GB2388094B - Missile with variable flying surface - Google Patents

Missile with variable flying surface

Info

Publication number
GB2388094B
GB2388094B GB8718410A GB8718410A GB2388094B GB 2388094 B GB2388094 B GB 2388094B GB 8718410 A GB8718410 A GB 8718410A GB 8718410 A GB8718410 A GB 8718410A GB 2388094 B GB2388094 B GB 2388094B
Authority
GB
United Kingdom
Prior art keywords
missile
flying surface
variable flying
variable
flying
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 - Fee Related
Application number
GB8718410A
Other versions
GB8718410D0 (en
GB2388094A (en
Inventor
Pierre Allard
Jean-Claude Pascal
Michel Dalle
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.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Publication of GB8718410D0 publication Critical patent/GB8718410D0/en
Publication of GB2388094A publication Critical patent/GB2388094A/en
Application granted granted Critical
Publication of GB2388094B publication Critical patent/GB2388094B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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
    • F42B10/20Stabilising 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)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Toys (AREA)
GB8718410A 1986-08-12 1987-08-04 Missile with variable flying surface Expired - Fee Related GB2388094B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8611629A FR2812936A1 (en) 1986-08-12 1986-08-12 Missile with variable wing configuration has moving wings extending from slots in hollow fixed wings on missile body

Publications (3)

Publication Number Publication Date
GB8718410D0 GB8718410D0 (en) 2003-07-30
GB2388094A GB2388094A (en) 2003-11-05
GB2388094B true GB2388094B (en) 2004-04-07

Family

ID=9338235

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8718410A Expired - Fee Related GB2388094B (en) 1986-08-12 1987-08-04 Missile with variable flying surface

Country Status (3)

Country Link
DE (1) DE3726735B3 (en)
FR (1) FR2812936A1 (en)
GB (1) GB2388094B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106741850B (en) * 2016-11-17 2019-01-15 北京临近空间飞行器系统工程研究所 A kind of deformable lateral stabilization suitable for high-speed aircraft
DE102019002705A1 (en) * 2019-04-12 2020-10-15 Mbda Deutschland Gmbh Cruise missile and methods of controlling a cruise missile

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB454556A (en) * 1935-03-27 1936-09-28 Rose Macdonald Improvements relating to aircraft
GB506136A (en) * 1938-09-14 1939-05-23 Michael Gliwa Improvements in or relating to wings for aircraft
GB564925A (en) * 1943-03-25 1944-10-19 Alfred Eric Budd Improvements in and relating to aircraft
US3053484A (en) * 1960-07-07 1962-09-11 Jr William J Alford Variable sweep wing configuration
GB1209189A (en) * 1967-05-23 1970-10-21 Dassault Avions A device for pivotally connecting the variable sweep wings of a variable geometry aircraft to the aircraft fuselage
EP0171473A1 (en) * 1984-06-04 1986-02-19 The State Of Israel Ministry Of Defence Israel Military Industries A projectile stabilization system
EP0209761A1 (en) * 1985-07-03 1987-01-28 DIEHL GMBH & CO. Missile with erectable wings
EP0251890A1 (en) * 1986-06-27 1988-01-07 Thomson-Brandt Armements Multiple unfolding wing, and its use in an aircraft missile

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2596436A (en) * 1947-03-11 1952-05-13 Robert Roger Aime Folding wing for aircraft
LU33739A1 (en) * 1955-07-21
GB1597098A (en) * 1971-06-23 1981-09-03 British Aerospace Missiles
AU524255B2 (en) * 1978-12-29 1982-09-09 Commonwealth Of Australia, The Deployable wing
US4336914A (en) * 1978-12-29 1982-06-29 The Commonwealth Of Australia Deployable wing mechanism
FR2530332B1 (en) * 1982-07-16 1987-01-02 Europ Propulsion DEVICE FOR OPENING THE SOCKET OF A PROJECTILE
DE3417082A1 (en) * 1984-05-09 1985-11-14 Diehl GmbH & Co, 8500 Nürnberg FOLDING WING, IN PARTICULAR FOR ONE STOREY
DE3432614A1 (en) * 1984-09-05 1986-03-13 Rheinmetall GmbH, 4000 Düsseldorf MISSILE

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB454556A (en) * 1935-03-27 1936-09-28 Rose Macdonald Improvements relating to aircraft
GB506136A (en) * 1938-09-14 1939-05-23 Michael Gliwa Improvements in or relating to wings for aircraft
GB564925A (en) * 1943-03-25 1944-10-19 Alfred Eric Budd Improvements in and relating to aircraft
US3053484A (en) * 1960-07-07 1962-09-11 Jr William J Alford Variable sweep wing configuration
GB1209189A (en) * 1967-05-23 1970-10-21 Dassault Avions A device for pivotally connecting the variable sweep wings of a variable geometry aircraft to the aircraft fuselage
EP0171473A1 (en) * 1984-06-04 1986-02-19 The State Of Israel Ministry Of Defence Israel Military Industries A projectile stabilization system
EP0209761A1 (en) * 1985-07-03 1987-01-28 DIEHL GMBH & CO. Missile with erectable wings
EP0251890A1 (en) * 1986-06-27 1988-01-07 Thomson-Brandt Armements Multiple unfolding wing, and its use in an aircraft missile

Also Published As

Publication number Publication date
FR2812936A1 (en) 2002-02-15
GB8718410D0 (en) 2003-07-30
GB2388094A (en) 2003-11-05
DE3726735B3 (en) 2004-02-05

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Legal Events

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

Effective date: 20040707