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FR2554577B1 - Systeme de commande pour munition guidee se propageant dans l'air a une vitesse supersonique - Google Patents

Systeme de commande pour munition guidee se propageant dans l'air a une vitesse supersonique

Info

Publication number
FR2554577B1
FR2554577B1 FR8416789A FR8416789A FR2554577B1 FR 2554577 B1 FR2554577 B1 FR 2554577B1 FR 8416789 A FR8416789 A FR 8416789A FR 8416789 A FR8416789 A FR 8416789A FR 2554577 B1 FR2554577 B1 FR 2554577B1
Authority
FR
France
Prior art keywords
superson
spreading
speed
air
control system
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.)
Expired
Application number
FR8416789A
Other languages
English (en)
Other versions
FR2554577A1 (fr
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.)
Diehl Verwaltungs Stiftung
Original Assignee
Diehl GmbH and 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 and Co filed Critical Diehl GmbH and Co
Publication of FR2554577A1 publication Critical patent/FR2554577A1/fr
Application granted granted Critical
Publication of FR2554577B1 publication Critical patent/FR2554577B1/fr
Expired legal-status Critical Current

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)
FR8416789A 1983-11-05 1984-11-05 Systeme de commande pour munition guidee se propageant dans l'air a une vitesse supersonique Expired FR2554577B1 (fr)

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 (2)

Publication Number Publication Date
FR2554577A1 FR2554577A1 (fr) 1985-05-10
FR2554577B1 true FR2554577B1 (fr) 1987-11-27

Family

ID=6213541

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8416789A Expired FR2554577B1 (fr) 1983-11-05 1984-11-05 Systeme de commande pour munition guidee se propageant dans l'air a une vitesse supersonique

Country Status (6)

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

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 (fr) * 1954-05-18 Ph. G. A. R. Von Zborowski Helmut Projectiles volants
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
DE3340037A1 (de) 1985-05-23
GB2150091A (en) 1985-06-26
GB2150091B (en) 1987-05-13
IT8423422A1 (it) 1986-05-01
IT8423662V0 (it) 1984-10-31
US4623107A (en) 1986-11-18
IT8423422A0 (it) 1984-10-31
IT1178608B (it) 1987-09-09
FR2554577A1 (fr) 1985-05-10
GB8427099D0 (en) 1984-12-05
IL73366A (en) 1990-11-05
DE3340037C2 (fr) 1989-07-13

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Legal Events

Date Code Title Description
ST Notification of lapse