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GB2010760B - Changing the trajectory of a missile - Google Patents

Changing the trajectory of a missile

Info

Publication number
GB2010760B
GB2010760B GB7850054A GB7850054A GB2010760B GB 2010760 B GB2010760 B GB 2010760B GB 7850054 A GB7850054 A GB 7850054A GB 7850054 A GB7850054 A GB 7850054A GB 2010760 B GB2010760 B GB 2010760B
Authority
GB
United Kingdom
Prior art keywords
missile
trajectory
changing
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
GB7850054A
Other versions
GB2010760A (en
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.)
Rheinmetall Industrie AG
Original Assignee
Rheinmetall GmbH
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 Rheinmetall GmbH filed Critical Rheinmetall GmbH
Publication of GB2010760A publication Critical patent/GB2010760A/en
Application granted granted Critical
Publication of GB2010760B publication Critical patent/GB2010760B/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
    • F42B10/60—Steering arrangements
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F42B10/663—Steering by varying intensity or direction of thrust using a plurality of transversally acting auxiliary nozzles, which are opened or closed by valves

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Toys (AREA)
GB7850054A 1977-12-23 1978-12-27 Changing the trajectory of a missile Expired GB2010760B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19772757664 DE2757664A1 (en) 1977-12-23 1977-12-23 DEVICE FOR CHANGING THE AIRWAY OF ONE FLOOR

Publications (2)

Publication Number Publication Date
GB2010760A GB2010760A (en) 1979-07-04
GB2010760B true GB2010760B (en) 1982-06-16

Family

ID=6027105

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7850054A Expired GB2010760B (en) 1977-12-23 1978-12-27 Changing the trajectory of a missile

Country Status (5)

Country Link
DE (1) DE2757664A1 (en)
FR (1) FR2412812A1 (en)
GB (1) GB2010760B (en)
IT (1) IT1099287B (en)
SE (1) SE7812955L (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2172383B (en) * 1981-06-04 1987-08-12 Aerospatiale Guided missile system
DE3231528C1 (en) * 1982-08-25 1983-10-27 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Control system for wingless steering ammunition
GB2251834B (en) * 1983-02-22 1992-12-16 George Alexander Tarrant Guided missiles
DE3427227A1 (en) * 1984-07-24 1986-01-30 Diehl GmbH & Co, 8500 Nürnberg END-PHASE-CONTROLLABLE AMMUNITION ITEM AND METHOD FOR ITS TARGET NAVIGATION
DE3603497C1 (en) * 1986-02-05 1993-01-07 Rheinmetall Gmbh Bullet for an anti-tank weapon to fight a tank from above
RU2258896C1 (en) * 2004-05-05 2005-08-20 Государственное унитарное предприятие "Конструкторское бюро приборостроения" Guided missile in launching pack
CN111350615B (en) * 2020-03-27 2023-09-05 惠州学院 An integral turning device suitable for vertical launching aircraft

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE428854A (en) * 1937-06-28
DE1158846B (en) * 1961-07-20 1963-12-05 Dornier System Gmbh Aircraft, especially unmanned missiles
SE429064B (en) * 1976-04-02 1983-08-08 Bofors Ab FINAL PHASE CORRECTION OF ROTATING PROJECTILE

Also Published As

Publication number Publication date
FR2412812A1 (en) 1979-07-20
IT1099287B (en) 1985-09-18
SE7812955L (en) 1979-06-24
GB2010760A (en) 1979-07-04
DE2757664A1 (en) 1979-06-28
FR2412812B1 (en) 1982-11-12
IT7828694A0 (en) 1978-10-12

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Legal Events

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