EP0176045A1 - Charge militaire explosive - Google Patents

Charge militaire explosive Download PDF

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Publication number
EP0176045A1
EP0176045A1 EP85111911A EP85111911A EP0176045A1 EP 0176045 A1 EP0176045 A1 EP 0176045A1 EP 85111911 A EP85111911 A EP 85111911A EP 85111911 A EP85111911 A EP 85111911A EP 0176045 A1 EP0176045 A1 EP 0176045A1
Authority
EP
European Patent Office
Prior art keywords
warhead
segments
longitudinal axis
angle
tail
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Withdrawn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
EP85111911A
Other languages
German (de)
English (en)
Inventor
Günter Backstein
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 EP0176045A1 publication Critical patent/EP0176045A1/fr
Withdrawn legal-status Critical Current

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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
    • F42B10/02—Stabilising arrangements
    • F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F42B10/16—Wrap-around fins

Definitions

  • the innovation concerns a warhead according to the preamble of protection claim 1.
  • Such a warhead is known from DE-05 22 42 930.
  • the known warhead comprises a warhead housing for receiving a shaped charge and an igniter connected to the warhead housing.
  • the warhead is transported in large numbers by a missile or cargo floor over a target area and is ejected there in order to sink braked or unbraked down to the target area.
  • the well-known warhead In order to stabilize its descent, the well-known warhead has an empennage which consists of several flexible wings that can be wrapped around the warhead.
  • the innovation is based on the task of improving the known warhead with respect to its tail so that this tail takes up less space despite a high launch resistance.
  • a warhead 10 which comprises a warhead housing 11 for receiving a hollow charge 14 having a lining 15 and an igniter 12 connected to the warhead housing 11.
  • a stabilizer 14 is provided to stabilize the descent of the warhead 10 after it has been ejected from the missile or cargo floor.
  • the empennage 14 comprises wing segments 14 a, 14 b, 14 c, which lie against one another, preferably to form a circular area (FIG. 3), and the axes (20 a, 20 b, 20 c) arranged vertically in the igniter 12 in a vertical direction are rotatably mounted to the longitudinal axis of the warhead lying plane.
  • FIG. 3 shows a plan view of only the segments 14 a, 14 b, 14 c, of the tail unit 14, the segments being folded together. Rotation in the direction of the arrows 30 about the axes 20 a, 20 b, 20 c leads to the state shown in FIG. 2, in which the segments 14 a, 14 b, 14 c of the tail unit 14 are unfolded and thereby over the circumference of the The warhead housing 11 protrude. Since the segments 14 a, 14 b, 14 c of the tail unit 14 in the collapsed state (FIG.
  • the axes 20 a In an advantageous development of the innovation, the axes 20 a,
EP85111911A 1984-09-22 1985-09-20 Charge militaire explosive Withdrawn EP0176045A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE8427959U 1984-09-22
DE19848427959 DE8427959U1 (de) 1984-09-22 1984-09-22 Gefechtskopf

Publications (1)

Publication Number Publication Date
EP0176045A1 true EP0176045A1 (fr) 1986-04-02

Family

ID=6770977

Family Applications (1)

Application Number Title Priority Date Filing Date
EP85111911A Withdrawn EP0176045A1 (fr) 1984-09-22 1985-09-20 Charge militaire explosive

Country Status (3)

Country Link
EP (1) EP0176045A1 (fr)
DE (1) DE8427959U1 (fr)
ES (1) ES289145Y (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5063849A (en) * 1989-10-20 1991-11-12 Aktiebolaget Bofors Subwarhead
EP0464589A1 (fr) * 1990-07-02 1992-01-08 Alliant Techsystems Inc. Insert de base pour projectile avec capacité de séparation augmentée par traînée
US9476682B1 (en) * 1989-01-26 2016-10-25 Qinetiq Limited Multi-charge munitions, incorporating hole-boring charge assemblies

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR529443A (fr) * 1919-02-05 1921-11-28 Perfectionnements aux projectiles
US2671398A (en) * 1951-05-11 1954-03-09 Allen S Peck Metal pop-out stabilizing tail for small bombs
US3295444A (en) * 1956-08-02 1967-01-03 Vincent J Cushing Dispersal type cluster warhead
US3964391A (en) * 1973-09-04 1976-06-22 The United States Of America As Represented By The Secretary Of The Army Dispenser-launched munition with two-stage spin-imparting vanes
EP0069899A1 (fr) * 1981-07-14 1983-01-19 Rheinmetall GmbH Méthode, conteneur, moyens et munition pour bombarder en tapis une zone de but

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR529443A (fr) * 1919-02-05 1921-11-28 Perfectionnements aux projectiles
US2671398A (en) * 1951-05-11 1954-03-09 Allen S Peck Metal pop-out stabilizing tail for small bombs
US3295444A (en) * 1956-08-02 1967-01-03 Vincent J Cushing Dispersal type cluster warhead
US3964391A (en) * 1973-09-04 1976-06-22 The United States Of America As Represented By The Secretary Of The Army Dispenser-launched munition with two-stage spin-imparting vanes
EP0069899A1 (fr) * 1981-07-14 1983-01-19 Rheinmetall GmbH Méthode, conteneur, moyens et munition pour bombarder en tapis une zone de but

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9476682B1 (en) * 1989-01-26 2016-10-25 Qinetiq Limited Multi-charge munitions, incorporating hole-boring charge assemblies
US5063849A (en) * 1989-10-20 1991-11-12 Aktiebolaget Bofors Subwarhead
EP0464589A1 (fr) * 1990-07-02 1992-01-08 Alliant Techsystems Inc. Insert de base pour projectile avec capacité de séparation augmentée par traînée

Also Published As

Publication number Publication date
ES289145U (es) 1986-03-01
DE8427959U1 (de) 1985-05-15
ES289145Y (es) 1986-10-01

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Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 19860129

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): DE FR GB IT NL SE

17Q First examination report despatched

Effective date: 19870430

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 19881109

RIN1 Information on inventor provided before grant (corrected)

Inventor name: BACKSTEIN, GUENTER