GB2172383B - Guided missile system - Google Patents

Guided missile system

Info

Publication number
GB2172383B
GB2172383B GB08215138A GB8215138A GB2172383B GB 2172383 B GB2172383 B GB 2172383B GB 08215138 A GB08215138 A GB 08215138A GB 8215138 A GB8215138 A GB 8215138A GB 2172383 B GB2172383 B GB 2172383B
Authority
GB
United Kingdom
Prior art keywords
guided missile
missile system
guided
missile
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
GB08215138A
Other versions
GB2172383A (en
Inventor
Jacques Raynaud
Michel Maree
Robert Vaillant
Jean Ansaldi
Jean Guillot
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
Priority claimed from FR8111088A external-priority patent/FR2578665B1/en
Application filed by Airbus Group SAS filed Critical Airbus Group SAS
Priority claimed from EP19860401004 external-priority patent/EP0245565B1/en
Publication of GB2172383A publication Critical patent/GB2172383A/en
Application granted granted Critical
Publication of GB2172383B publication Critical patent/GB2172383B/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • 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
    • F42B10/665—Steering by varying intensity or direction of thrust characterised by using a nozzle provided with at least a deflector mounted within the nozzle
    • 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
    • F42B10/666—Steering by varying intensity or direction of thrust characterised by using a nozzle rotatable about an axis transverse to the axis of the projectile

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
GB08215138A 1981-06-04 1982-05-27 Guided missile system Expired GB2172383B (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR8111088A FR2578665B1 (en) 1981-06-04 1981-06-04 LOW SPEED MISSILE PILOTING METHOD, WEAPON AND MISSILE SYSTEM FOR IMPLEMENTING THE METHOD
EP19860401004 EP0245565B1 (en) 1986-05-12 1986-05-12 Steering method for a low-velocity missile, weapon system and missile therefor

Publications (2)

Publication Number Publication Date
GB2172383A GB2172383A (en) 1986-09-17
GB2172383B true GB2172383B (en) 1987-08-12

Family

ID=26105687

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08215138A Expired GB2172383B (en) 1981-06-04 1982-05-27 Guided missile system

Country Status (1)

Country Link
GB (1) GB2172383B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3821309A1 (en) * 1988-06-24 1990-02-15 Messerschmitt Boelkow Blohm Anti-tank missile
GB201312593D0 (en) * 2013-07-13 2013-08-28 Mbda Uk Ltd A thrust flow powered vehicle

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE340417B (en) * 1969-06-06 1971-11-15 Bofors Ab
DE2757664A1 (en) * 1977-12-23 1979-06-28 Rheinmetall Gmbh DEVICE FOR CHANGING THE AIRWAY OF ONE FLOOR

Also Published As

Publication number Publication date
GB2172383A (en) 1986-09-17

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Legal Events

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

Effective date: 20010527