IT1290876B1 - Procedimento per la guida di un missile e relativo missile impiegato - Google Patents

Procedimento per la guida di un missile e relativo missile impiegato

Info

Publication number
IT1290876B1
IT1290876B1 IT93RM000190A ITRM930190A IT1290876B1 IT 1290876 B1 IT1290876 B1 IT 1290876B1 IT 93RM000190 A IT93RM000190 A IT 93RM000190A IT RM930190 A ITRM930190 A IT RM930190A IT 1290876 B1 IT1290876 B1 IT 1290876B1
Authority
IT
Italy
Prior art keywords
missile
guiding
procedure
missile used
Prior art date
Application number
IT93RM000190A
Other languages
English (en)
Italian (it)
Inventor
Athanassions Zacharias
Original Assignee
Buck Chem Tech Werke
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 Buck Chem Tech Werke filed Critical Buck Chem Tech Werke
Publication of ITRM930190A0 publication Critical patent/ITRM930190A0/it
Publication of ITRM930190A1 publication Critical patent/ITRM930190A1/it
Application granted granted Critical
Publication of IT1290876B1 publication Critical patent/IT1290876B1/it

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)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
IT93RM000190A 1992-03-27 1993-03-26 Procedimento per la guida di un missile e relativo missile impiegato IT1290876B1 (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE4210113A DE4210113C1 (de) 1992-03-27 1992-03-27 Verfahren zum Leiten eines Flugkörpers und Flugkörper

Publications (3)

Publication Number Publication Date
ITRM930190A0 ITRM930190A0 (en, 2012) 1993-03-26
ITRM930190A1 ITRM930190A1 (it) 1994-09-26
IT1290876B1 true IT1290876B1 (it) 1998-12-14

Family

ID=6455243

Family Applications (1)

Application Number Title Priority Date Filing Date
IT93RM000190A IT1290876B1 (it) 1992-03-27 1993-03-26 Procedimento per la guida di un missile e relativo missile impiegato

Country Status (6)

Country Link
US (1) US5880396A (en, 2012)
CA (1) CA2092441A1 (en, 2012)
DE (1) DE4210113C1 (en, 2012)
FR (1) FR2769083A1 (en, 2012)
GB (1) GB2328497B (en, 2012)
IT (1) IT1290876B1 (en, 2012)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19806066B4 (de) * 1998-02-13 2004-07-08 Lfk-Lenkflugkörpersysteme Gmbh Flugkörper gegen Reaktivpanzerung
RU2177599C1 (ru) * 2000-08-30 2001-12-27 Открытое акционерное общество АК "Туламашзавод" Управляемый артиллерийский снаряд. способ сборки боевой части артиллерийского снаряда
GB0120611D0 (en) * 2001-08-24 2001-10-17 Igt Uk Ltd Video display systems
US7252270B2 (en) * 2003-08-05 2007-08-07 Israel Aircraft Industries, Ltd. System and method for launching a missile from a flying aircraft
IL162027A (en) * 2004-05-17 2009-05-04 Rafael Advanced Defense Sys Method and system for resetting the flight path of a non-guided bullet, including compensation for deviation from the oscillations of the launcher
US7947938B2 (en) * 2007-03-15 2011-05-24 Raytheon Company Methods and apparatus for projectile guidance
US8546736B2 (en) 2007-03-15 2013-10-01 Raytheon Company Modular guided projectile

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2974594A (en) * 1958-08-14 1961-03-14 Boehm Josef Space vehicle attitude control system
US3196794A (en) * 1959-06-18 1965-07-27 Robert C Meade Piezo-electric fuse device
US3072055A (en) * 1959-08-03 1963-01-08 Ross Sidney Gun launched, terminal guided projectile
US3276376A (en) * 1964-09-30 1966-10-04 Robert W Cubbison Thrust and direction control apparatus
NL135093C (en, 2012) * 1966-03-22
BE683586A (en, 2012) * 1966-07-04 1966-12-16
US3612442A (en) * 1969-04-03 1971-10-12 Nasa Fluidic proportional thruster system
DE2055088A1 (de) * 1970-11-10 1972-05-18 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Einrichtung zum Erzeugen von Steuermomenten bei raketengetriebenen Flugkörpern
FR2386802A1 (fr) * 1977-04-08 1978-11-03 Thomson Brandt Dispositif de pilotage pour projectile du genre missile, et projectile equipe de ce dispositif
FR2401400A1 (fr) * 1977-08-23 1979-03-23 Serat Arme antichar sol-sol
GB2094240B (en) * 1981-03-10 1984-08-01 Secr Defence Attitude control systems for rocket powered vehicles
FR2517818A1 (fr) * 1981-12-09 1983-06-10 Thomson Brandt Methode de guidage terminal et missile guide operant selon cette methode
FR2534370B1 (fr) * 1982-10-11 1986-12-19 Luchaire Sa Engin destine a l'attaque en survol d'objectifs tels que notamment des blindes
GB2251834B (en) * 1983-02-22 1992-12-16 George Alexander Tarrant Guided missiles
DE3427227A1 (de) * 1984-07-24 1986-01-30 Diehl GmbH & Co, 8500 Nürnberg Endphasen-steuerbarer munitionsartikel und verfahren zu seiner zielnavigation
DE3516673A1 (de) * 1985-05-09 1986-11-13 Diehl GmbH & Co, 8500 Nürnberg Endphasen-korrigierbare suchzuender-munition und verfahren zum bekaempfen gepanzerter zielobjekte
EP0438343B1 (fr) * 1990-01-16 1998-07-22 Tda Armements S.A.S. Munition perforante pour des cibles à haute résistance mécanique
DE4012153A1 (de) * 1990-04-14 1991-10-17 Rheinmetall Gmbh Steuervorrichtung fuer einen flugkoerper

Also Published As

Publication number Publication date
FR2769083A1 (fr) 1999-04-02
US5880396A (en) 1999-03-09
GB2328497B (en) 1999-06-02
GB2328497A (en) 1999-02-24
CA2092441A1 (en) 1999-11-03
GB9305667D0 (en) 1998-10-14
ITRM930190A1 (it) 1994-09-26
ITRM930190A0 (en, 2012) 1993-03-26
DE4210113C1 (de) 1998-11-05

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Legal Events

Date Code Title Description
0001 Granted