GB2469767A - Control of projectiles or the like - Google Patents

Control of projectiles or the like Download PDF

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Publication number
GB2469767A
GB2469767A GB1012726A GB201012726A GB2469767A GB 2469767 A GB2469767 A GB 2469767A GB 1012726 A GB1012726 A GB 1012726A GB 201012726 A GB201012726 A GB 201012726A GB 2469767 A GB2469767 A GB 2469767A
Authority
GB
United Kingdom
Prior art keywords
canards
projectile
retracted
array
respect
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.)
Withdrawn
Application number
GB1012726A
Other versions
GB201012726D0 (en
Inventor
Roy William Buckland
Stephen George Gladwell Smith
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.)
Qinetiq Ltd
Original Assignee
Qinetiq Ltd
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 Qinetiq Ltd filed Critical Qinetiq Ltd
Publication of GB201012726D0 publication Critical patent/GB201012726D0/en
Publication of GB2469767A publication Critical patent/GB2469767A/en
Withdrawn legal-status Critical Current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
    • 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
    • F42B10/60—Steering arrangements
    • F42B10/62—Steering by movement of flight surfaces
    • F42B10/64—Steering by movement of flight surfaces of fins

Abstract

A gun-fired projectile or ballistic missile (1) is equipped with a pair of canards (3) and an array of tail fins (2). Selected tail fins can be retracted or jettisoned following the ballistic phase to vary the geometry of the array from a rotationally symmetrical configuration to an asymmetric configuration for the glide phase, which together with the canards tends to stabilise the projectile in roll. The canards (3) can be independently extended and retracted with respect to the body of the projectile to generate differential lift for banking the projectile to turn. The canards (3) also preferably have a positive dihedral angle with respect to the intended gliding attitude. In an alternative embodiment the canards are replaced by functionally equivalent thrusters.
GB1012726A 2008-02-22 2009-01-13 Control of projectiles or the like Withdrawn GB2469767A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB0803282.3A GB0803282D0 (en) 2008-02-22 2008-02-22 Control of projectiles or the like
PCT/GB2009/000082 WO2009103939A2 (en) 2008-02-22 2009-01-13 Control of projectiles or the like

Publications (2)

Publication Number Publication Date
GB201012726D0 GB201012726D0 (en) 2010-09-15
GB2469767A true GB2469767A (en) 2010-10-27

Family

ID=39284408

Family Applications (2)

Application Number Title Priority Date Filing Date
GBGB0803282.3A Ceased GB0803282D0 (en) 2008-02-22 2008-02-22 Control of projectiles or the like
GB1012726A Withdrawn GB2469767A (en) 2008-02-22 2009-01-13 Control of projectiles or the like

Family Applications Before (1)

Application Number Title Priority Date Filing Date
GBGB0803282.3A Ceased GB0803282D0 (en) 2008-02-22 2008-02-22 Control of projectiles or the like

Country Status (5)

Country Link
US (1) US8674278B2 (en)
EP (1) EP2245416B1 (en)
AT (1) ATE534011T1 (en)
GB (2) GB0803282D0 (en)
WO (1) WO2009103939A2 (en)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8319164B2 (en) * 2009-10-26 2012-11-27 Nostromo, Llc Rolling projectile with extending and retracting canards
US8624172B2 (en) * 2010-10-13 2014-01-07 Woodward Hrt, Inc. Shift lock assembly
RU2458316C1 (en) * 2011-02-22 2012-08-10 Открытое акционерное общество "Государственное машиностроительное конструкторское бюро "Вымпел" им. И.И. Торопова" Collapsible steer of guided missile
US8939084B2 (en) * 2011-03-15 2015-01-27 Anthony Joseph Cesaroni Surface skimming munition
IL214191A (en) * 2011-07-19 2017-06-29 Elkayam Ami Munition guidance system and method of assembling the same
US9366514B1 (en) 2014-02-25 2016-06-14 Lockheed Martin Corporation System, method and computer program product for providing for a course vector change of a multiple propulsion rocket propelled grenade
WO2015179101A2 (en) * 2014-04-30 2015-11-26 Bae Systems Land & Armaments L.P. Gun launched munition with strakes
US11754379B2 (en) * 2018-03-23 2023-09-12 Simmonds Precision Products, Inc. Space saving wing stowage
CN110307759B (en) * 2019-06-24 2021-10-01 中国航天空气动力技术研究院 Rapid self-overturning missile layout
US11624594B1 (en) 2020-03-31 2023-04-11 Barron Associates, Inc. Device, method and system for extending range and improving tracking precision of mortar rounds
EP4060282B1 (en) * 2021-03-17 2023-10-25 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Missile having a body forming an airfoil at an angle oblique to the longitudinal axis of the missile
JP3235928U (en) * 2021-10-22 2022-01-17 正紘 野崎 Jumping Torpedo JT (Jumping Torpedo)
CN115265289B (en) * 2022-05-16 2023-08-29 东北大学 Bullet with small critical incident angle

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH323227A (en) * 1953-05-22 1957-07-15 Sncan Device for adjusting the maneuverability and stability of a supersonic aerodyne provided with a fixed airfoil
US4076187A (en) * 1975-07-29 1978-02-28 Thomson-Brandt Attitude-controlling system and a missile equipped with such a system
US4917333A (en) * 1988-05-11 1990-04-17 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Actuated forebody strakes
US20070125904A1 (en) * 2005-12-01 2007-06-07 Janka Ronald E Apparatus and method for restraining and deploying an airfoil

Family Cites Families (15)

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Publication number Priority date Publication date Assignee Title
GB778185A (en) 1952-12-04 1957-07-03 Baynes Aircraft Interiors Ltd Improvements in and relating to winged aerial targets
US5439188A (en) 1964-09-04 1995-08-08 Hughes Missile Systems Company Control system
DE1956173C3 (en) 1969-11-07 1975-07-03 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Jet-controlled aircraft with control flaps arranged in the area of the pilot's room
GB1523963A (en) 1976-02-26 1978-09-06 Hawker Siddeley Dynamics Ltd Method and means for auxiliary control of vehicle direction
GB2085820B (en) 1980-09-09 1984-06-06 Secr Defence Aircraft with variable strakes
IT1235222B (en) 1982-11-26 1992-06-26 Secratary Of State For Defence IMPROVEMENT IN MISSILE AND SIMILAR FUSELETS
US4542866A (en) 1983-09-30 1985-09-24 The Boeing Company Aircraft with directional controlling canards
US5271579A (en) 1992-07-10 1993-12-21 Luca Nicholas J De Recreational and sport rocket construction
US5398888A (en) 1993-05-12 1995-03-21 Northrop Grumman Corporation Skewed hinge control surface
US5590850A (en) 1995-06-05 1997-01-07 Hughes Missile Systems Company Blended missile autopilot
US6869044B2 (en) 2003-05-23 2005-03-22 Raytheon Company Missile with odd symmetry tail fins
US6913228B2 (en) 2003-09-04 2005-07-05 Supersonic Aerospace International, Llc Aircraft with active center of gravity control
US7735775B2 (en) 2004-01-30 2010-06-15 Piet Ellnor Wing-in-ground-effect craft
SE528624C2 (en) 2005-11-15 2007-01-09 Bae Systems Bofors Ab Increasing a range of trajectory shells for explosive substances by utilizing folding/fixed rear guide fins with specified radial extent range and folding/fixed front steerable so-called canard fins with aerodynamic bearing surfaces
US7185846B1 (en) * 2006-03-06 2007-03-06 The United States Of America As Represented By The Secretary Of The Army Asymmetrical control surface system for tube-launched air vehicles

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH323227A (en) * 1953-05-22 1957-07-15 Sncan Device for adjusting the maneuverability and stability of a supersonic aerodyne provided with a fixed airfoil
US4076187A (en) * 1975-07-29 1978-02-28 Thomson-Brandt Attitude-controlling system and a missile equipped with such a system
US4917333A (en) * 1988-05-11 1990-04-17 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Actuated forebody strakes
US20070125904A1 (en) * 2005-12-01 2007-06-07 Janka Ronald E Apparatus and method for restraining and deploying an airfoil

Also Published As

Publication number Publication date
GB201012726D0 (en) 2010-09-15
EP2245416B1 (en) 2011-11-16
US20100314489A1 (en) 2010-12-16
ATE534011T1 (en) 2011-12-15
EP2245416A2 (en) 2010-11-03
WO2009103939A3 (en) 2009-12-03
WO2009103939A2 (en) 2009-08-27
GB0803282D0 (en) 2008-04-02
US8674278B2 (en) 2014-03-18

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)