Nothing Special   »   [go: up one dir, main page]

IT9047997A0 - SYSTEM FOR THE DEPLOYMENT OF AERODYNAMIC SURFACES (AEROFOIL) ON PROJECTILES, MISSILES OR SIMILAR - Google Patents

SYSTEM FOR THE DEPLOYMENT OF AERODYNAMIC SURFACES (AEROFOIL) ON PROJECTILES, MISSILES OR SIMILAR

Info

Publication number
IT9047997A0
IT9047997A0 IT9047997A IT4799790A IT9047997A0 IT 9047997 A0 IT9047997 A0 IT 9047997A0 IT 9047997 A IT9047997 A IT 9047997A IT 4799790 A IT4799790 A IT 4799790A IT 9047997 A0 IT9047997 A0 IT 9047997A0
Authority
IT
Italy
Prior art keywords
missiles
aerofoil
projectiles
deployment
similar
Prior art date
Application number
IT9047997A
Other languages
Italian (it)
Other versions
IT9047997A1 (en
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 filed Critical
Publication of IT9047997A0 publication Critical patent/IT9047997A0/en
Publication of IT9047997A1 publication Critical patent/IT9047997A1/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

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
IT047997A 1989-06-02 1990-05-24 SYSTEM FOR THE DISPOSAL OF AERODYNAMIC SURFACES (AEROFOIL) ON BULLETS, MISSILES OR SIMILAR IT9047997A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB898912632A GB8912632D0 (en) 1989-06-02 1989-06-02 Aerofoil deployment system

Publications (2)

Publication Number Publication Date
IT9047997A0 true IT9047997A0 (en) 1990-05-24
IT9047997A1 IT9047997A1 (en) 1990-12-03

Family

ID=10657733

Family Applications (1)

Application Number Title Priority Date Filing Date
IT047997A IT9047997A1 (en) 1989-06-02 1990-05-24 SYSTEM FOR THE DISPOSAL OF AERODYNAMIC SURFACES (AEROFOIL) ON BULLETS, MISSILES OR SIMILAR

Country Status (3)

Country Link
DE (1) DE4017504A1 (en)
GB (1) GB8912632D0 (en)
IT (1) IT9047997A1 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19941555C5 (en) * 1999-09-01 2004-12-30 Rheinmetall W & M Gmbh missile
FR2895071B1 (en) * 2005-12-19 2008-01-18 Giat Ind Sa ANTI-REBOUND LOCKING DEVICE OF A DEPLOYABLE FIN OF A PROJECTILE.
US8338769B1 (en) * 2008-02-07 2012-12-25 Simmonds Precision Products, Inc. Pyrotechnic fin deployment and retention mechanism
CN101973390B (en) * 2010-09-25 2013-05-22 中国航天科工集团第二研究院二一〇所 Unfolding mechanism for foldable double wing boards of aircraft
CN103963960B (en) * 2014-05-14 2016-08-24 北京航空航天大学 A kind of semi-rigid inflated type opens up receipts wing automatically

Also Published As

Publication number Publication date
DE4017504A1 (en) 1993-07-15
GB8912632D0 (en) 1992-11-04
IT9047997A1 (en) 1990-12-03

Similar Documents

Publication Publication Date Title
IT8224675A0 (en) INSTALLATION SYSTEM OF GONDOLA OR NASCELLA FOR AIRCRAFT ENGINES.
IT8620137A0 (en) AIR CONTROL SYSTEM ESPECIALLY FOR AIRCRAFT ENGINES.
NO874474D0 (en) WINGS FOR SUPERSONIC WEIGHT OR COMPRESSOR.
ES2014029B3 (en) CONTROL SYSTEM OF THE HYPER-SUSTAINING WINGS OF AN AIRCRAFT.
FR2653742B1 (en) AIRPLANE PROPELLER.
DE68919297D1 (en) Trajectory improvement system for missiles with controllable trajectory.
IT1206865B (en) AIMING SYSTEM FOR ARTILLERY
PT88987A (en) LANDING COATING SYSTEM
IT9047997A0 (en) SYSTEM FOR THE DEPLOYMENT OF AERODYNAMIC SURFACES (AEROFOIL) ON PROJECTILES, MISSILES OR SIMILAR
NO174365C (en) Gas generator missile launch system
NO904331D0 (en) DEVICE FOR EMISSION OF NAVLE CORD-GUIDED MISSILES.
IT1236706B (en) SYNCHROPHASE SYSTEM FOR AIRPLANE TURBOMOTOR.
DE69010356D1 (en) Ejectable aerodynamic rudder.
FI870837A0 (en) PRINCIPLE FOR LAGRING AV GAS ELLER VAETSKA.
NO905283D0 (en) MISSILE SYSTEM.
IT8867328A0 (en) PROCEDURE AND PROJECTILE FOR THE NEUTRALIZATION OF TARGETS, PARTICULARLY HELICOPTERS OR SHIPS
IT1229341B (en) TARGET LOCATION SYSTEM.
FI920872A0 (en) FOERBAETTRINGAR I SKYDDSHJAELMAR ELLER I ANSLUTNING TILL DESSA.
FI903920A0 (en) FOERBAETTRINGAR I ELLER I ANSLUTNING TILL UPPHETTNINGSBARA VATTENHALTIGA FOTOPOLYMERER.
FR2686409B1 (en) PILOTABLE SUPERSONIC PROJECTILE.
DE59007432D1 (en) Aerodynamic plain bearing.
ES555767A0 (en) PROCEDURE FOR DIRECTING A LOW SPEED MISSILE, A WEAPON SYSTEM USED FOR THE SAME AND A MISSILE FOR THE IMPLEMENTATION OF SUCH PROCEDURE
NO892613D0 (en) Fuselage of an aircraft.
FR2709824B1 (en) Method of readjusting the altitude provided by an altimeter on board an aircraft.
SE8903138D0 (en) LAUNCH MECHANISM FOR THE AIRCRAFT