GB2121147B - Missile fin assemblies - Google Patents

Missile fin assemblies

Info

Publication number
GB2121147B
GB2121147B GB08315131A GB8315131A GB2121147B GB 2121147 B GB2121147 B GB 2121147B GB 08315131 A GB08315131 A GB 08315131A GB 8315131 A GB8315131 A GB 8315131A GB 2121147 B GB2121147 B GB 2121147B
Authority
GB
United Kingdom
Prior art keywords
fin assemblies
missile fin
missile
assemblies
fin
Prior art date
Legal status (The legal status 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 status listed.)
Expired
Application number
GB08315131A
Other versions
GB2121147A (en
Inventor
Laurence Goodwin
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BAE Systems PLC
Original Assignee
British Aerospace PLC
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 British Aerospace PLC filed Critical British Aerospace PLC
Priority to GB08315131A priority Critical patent/GB2121147B/en
Publication of GB2121147A publication Critical patent/GB2121147A/en
Application granted granted Critical
Publication of GB2121147B publication Critical patent/GB2121147B/en
Expired legal-status Critical Current

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

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)
GB08315131A 1982-06-02 1983-06-02 Missile fin assemblies Expired GB2121147B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB08315131A GB2121147B (en) 1982-06-02 1983-06-02 Missile fin assemblies

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB8215895 1982-06-02
GB08315131A GB2121147B (en) 1982-06-02 1983-06-02 Missile fin assemblies

Publications (2)

Publication Number Publication Date
GB2121147A GB2121147A (en) 1983-12-14
GB2121147B true GB2121147B (en) 1985-10-16

Family

ID=26283002

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08315131A Expired GB2121147B (en) 1982-06-02 1983-06-02 Missile fin assemblies

Country Status (1)

Country Link
GB (1) GB2121147B (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3408585A1 (en) * 1984-03-09 1985-09-12 Rheinmetall GmbH, 4000 Düsseldorf WING STABILIZED SHELL
GB2168794B (en) * 1984-10-01 1987-12-23 Commw Of Australia Wing or fin deploying mechanism
GB8609166D0 (en) * 1986-04-15 1986-09-17 British Aerospace Deployment arrangement for spinning body
FR2617587B1 (en) * 1987-07-03 1993-04-16 Thomson Brandt Armements DEVICE FOR CONJUGATED DEPLOYMENT OF WINGS, AND APPLICATION TO A FLYING MACHINE
DE3730019C1 (en) * 1987-09-08 1988-12-22 Diehl Gmbh & Co Submunition missile
DE3915585A1 (en) * 1989-05-12 1990-11-15 Diehl Gmbh & Co SUBMUNITION MISSILE
US5816532A (en) * 1996-12-17 1998-10-06 Northrop Grumman Corporation Multiposition folding control surface for improved launch stability in missiles
RU2520846C1 (en) * 2013-03-29 2014-06-27 Открытое акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Rocket aerodynamic rudder
SE540036C2 (en) 2013-10-10 2018-03-06 Bae Systems Bofors Ab Fen-precipitation mechanism and method for fen-precipitation
IL231186A (en) * 2014-02-26 2017-07-31 Israel Aerospace Ind Ltd Fin deployment system
RU2587751C1 (en) * 2015-03-16 2016-06-20 Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Deployable rudder

Also Published As

Publication number Publication date
GB2121147A (en) 1983-12-14

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee