SE410520B - Missiler med korsformig roderanordning - Google Patents

Missiler med korsformig roderanordning

Info

Publication number
SE410520B
SE410520B SE7400903A SE7400903A SE410520B SE 410520 B SE410520 B SE 410520B SE 7400903 A SE7400903 A SE 7400903A SE 7400903 A SE7400903 A SE 7400903A SE 410520 B SE410520 B SE 410520B
Authority
SE
Sweden
Prior art keywords
fins
clamp
missile
west
east
Prior art date
Application number
SE7400903A
Other languages
English (en)
Swedish (sv)
Inventor
J H Fieuzal
L G Bourgine
A C Jean
R P Benzoni
Original Assignee
France Etat Armement
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 France Etat Armement filed Critical France Etat Armement
Publication of SE410520B publication Critical patent/SE410520B/sv

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
    • F42B10/62—Steering by movement of flight surfaces
    • F42B10/64—Steering by movement of flight surfaces of fins

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)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
SE7400903A 1973-04-17 1974-01-24 Missiler med korsformig roderanordning SE410520B (sv)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7313815A FR2226641B1 (it) 1973-04-17 1973-04-17

Publications (1)

Publication Number Publication Date
SE410520B true SE410520B (sv) 1979-10-15

Family

ID=9118050

Family Applications (1)

Application Number Title Priority Date Filing Date
SE7400903A SE410520B (sv) 1973-04-17 1974-01-24 Missiler med korsformig roderanordning

Country Status (6)

Country Link
US (1) US3976266A (it)
DE (1) DE2410255C2 (it)
FR (1) FR2226641B1 (it)
GB (1) GB1431744A (it)
IT (1) IT1007243B (it)
SE (1) SE410520B (it)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2150092B (en) * 1983-11-25 1987-07-22 British Aerospace Deployment and actuation mechanisms
DE3441534A1 (de) * 1984-11-14 1986-05-15 Diehl GmbH & Co, 8500 Nürnberg Lageranordnung fuer das ruderblatt eines flugkoerpers
DE3717688C1 (en) * 1987-05-26 1988-06-09 Messerschmitt Boelkow Blohm Rotating device for aerodynamically acting control surfaces which are mounted such that they can rotate
GB8721291D0 (en) * 1987-09-10 1990-05-16 British Aerospace Projectile guidance
DE3915585A1 (de) * 1989-05-12 1990-11-15 Diehl Gmbh & Co Submunitions-flugkoerper
FR2657703B1 (fr) * 1990-01-26 1992-04-10 Thomson Brandt Armements Dispositif pour la commande d'attitude en roulis d'un projectile stabilise par empennage.
IL107844A (en) * 1993-12-02 1996-06-18 Ministry Of Defence Armaments Flying object control system
DE19827278A1 (de) * 1998-06-19 1999-12-23 Diehl Stiftung & Co Lenkbarer Flugkörper
DE19827277B4 (de) 1998-06-19 2006-08-10 Diehl Stiftung & Co.Kg Lageranordnung für die aufschwenkbaren Ruderblätter eines lenkbaren Flugkörpers
GB2374055B (en) * 2000-10-07 2004-08-04 Bayern Chemie Gmbh Flugchemie A rudder blade guidance arrangement for missiles
RU2191984C2 (ru) * 2000-10-23 2002-10-27 Государственное унитарное предприятие "Конструкторское бюро приборостроения" Способ взведения бортовых систем управляемого снаряда
RU2205358C2 (ru) * 2000-11-30 2003-05-27 Государственное унитарное предприятие "Конструкторское бюро приборостроения" Система наведения управляемого снаряда
RU2205359C2 (ru) * 2000-12-25 2003-05-27 Государственное унитарное предприятие "Конструкторское бюро приборостроения" Система наведения управляемого снаряда
ITMI20010648A1 (it) 2001-03-27 2002-09-27 Finmeccanica S P A Alenia Dife Gruppo di controllo per alette direzionali di missili e/o proiettili
US6721682B1 (en) 2002-01-07 2004-04-13 The United States Of America As Represented By The Secretary Of The Navy Aerodynamic prediction using semiempirical prediction techniques and methods therefor
US7526988B2 (en) * 2006-05-11 2009-05-05 The Boeing Company Electromagnetic railgun projectile
US8278612B2 (en) 2010-07-27 2012-10-02 Raytheon Company Aerodynamic fin lock for adjustable and deployable fin
SE535991C2 (sv) * 2011-07-07 2013-03-19 Bae Systems Bofors Ab Rotationsstabiliserad styrbar projektil och förfarande därför
FR3041744B1 (fr) * 2015-09-29 2018-08-17 Nexter Munitions Projectile d'artillerie ayant une phase pilotee.
WO2020243573A1 (en) * 2019-05-30 2020-12-03 Pliant Energy Systems Llc Aerial swimmer apparatuses, methods and systems

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3128061A (en) * 1945-08-11 1964-04-07 Thornton W Chew Automatic self-guidance system for movable objects
FR1219350A (fr) * 1958-12-24 1960-05-17 Projectile autopropulsé à empennage fixe
US3104081A (en) * 1959-11-27 1963-09-17 Bendix Corp Solenoid operated three-position pneumatic actuator
US3154015A (en) * 1962-09-19 1964-10-27 Martin Marietta Corp Missile flight control system
US3373955A (en) * 1964-05-25 1968-03-19 Huska Paul Pitch and yaw actuator assembly for vehicle guidance surfaces

Also Published As

Publication number Publication date
DE2410255A1 (de) 1974-10-24
FR2226641B1 (it) 1976-11-12
GB1431744A (en) 1976-04-14
IT1007243B (it) 1976-10-30
US3976266A (en) 1976-08-24
FR2226641A1 (it) 1974-11-15
DE2410255C2 (de) 1984-05-10

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