GB2154715B - Aerodynamic stabilisation mechanism for missiles - Google Patents

Aerodynamic stabilisation mechanism for missiles

Info

Publication number
GB2154715B
GB2154715B GB08501791A GB8501791A GB2154715B GB 2154715 B GB2154715 B GB 2154715B GB 08501791 A GB08501791 A GB 08501791A GB 8501791 A GB8501791 A GB 8501791A GB 2154715 B GB2154715 B GB 2154715B
Authority
GB
United Kingdom
Prior art keywords
missiles
stabilisation mechanism
aerodynamic
aerodynamic stabilisation
stabilisation
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
GB08501791A
Other versions
GB2154715A (en
GB8501791D0 (en
Inventor
Horst Hutter
Siegfried Bock
Oswald Pepina
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 Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of GB8501791D0 publication Critical patent/GB8501791D0/en
Publication of GB2154715A publication Critical patent/GB2154715A/en
Application granted granted Critical
Publication of GB2154715B publication Critical patent/GB2154715B/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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/10—Stabilising surfaces adjustable
    • B64C5/12—Stabilising surfaces adjustable for retraction against or within fuselage or nacelle

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)
  • Clamps And Clips (AREA)
GB08501791A 1984-02-18 1985-01-24 Aerodynamic stabilisation mechanism for missiles Expired GB2154715B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19843405974 DE3405974C1 (en) 1984-02-18 1984-02-18 Aerodynamic stabilization device for missiles

Publications (3)

Publication Number Publication Date
GB8501791D0 GB8501791D0 (en) 1985-02-27
GB2154715A GB2154715A (en) 1985-09-11
GB2154715B true GB2154715B (en) 1987-12-23

Family

ID=6228203

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08501791A Expired GB2154715B (en) 1984-02-18 1985-01-24 Aerodynamic stabilisation mechanism for missiles

Country Status (3)

Country Link
DE (1) DE3405974C1 (en)
FR (1) FR2559894B1 (en)
GB (1) GB2154715B (en)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2369177A (en) * 1989-06-02 2002-05-22 British Aerospace Aerofoil deployment system
DE4119613C2 (en) * 1991-06-14 1997-03-27 Diehl Gmbh & Co Missiles with fold-out guidance devices
US5671899A (en) * 1996-02-26 1997-09-30 Lockheed Martin Corporation Airborne vehicle with wing extension and roll control
US5829715A (en) * 1996-04-19 1998-11-03 Lockheed Martin Vought Systems Corp. Multi-axis unfolding mechanism with rate controlled synchronized movement
US6092264A (en) * 1998-11-13 2000-07-25 Lockheed Martin Corporation Single axis fold actuator and lock for member
US7338010B2 (en) * 2004-02-07 2008-03-04 Raytheon Company Air-launchable aircraft and method of use
RU2463210C1 (en) * 2011-05-13 2012-10-10 Открытое акционерное общество "Корпорация "Тактическое ракетное вооружение" Aircraft outer wing deployment and fixation device
CN105173082B (en) * 2015-09-15 2017-04-12 航宇救生装备有限公司 Heavy-load air drop discharge safety mechanism
CN107458578A (en) * 2017-08-09 2017-12-12 中北大学 Imitative flying fish formula flight bus
CN109383815B (en) * 2018-11-21 2023-10-20 航宇救生装备有限公司 Pneumatic unlocking cabin opening mechanism
AU2021252429A1 (en) * 2020-04-06 2022-10-06 Skyborne Technologies Pty Ltd A glide bomb and method of use thereof
DE102021001038B4 (en) 2021-02-26 2023-01-19 Diehl Defence Gmbh & Co. Kg Aircraft with wing folding mechanism

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR715385A (en) * 1931-08-10 1931-12-02 Folding tail for aviation bombs
GB759679A (en) * 1949-04-29 1956-10-24 Vickers Armstrongs Aircraft Improvements in guided missiles
US3113486A (en) * 1959-06-10 1963-12-10 Kongelbeck Sverre Turrent launcher
US3273500A (en) * 1965-01-25 1966-09-20 Kongelbeck Sverre Self-erecting folding fin
US3350984A (en) * 1966-03-25 1967-11-07 Fmc Corp Fin openers for missile launcher system
FR1563898A (en) * 1968-02-13 1969-04-18
DE2137766A1 (en) * 1971-07-28 1973-02-08 Reinhold Moltrecht BULLET FOR TANK FIST AND SIMILAR GUNS WITH A STABILIZING WING ARRANGEMENT, IN PARTICULAR. FOR EXERCISE PURPOSES
DE7804927U1 (en) * 1978-02-18 1978-06-01 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen DEVICE FOR FOLDING OUT SWING LEAVES

Also Published As

Publication number Publication date
FR2559894A1 (en) 1985-08-23
DE3405974C1 (en) 1985-04-11
GB2154715A (en) 1985-09-11
FR2559894B1 (en) 1987-01-09
GB8501791D0 (en) 1985-02-27

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Legal Events

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