IT8423662V0 - Sistema di impostazione per aeromobili guidati, volanti a velocita' supersonica. - Google Patents

Sistema di impostazione per aeromobili guidati, volanti a velocita' supersonica.

Info

Publication number
IT8423662V0
IT8423662V0 IT8423662U IT2366284U IT8423662V0 IT 8423662 V0 IT8423662 V0 IT 8423662V0 IT 8423662 U IT8423662 U IT 8423662U IT 2366284 U IT2366284 U IT 2366284U IT 8423662 V0 IT8423662 V0 IT 8423662V0
Authority
IT
Italy
Prior art keywords
aircrafts
guided
steering wheels
setting system
supersonic speed
Prior art date
Application number
IT8423662U
Other languages
English (en)
Inventor
Helmut Misoph
Original Assignee
Diehl Gmbh & Co
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 Diehl Gmbh & Co filed Critical Diehl Gmbh & Co
Publication of IT8423662V0 publication Critical patent/IT8423662V0/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
    • F42B10/62—Steering by movement of flight surfaces
    • F42B10/64—Steering by movement of flight surfaces of fins
    • 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

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)
IT8423662U 1983-11-05 1984-10-31 Sistema di impostazione per aeromobili guidati, volanti a velocita' supersonica. IT8423662V0 (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19833340037 DE3340037A1 (de) 1983-11-05 1983-11-05 Stellsystem fuer gelenkte, mit ueberschallgeschwindigkeit fliegende flugkoerper

Publications (1)

Publication Number Publication Date
IT8423662V0 true IT8423662V0 (it) 1984-10-31

Family

ID=6213541

Family Applications (2)

Application Number Title Priority Date Filing Date
IT23422/84A IT1178608B (it) 1983-11-05 1984-10-31 Sistema di impostazione per aeromobili guidati, volanti a velocita' supersonica
IT8423662U IT8423662V0 (it) 1983-11-05 1984-10-31 Sistema di impostazione per aeromobili guidati, volanti a velocita' supersonica.

Family Applications Before (1)

Application Number Title Priority Date Filing Date
IT23422/84A IT1178608B (it) 1983-11-05 1984-10-31 Sistema di impostazione per aeromobili guidati, volanti a velocita' supersonica

Country Status (6)

Country Link
US (1) US4623107A (it)
DE (1) DE3340037A1 (it)
FR (1) FR2554577B1 (it)
GB (1) GB2150091B (it)
IL (1) IL73366A (it)
IT (2) IT1178608B (it)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4951901A (en) * 1985-11-22 1990-08-28 Ship Systems, Inc. Spin-stabilized projectile with pulse receiver and method of use
DE3546269C1 (de) * 1985-12-28 1987-08-13 Deutsche Forsch Luft Raumfahrt Flugkoerper
SE461750B (sv) * 1987-03-20 1990-03-19 Lars Johan Schleimann Jensen Foerfarande foer styrning av ett flygande objekt, saasom en projektil, mot ett maal och projektil foer foerfarandets genomfoerande
FR2686409B1 (fr) * 1988-06-22 1994-05-13 Saint Louis Inst Franco Alle Rec Projectile supersonique pilotable.
US5076511A (en) * 1990-12-19 1991-12-31 Honeywell Inc. Discrete impulse spinning-body hard-kill (disk)
FR2762080B1 (fr) * 1997-04-15 1999-07-02 Tda Armements Sas Dispositif de microgouverne pour la correction de trajectoire de munition stabilisee par rotation
US7262394B2 (en) * 2004-03-05 2007-08-28 The Boeing Company Mortar shell ring tail and associated method
US7373883B1 (en) * 2005-01-10 2008-05-20 The United States Of America As Represented By The Secretary Of The Navy Projectile with tail-mounted gas generator assembly
US8502126B2 (en) * 2010-05-27 2013-08-06 Raytheon Company System and method for navigating an object
CN103115532B (zh) * 2013-03-05 2014-11-05 西北工业大学 一种超音速导弹减阻翼

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA502517A (en) * 1954-05-18 Ph. G. A. R. Von Zborowski Helmut Flying missiles
FR556302A (fr) * 1921-12-23 1923-07-17 Perfectionnements aux projectiles à empennage
US2495304A (en) * 1946-05-31 1950-01-24 Gulf Research Development Co Dirigible bomb
US2584826A (en) * 1946-05-31 1952-02-05 Gulf Research Development Co Aerodynamic surface for dirigible bombs
FR1039689A (fr) * 1951-04-25 1953-10-08 Perfectionnements apportés aux systèmes de gouvernes pour engins se déplaçant dans un fluide, notamment à ceux pour aérodynes
US2835199A (en) * 1955-01-05 1958-05-20 Hughes Aircraft Co Stabilized self-propelled missile
US3162162A (en) * 1959-07-16 1964-12-22 Clevite Corp Torpedo steering system
US3096739A (en) * 1960-06-20 1963-07-09 Kenneth E Smith Method and apparatus for steering underwater bodies
US3156207A (en) * 1961-01-09 1964-11-10 Gen Electric Control device for boundary layer control vehicle
US3603533A (en) * 1969-09-29 1971-09-07 Us Army Spin stabilized ring-wing canard controlled missile
US3724782A (en) * 1971-07-22 1973-04-03 Us Navy Deployable aerodynamic ring stabilizer
DE2856286C2 (de) * 1978-12-27 1986-06-12 Rheinmetall GmbH, 4000 Düsseldorf Mit Überschallgeschwindigkeit fliegendes Geschoß
FR2504252B1 (fr) * 1981-04-21 1987-03-06 Thomson Brandt Projectile guide
FR2508414B1 (fr) * 1981-06-30 1985-06-07 Thomson Brandt Dispositif de pilotage par jets de gaz pour engin guide

Also Published As

Publication number Publication date
GB2150091B (en) 1987-05-13
DE3340037A1 (de) 1985-05-23
IL73366A (en) 1990-11-05
DE3340037C2 (it) 1989-07-13
GB8427099D0 (en) 1984-12-05
IT1178608B (it) 1987-09-09
FR2554577A1 (fr) 1985-05-10
IT8423422A0 (it) 1984-10-31
FR2554577B1 (fr) 1987-11-27
US4623107A (en) 1986-11-18
IT8423422A1 (it) 1986-05-01
GB2150091A (en) 1985-06-26

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