkflugkörper mit mehreren mittels einer Antriebsanordnung drehbaren Flügeln mit mindestens einem Aktuator und mindestens einem Planetengetriebe
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
ZA200306817B (en) 2004-09-01
SE0100956L (sv) 2002-09-21
IL157972A (en) 2009-07-20
WO2002079716A1 (en) 2002-10-10
CA2441277C (en) 2009-06-09
NO327496B1 (no) 2009-07-20
CA2441277A1 (en) 2002-10-10
US20050229806A1 (en) 2005-10-20
IL181105A (en) 2009-07-20
US7487934B2 (en) 2009-02-10
SE0100956D0 (sv) 2001-03-20
EP1370824A1 (en) 2003-12-17
US7104497B2 (en) 2006-09-12
SE521445C2 (sv) 2003-11-04
NO20034174D0 (no) 2003-09-19
IL181105A0 (en) 2007-07-04
EP1370824B1 (en) 2017-05-03
US20070114323A1 (en) 2007-05-24
NO20034174L (no) 2003-11-10

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