IL265487A - Projectile - Google Patents

Projectile

Info

Publication number
IL265487A
IL265487A IL265487A IL26548719A IL265487A IL 265487 A IL265487 A IL 265487A IL 265487 A IL265487 A IL 265487A IL 26548719 A IL26548719 A IL 26548719A IL 265487 A IL265487 A IL 265487A
Authority
IL
Israel
Prior art keywords
projectile
Prior art date
Application number
IL265487A
Other languages
Hebrew (he)
Inventor
Stubenrauch Philipp
Original Assignee
Diehl Defence Gmbh & Co Kg
Stubenrauch Philipp
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 Diehl Defence Gmbh & Co Kg, Stubenrauch Philipp filed Critical Diehl Defence Gmbh & Co Kg
Publication of IL265487A publication Critical patent/IL265487A/en

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
    • 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
    • F42B10/20—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel deployed by combustion gas pressure, or by pneumatic or hydraulic forces

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluid-Damping Devices (AREA)
  • Toys (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
IL265487A 2018-03-21 2019-03-19 Projectile IL265487A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102018002321 2018-03-21

Publications (1)

Publication Number Publication Date
IL265487A true IL265487A (en) 2019-05-30

Family

ID=65812197

Family Applications (1)

Application Number Title Priority Date Filing Date
IL265487A IL265487A (en) 2018-03-21 2019-03-19 Projectile

Country Status (2)

Country Link
EP (1) EP3543640A3 (en)
IL (1) IL265487A (en)

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6880780B1 (en) * 2003-03-17 2005-04-19 General Dynamics Ordnance And Tactical Systems, Inc. Cover ejection and fin deployment system for a gun-launched projectile
FR2864612B1 (en) * 2003-12-24 2007-11-23 Giat Ind Sa DEVICE FOR DEPLOYING THE FINS OF A PROJECTILE
FR2949848B1 (en) 2009-09-10 2012-09-28 Nexter Munitions DEVICE FOR OPENING AND LOCKING A DUCK FIN.
FR2955653A1 (en) * 2010-01-28 2011-07-29 Nexter Munitions DEVICE FOR SIMULTANEOUS DEPLOYMENT OF GOVERNMENTS OF A PROJECTILE
FR2986319B1 (en) * 2012-01-27 2014-03-14 Tda Armements Sas PILOTAGE TRUNK FOR GUIDED MUNITION
US9702673B1 (en) * 2014-09-24 2017-07-11 The United States Of America As Represented By The Secretary Of The Army Projectile tail boom with self-locking fin
CN105737685B (en) * 2016-02-18 2017-07-21 江西洪都航空工业集团有限责任公司 A kind of two-way dibit foldable structure of aerofoil
CN106839897B (en) * 2017-01-03 2019-01-15 北京临近空间飞行器系统工程研究所 A kind of straight-line helix unfolded wing mechanism

Also Published As

Publication number Publication date
EP3543640A3 (en) 2020-01-08
EP3543640A2 (en) 2019-09-25

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