GB2251834B - Guided missiles - Google Patents

Guided missiles

Info

Publication number
GB2251834B
GB2251834B GB8304925A GB8304925A GB2251834B GB 2251834 B GB2251834 B GB 2251834B GB 8304925 A GB8304925 A GB 8304925A GB 8304925 A GB8304925 A GB 8304925A GB 2251834 B GB2251834 B GB 2251834B
Authority
GB
United Kingdom
Prior art keywords
guided missiles
missiles
guided
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 - Lifetime
Application number
GB8304925A
Other versions
GB2251834A (en
Inventor
George Alexander Tarrant
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB8304925A priority Critical patent/GB2251834B/en
Publication of GB2251834A publication Critical patent/GB2251834A/en
Application granted granted Critical
Publication of GB2251834B publication Critical patent/GB2251834B/en
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F42B10/60—Steering arrangements
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F42B10/661—Steering by varying intensity or direction of thrust using several transversally acting rocket motors, each motor containing an individual propellant charge, e.g. solid charge

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)
GB8304925A 1983-02-22 1983-02-22 Guided missiles Expired - Lifetime GB2251834B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8304925A GB2251834B (en) 1983-02-22 1983-02-22 Guided missiles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8304925A GB2251834B (en) 1983-02-22 1983-02-22 Guided missiles

Publications (2)

Publication Number Publication Date
GB2251834A GB2251834A (en) 1992-07-22
GB2251834B true GB2251834B (en) 1992-12-16

Family

ID=10538426

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8304925A Expired - Lifetime GB2251834B (en) 1983-02-22 1983-02-22 Guided missiles

Country Status (1)

Country Link
GB (1) GB2251834B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4210113C1 (en) * 1992-03-27 1998-11-05 Athanassios Dr Ing Zacharias Method of steering flying body for elongated munitions launched from overhead, e.g. from helicopter
FR2730302B1 (en) * 1995-02-03 1997-03-14 Tda Armements Sas CONTROL OF A PROJECTILE BY MULTI-CHAMBER AND SINGLE-TUBE IMPELLER
US8800913B2 (en) 2009-07-30 2014-08-12 Raytheon Company Methods and apparatus for a tandem divert and attitude control system
FR2975481B1 (en) * 2011-05-19 2017-09-01 Snecma Propulsion Solide SYSTEM FOR FORCE DRIVING AND ATTITUDE CONTROL IN FLIGHT OF A VEHICLE AND A VEHICLE COMPRISING SUCH A SYSTEM

Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB764395A (en) * 1950-08-30 1956-12-28 Vickers Armstrongs Aircraft Improvements relating to the automatic control of flying bodies
GB930961A (en) * 1961-04-11 1963-07-10 Mcdonnell Aircraft Corp Guidance system
GB952928A (en) * 1960-05-05 1964-03-18 Brevets Aero Mecaniques Improvements in projectiles to be slidably fitted on the end of a gun barrel
GB975020A (en) * 1959-11-25 1964-11-11 Romald Edward Bowles Improvements in or relating to fluid-operated control devices
GB1075705A (en) * 1964-09-22 1967-07-12 Aerojet General Co Attitude control system for sounding rockets
GB1193304A (en) * 1966-07-04 1970-05-28 Nationale D Armes De Geurre Fa Projectiles having Means for Correcting the Trajectory
GB1359864A (en) * 1970-11-10 1974-07-10 Messerschmitt Boelkow Blohm Missile
GB2010760A (en) * 1977-12-23 1979-07-04 Rheinmetall Gmbh Changing the trajectory of a missile
WO1980000825A1 (en) * 1978-10-19 1980-05-01 Airships Int Inc Thrusters for airship control
GB1578291A (en) * 1976-04-02 1980-11-05 Bofors Ab Terminally corrected projectile
GB2056392A (en) * 1979-08-22 1981-03-18 Rca Corp Attitude control system for spacecraft utilizing the thruster plume
GB2068311A (en) * 1980-01-30 1981-08-12 Dornier Gmbh A jet reaction propelled flying body
GB2094240A (en) * 1981-03-10 1982-09-15 Secr Defence Attitude control systems for rocket powered vehicles

Patent Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB764395A (en) * 1950-08-30 1956-12-28 Vickers Armstrongs Aircraft Improvements relating to the automatic control of flying bodies
GB975020A (en) * 1959-11-25 1964-11-11 Romald Edward Bowles Improvements in or relating to fluid-operated control devices
GB952928A (en) * 1960-05-05 1964-03-18 Brevets Aero Mecaniques Improvements in projectiles to be slidably fitted on the end of a gun barrel
GB930961A (en) * 1961-04-11 1963-07-10 Mcdonnell Aircraft Corp Guidance system
GB1075705A (en) * 1964-09-22 1967-07-12 Aerojet General Co Attitude control system for sounding rockets
GB1193304A (en) * 1966-07-04 1970-05-28 Nationale D Armes De Geurre Fa Projectiles having Means for Correcting the Trajectory
GB1359864A (en) * 1970-11-10 1974-07-10 Messerschmitt Boelkow Blohm Missile
GB1578291A (en) * 1976-04-02 1980-11-05 Bofors Ab Terminally corrected projectile
GB2010760A (en) * 1977-12-23 1979-07-04 Rheinmetall Gmbh Changing the trajectory of a missile
WO1980000825A1 (en) * 1978-10-19 1980-05-01 Airships Int Inc Thrusters for airship control
GB2056392A (en) * 1979-08-22 1981-03-18 Rca Corp Attitude control system for spacecraft utilizing the thruster plume
GB2068311A (en) * 1980-01-30 1981-08-12 Dornier Gmbh A jet reaction propelled flying body
GB2094240A (en) * 1981-03-10 1982-09-15 Secr Defence Attitude control systems for rocket powered vehicles

Also Published As

Publication number Publication date
GB2251834A (en) 1992-07-22

Similar Documents

Publication Publication Date Title
GB8417125D0 (en) Cannon-launched projectile
DE3468527D1 (en) Missile
GB2149481B (en) Projectile
EP0180722A3 (en) Missile
IL76404A0 (en) Missile
GB8404647D0 (en) Fin-stabilised projectile
GB2120166B (en) Structural member
EP0149713A3 (en) Practice projectile
GB2150091B (en) Guided munition
GB8304412D0 (en) Projectile
AR242637A1 (en) Staking-machine
DE3272598D1 (en) Missile
GB8316784D0 (en) Launcher
GB2251834B (en) Guided missiles
GB2131925B (en) Projectile
GB8310390D0 (en) Dartboard
EP0106093A3 (en) Iodopropargylsulfamide
GB8317113D0 (en) Projectile
GB8424764D0 (en) Projectiles
GB8331557D0 (en) Birdfood member
GB8315138D0 (en) Facing member
GB8325150D0 (en) Submarine
GB8408580D0 (en) Projectiles
GB8420115D0 (en) Guided missiles
GB8420773D0 (en) Dartboard

Legal Events

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

Effective date: 19950222