DE502006000632D1 - Wing arrangement and missile - Google Patents

Wing arrangement and missile

Info

Publication number
DE502006000632D1
DE502006000632D1 DE502006000632T DE502006000632T DE502006000632D1 DE 502006000632 D1 DE502006000632 D1 DE 502006000632D1 DE 502006000632 T DE502006000632 T DE 502006000632T DE 502006000632 T DE502006000632 T DE 502006000632T DE 502006000632 D1 DE502006000632 D1 DE 502006000632D1
Authority
DE
Germany
Prior art keywords
missile
wing arrangement
wing
arrangement
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.)
Active
Application number
DE502006000632T
Other languages
German (de)
Inventor
Peter Gerd Fisch
Alexander Stengele
Gerd Elsner
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.)
Diehl BGT Defence GmbH and Co KG
Original Assignee
Diehl BGT Defence GmbH and Co KG
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 BGT Defence GmbH and Co KG filed Critical Diehl BGT Defence GmbH and Co KG
Publication of DE502006000632D1 publication Critical patent/DE502006000632D1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F42B10/04—Stabilising arrangements using fixed fins
    • F42B10/06—Tail 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)
DE502006000632T 2005-06-07 2006-05-16 Wing arrangement and missile Active DE502006000632D1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102005026070A DE102005026070B4 (en) 2005-06-07 2005-06-07 Wing arrangement and missile

Publications (1)

Publication Number Publication Date
DE502006000632D1 true DE502006000632D1 (en) 2008-05-29

Family

ID=36942557

Family Applications (2)

Application Number Title Priority Date Filing Date
DE102005026070A Expired - Fee Related DE102005026070B4 (en) 2005-06-07 2005-06-07 Wing arrangement and missile
DE502006000632T Active DE502006000632D1 (en) 2005-06-07 2006-05-16 Wing arrangement and missile

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE102005026070A Expired - Fee Related DE102005026070B4 (en) 2005-06-07 2005-06-07 Wing arrangement and missile

Country Status (3)

Country Link
US (1) US20070075183A1 (en)
EP (1) EP1731871B1 (en)
DE (2) DE102005026070B4 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7800032B1 (en) * 2006-11-30 2010-09-21 Raytheon Company Detachable aerodynamic missile stabilizing system
DE102010025174A1 (en) * 2010-06-25 2011-12-29 Rheinmetall Waffe Munition Gmbh Missile, especially mortar shell
US12050092B2 (en) 2022-09-22 2024-07-30 Raytheon Company Mechanism for attachment and detachment of an airfoil to an airframe
CN116878340B (en) * 2023-09-07 2023-12-29 北京爱思达航天科技有限公司 Large-bearing light composite material flying wing and preparation method thereof

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1509336A (en) * 1922-06-27 1924-09-23 William A Borden Stabilizer or fin assembly of a bomb
US1515705A (en) * 1923-05-04 1924-11-18 Short Frank Bomb
US2597703A (en) * 1946-02-07 1952-05-20 Us Navy Rocket fin
US2771842A (en) * 1953-08-21 1956-11-27 Hillmer Willy Toggle clamp fin retaining band
DE1116577B (en) * 1959-11-21 1961-11-02 Kunststofftechnische Studienge Plastic tail wing for rockets
FR1307270A (en) * 1961-06-08 1962-10-26 Le Ministre Des Armees Terre D Tailplane for projectile and method of assembly
DE1897816U (en) * 1964-04-21 1964-07-30 J G W Berckholtz Fa STABILIZING SLEEVE FOR MISSILE, IN PARTICULAR MISSILE
US3374969A (en) * 1966-07-28 1968-03-26 Army Usa Stabilized projectile
SE339646B (en) * 1970-01-08 1971-10-11 Bofors Ab
US3633846A (en) * 1970-05-28 1972-01-11 Us Navy Expandable aerodynamic fin
US4708304A (en) * 1985-12-27 1987-11-24 General Dynamics, Pomona Division Ring-wing
FR2630502B1 (en) * 1988-04-25 1990-08-31 Europ Propulsion COMPOSITE PROPELLER WITH INTEGRATED COMPOSITE WINGS AND MANUFACTURING METHOD THEREOF
DE8901940U1 (en) * 1989-02-18 1989-05-11 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Missile with tail fins
DE3927798A1 (en) * 1989-08-23 1991-03-14 Rheinmetall Gmbh Stable missile tail unit - consists of aluminium or steel with low resistance or relatively high wt.
US5927643A (en) * 1997-11-05 1999-07-27 Atlantic Research Corporation Self-deploying airfoil for missile or the like

Also Published As

Publication number Publication date
DE102005026070A1 (en) 2006-12-14
US20070075183A1 (en) 2007-04-05
DE102005026070B4 (en) 2009-07-09
EP1731871B1 (en) 2008-04-16
EP1731871A1 (en) 2006-12-13

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition