PL2876405T3 - Guided missile and method for steering a guided missile - Google Patents

Guided missile and method for steering a guided missile

Info

Publication number
PL2876405T3
PL2876405T3 PL14003885T PL14003885T PL2876405T3 PL 2876405 T3 PL2876405 T3 PL 2876405T3 PL 14003885 T PL14003885 T PL 14003885T PL 14003885 T PL14003885 T PL 14003885T PL 2876405 T3 PL2876405 T3 PL 2876405T3
Authority
PL
Poland
Prior art keywords
guided missile
steering
missile
guided
Prior art date
Application number
PL14003885T
Other languages
Polish (pl)
Inventor
Ludwig Netter
Harald Wasner
Thomas Gallhauser
Original Assignee
Mbda Deutschland 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 Mbda Deutschland Gmbh filed Critical Mbda Deutschland Gmbh
Publication of PL2876405T3 publication Critical patent/PL2876405T3/en

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
    • 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)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
PL14003885T 2013-11-20 2014-11-19 Guided missile and method for steering a guided missile PL2876405T3 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE102013019342 2013-11-20
DE102014004251.0A DE102014004251A1 (en) 2013-11-20 2014-03-24 Guided missile and method for steering a missile
EP14003885.2A EP2876405B1 (en) 2013-11-20 2014-11-19 Guided missile and method for steering a guided missile

Publications (1)

Publication Number Publication Date
PL2876405T3 true PL2876405T3 (en) 2018-07-31

Family

ID=52020884

Family Applications (1)

Application Number Title Priority Date Filing Date
PL14003885T PL2876405T3 (en) 2013-11-20 2014-11-19 Guided missile and method for steering a guided missile

Country Status (4)

Country Link
EP (1) EP2876405B1 (en)
DE (1) DE102014004251A1 (en)
ES (1) ES2665370T3 (en)
PL (1) PL2876405T3 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102016101560A1 (en) * 2016-01-28 2017-08-03 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Transverse thrust device for active web and attitude control of missiles

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2822755A (en) * 1950-12-01 1958-02-11 Mcdonnell Aircraft Corp Flight control mechanism for rockets
US3749334A (en) * 1966-04-04 1973-07-31 Us Army Attitude compensating missile system
DE2809281C2 (en) * 1978-03-03 1984-01-05 Emile Jean Versailles Stauff Control device for a self-rotating projectile
GB8803164D0 (en) * 1988-02-11 1988-08-24 British Aerospace Reaction control system
FR2684723B1 (en) * 1991-12-10 1995-05-19 Thomson Csf SOLID PROPERGOL PROPELLER WITH MODULAR PUSH AND MISSILE EQUIPPED.
US5631830A (en) * 1995-02-03 1997-05-20 Loral Vought Systems Corporation Dual-control scheme for improved missle maneuverability
US5590850A (en) * 1995-06-05 1997-01-07 Hughes Missile Systems Company Blended missile autopilot
DE19645562A1 (en) * 1996-04-02 1997-10-09 Bodenseewerk Geraetetech Regulator for nonlinear closed-loop controlled system
US6308911B1 (en) * 1998-10-30 2001-10-30 Lockheed Martin Corp. Method and apparatus for rapidly turning a vehicle in a fluid medium

Also Published As

Publication number Publication date
EP2876405B1 (en) 2018-01-10
DE102014004251A1 (en) 2015-06-25
EP2876405A1 (en) 2015-05-27
ES2665370T3 (en) 2018-04-25

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PL2876405T3 (en) Guided missile and method for steering a guided missile