EP0384965A3 - Flügelstabilisierter Submunitionskörper - Google Patents

Flügelstabilisierter Submunitionskörper Download PDF

Info

Publication number
EP0384965A3
EP0384965A3 EP19890120959 EP89120959A EP0384965A3 EP 0384965 A3 EP0384965 A3 EP 0384965A3 EP 19890120959 EP19890120959 EP 19890120959 EP 89120959 A EP89120959 A EP 89120959A EP 0384965 A3 EP0384965 A3 EP 0384965A3
Authority
EP
European Patent Office
Prior art keywords
stabilized
subprojectile
fin
submunition
submunitions
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.)
Withdrawn
Application number
EP19890120959
Other languages
German (de)
English (en)
French (fr)
Other versions
EP0384965A2 (de
Inventor
Gerhard Dr. Glotz
Werner Grosswendt
Helmut Dr. Peller
Jens Dr. Seidensticker
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.)
Rheinmetall Industrie AG
Original Assignee
Rheinmetall 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 Rheinmetall GmbH filed Critical Rheinmetall GmbH
Publication of EP0384965A2 publication Critical patent/EP0384965A2/de
Publication of EP0384965A3 publication Critical patent/EP0384965A3/de
Withdrawn legal-status Critical Current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
    • F42B10/66—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
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22—Homing guidance systems
    • F41G7/2233—Multimissile systems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22—Homing guidance systems
    • F41G7/2253—Passive homing systems, i.e. comprising a receiver and do not requiring an active illumination of the target
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22—Homing guidance systems
    • F41G7/2273—Homing guidance systems characterised by the type of waves
    • F41G7/2293—Homing guidance systems characterised by the type of waves using electromagnetic waves other than radio waves
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/01—Arrangements thereon for guidance or control

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Electromagnetism (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Gyroscopes (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Preparation Of Compounds By Using Micro-Organisms (AREA)
  • Lasers (AREA)
EP19890120959 1989-03-01 1989-11-11 Flügelstabilisierter Submunitionskörper Withdrawn EP0384965A3 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3906372 1989-03-01
DE3906372A DE3906372A1 (de) 1989-03-01 1989-03-01 Fluegelstabilisierter submunitionskoerper

Publications (2)

Publication Number Publication Date
EP0384965A2 EP0384965A2 (de) 1990-09-05
EP0384965A3 true EP0384965A3 (de) 1992-08-12

Family

ID=6375175

Family Applications (1)

Application Number Title Priority Date Filing Date
EP19890120959 Withdrawn EP0384965A3 (de) 1989-03-01 1989-11-11 Flügelstabilisierter Submunitionskörper

Country Status (4)

Country Link
US (1) US5037040A (pt)
EP (1) EP0384965A3 (pt)
CA (1) CA2011046A1 (pt)
DE (1) DE3906372A1 (pt)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5261629A (en) * 1989-04-08 1993-11-16 Rheinmetall Gmbh Fin stabilized projectile
DE29512894U1 (de) * 1995-08-10 1995-10-26 Mafo Systemtechnik Dr.-Ing. A. Zacharias GmbH & Co. KG, 83317 Teisendorf Waffe
US6502785B1 (en) * 1999-11-17 2003-01-07 Lockheed Martin Corporation Three axis flap control system
US20070089628A1 (en) * 2005-10-20 2007-04-26 Elder Steven M Firearm ammunition having improved flight and impact characteristics
SE534614C2 (sv) * 2010-02-25 2011-10-25 Bae Systems Bofors Ab Granat anordnad med utfällbara vingar och styranordning
US9464876B2 (en) * 2014-05-30 2016-10-11 General Dynamics Ordnance and Tacital Systems, Inc. Trajectory modification of a spinning projectile by controlling the roll orientation of a decoupled portion of the projectile that has actuated aerodynamic surfaces
CN110077588B (zh) 2019-04-22 2022-05-20 大连理工大学 一种可垂直起降的海陆空潜四栖航行器

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3282540A (en) * 1964-05-05 1966-11-01 Henry S Lipinski Gun launched terminal guided projectile
EP0028966A1 (fr) * 1979-11-09 1981-05-20 Thomson-Brandt Armements Procédé de pilotage et de guidage de projectiles en phase terminale de vol
EP0081421A1 (fr) * 1981-12-09 1983-06-15 Thomson-Brandt Armements Méthode de guidage terminal et missile guidé opérant selon cette méthode
DE3337873A1 (de) * 1982-10-18 1984-04-19 Raytheon Co., 02173 Lexington, Mass. Geschoss fuer granatwerfersysteme
US4598884A (en) * 1984-11-28 1986-07-08 General Dynamics Pomona Division Infrared target sensor and system

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3304434A (en) * 1965-06-01 1967-02-14 Bunker Ramo Position control system employing pulse producing means indicative of magnitude and direction of movement
US4533094A (en) * 1982-10-18 1985-08-06 Raytheon Company Mortar system with improved round

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3282540A (en) * 1964-05-05 1966-11-01 Henry S Lipinski Gun launched terminal guided projectile
EP0028966A1 (fr) * 1979-11-09 1981-05-20 Thomson-Brandt Armements Procédé de pilotage et de guidage de projectiles en phase terminale de vol
EP0081421A1 (fr) * 1981-12-09 1983-06-15 Thomson-Brandt Armements Méthode de guidage terminal et missile guidé opérant selon cette méthode
DE3337873A1 (de) * 1982-10-18 1984-04-19 Raytheon Co., 02173 Lexington, Mass. Geschoss fuer granatwerfersysteme
US4598884A (en) * 1984-11-28 1986-07-08 General Dynamics Pomona Division Infrared target sensor and system

Also Published As

Publication number Publication date
CA2011046A1 (en) 1990-09-01
EP0384965A2 (de) 1990-09-05
US5037040A (en) 1991-08-06
DE3906372A1 (de) 1990-09-13
DE3906372C2 (pt) 1991-06-27

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