DE58905698D1 - Wing stabilized bullet. - Google Patents

Wing stabilized bullet.

Info

Publication number
DE58905698D1
DE58905698D1 DE89122526T DE58905698T DE58905698D1 DE 58905698 D1 DE58905698 D1 DE 58905698D1 DE 89122526 T DE89122526 T DE 89122526T DE 58905698 T DE58905698 T DE 58905698T DE 58905698 D1 DE58905698 D1 DE 58905698D1
Authority
DE
Germany
Prior art keywords
wing stabilized
stabilized bullet
bullet
wing
stabilized
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 - Fee Related
Application number
DE89122526T
Other languages
German (de)
Inventor
Wilfried Becker
Gerhard Dr Glotz
Helmut Dr Peller
Josef Dr Osthues
Hans-Peter Opitz
Heinz-Josef Dr Kruse
Jutta Peters
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
Application granted granted Critical
Publication of DE58905698D1 publication Critical patent/DE58905698D1/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/01Arrangements thereon for guidance or control
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/60Steering arrangements
    • F42B10/66Steering by varying intensity or direction of thrust

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
DE89122526T 1989-04-08 1989-12-06 Wing stabilized bullet. Expired - Fee Related DE58905698D1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3911576A DE3911576A1 (en) 1989-04-08 1989-04-08 WING STABILIZED SHELL

Publications (1)

Publication Number Publication Date
DE58905698D1 true DE58905698D1 (en) 1993-10-28

Family

ID=6378260

Family Applications (2)

Application Number Title Priority Date Filing Date
DE3911576A Granted DE3911576A1 (en) 1989-04-08 1989-04-08 WING STABILIZED SHELL
DE89122526T Expired - Fee Related DE58905698D1 (en) 1989-04-08 1989-12-06 Wing stabilized bullet.

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE3911576A Granted DE3911576A1 (en) 1989-04-08 1989-04-08 WING STABILIZED SHELL

Country Status (2)

Country Link
EP (1) EP0392086B1 (en)
DE (2) DE3911576A1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19505791C1 (en) * 1995-02-20 1996-08-14 Daimler Benz Aerospace Ag Method and device for combating covertly operating helicopters
DE19847218A1 (en) * 1998-10-13 2000-04-20 Bodenseewerk Geraetetech Seeker head, especially for high-speed missiles
EP1767893B1 (en) * 2005-09-23 2016-12-28 Saab Ab Missile guidance system

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE683586A (en) * 1966-07-04 1966-12-16
US3674227A (en) * 1970-03-23 1972-07-04 Hughes Aircraft Co Fragmenting cover
US4492166A (en) * 1977-04-28 1985-01-08 Martin Marietta Corporation Submunition having terminal trajectory correction
GB2129103A (en) * 1982-10-18 1984-05-10 Raytheon Co Mortar round
US4519315A (en) * 1982-12-20 1985-05-28 The United States Of America As Represented By The Secretary Of The Army Fire and forget missiles system
DE3300709C2 (en) * 1983-01-11 1985-12-19 Friedrich Dr. 8890 Aichach Schäff Rotating missile for engaging airborne targets
FR2590973B1 (en) * 1985-11-29 1988-02-12 France Etat Armement DEVICE FOR TILTING PROJECTILE ON TRAJECTORY

Also Published As

Publication number Publication date
DE3911576A1 (en) 1990-10-11
EP0392086B1 (en) 1993-09-22
DE3911576C2 (en) 1991-09-05
EP0392086A3 (en) 1991-05-02
EP0392086A2 (en) 1990-10-17

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: RHEINMETALL INDUSTRIE GMBH, 40882 RATINGEN, DE

8327 Change in the person/name/address of the patent owner

Owner name: RHEINMETALL INDUSTRIE AG, 40882 RATINGEN, DE

8339 Ceased/non-payment of the annual fee