ES2665370T3 - Misil guiado y procedimiento para dirigir un misil guiado - Google Patents

Misil guiado y procedimiento para dirigir un misil guiado Download PDF

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Publication number
ES2665370T3
ES2665370T3 ES14003885.2T ES14003885T ES2665370T3 ES 2665370 T3 ES2665370 T3 ES 2665370T3 ES 14003885 T ES14003885 T ES 14003885T ES 2665370 T3 ES2665370 T3 ES 2665370T3
Authority
ES
Spain
Prior art keywords
drive
guided missile
thrust
longitudinal axis
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.)
Active
Application number
ES14003885.2T
Other languages
English (en)
Spanish (es)
Inventor
Ludwig Netter
Harald Wasner
Thomas Gallhauser
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.)
MBDA Deutschland GmbH
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
Application granted granted Critical
Publication of ES2665370T3 publication Critical patent/ES2665370T3/es
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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)
ES14003885.2T 2013-11-20 2014-11-19 Misil guiado y procedimiento para dirigir un misil guiado Active ES2665370T3 (es)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
DE102013019342 2013-11-20
DE102013019342 2013-11-20
DE102014004251.0A DE102014004251A1 (de) 2013-11-20 2014-03-24 Lenkflugkörper und Verfahren zum Lenken eines Lenkflugkörpers
DE102014004251 2014-03-24

Publications (1)

Publication Number Publication Date
ES2665370T3 true ES2665370T3 (es) 2018-04-25

Family

ID=52020884

Family Applications (1)

Application Number Title Priority Date Filing Date
ES14003885.2T Active ES2665370T3 (es) 2013-11-20 2014-11-19 Misil guiado y procedimiento para dirigir un misil guiado

Country Status (4)

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

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102016101560A1 (de) * 2016-01-28 2017-08-03 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Querschubeinrichtung zur aktiven Bahn- und Lagesteuerung von Flugkörpern

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 (de) * 1978-03-03 1984-01-05 Emile Jean Versailles Stauff Steuervorrichtung für ein Geschoß mit Eigendrehung
GB8803164D0 (en) * 1988-02-11 1988-08-24 British Aerospace Reaction control system
FR2684723B1 (fr) * 1991-12-10 1995-05-19 Thomson Csf Propulseur a propergol solide a poussee modulable et missile equipe.
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
DE19645556A1 (de) * 1996-04-02 1997-10-30 Bodenseewerk Geraetetech Vorrichtung zur Erzeugung von Lenksignalen für zielverfolgende Flugkörper
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
DE102014004251A1 (de) 2015-06-25
EP2876405A1 (de) 2015-05-27
PL2876405T3 (pl) 2018-07-31
EP2876405B1 (de) 2018-01-10

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