GB8912632D0 - Aerofoil deployment system - Google Patents

Aerofoil deployment system

Info

Publication number
GB8912632D0
GB8912632D0 GB898912632A GB8912632A GB8912632D0 GB 8912632 D0 GB8912632 D0 GB 8912632D0 GB 898912632 A GB898912632 A GB 898912632A GB 8912632 A GB8912632 A GB 8912632A GB 8912632 D0 GB8912632 D0 GB 8912632D0
Authority
GB
United Kingdom
Prior art keywords
aerofoil
deployment system
deployment
aerofoil deployment
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.)
Pending
Application number
GB898912632A
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 GB898912632A priority Critical patent/GB8912632D0/en
Priority to IT047997A priority patent/IT9047997A1/en
Priority to DE4017504A priority patent/DE4017504A1/en
Publication of GB8912632D0 publication Critical patent/GB8912632D0/en
Pending 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

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)
GB898912632A 1989-06-02 1989-06-02 Aerofoil deployment system Pending GB8912632D0 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GB898912632A GB8912632D0 (en) 1989-06-02 1989-06-02 Aerofoil deployment system
IT047997A IT9047997A1 (en) 1989-06-02 1990-05-24 SYSTEM FOR THE DISPOSAL OF AERODYNAMIC SURFACES (AEROFOIL) ON BULLETS, MISSILES OR SIMILAR
DE4017504A DE4017504A1 (en) 1989-06-02 1990-05-31 Unfolding system for projectile flow line vane - comprises drive which activates support vane via single connecting cable.

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
GB8912632D0 true GB8912632D0 (en) 1992-11-04

Family

ID=10657733

Family Applications (1)

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

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
IT9047997A0 (en) 1990-05-24
IT9047997A1 (en) 1990-12-03
DE4017504A1 (en) 1993-07-15

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