WO2020152165A1 - Système de charge explosive d'un missile comportant une charge creuse à action latérale et une charge à fragmentation à action latérale - Google Patents

Système de charge explosive d'un missile comportant une charge creuse à action latérale et une charge à fragmentation à action latérale Download PDF

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Publication number
WO2020152165A1
WO2020152165A1 PCT/EP2020/051409 EP2020051409W WO2020152165A1 WO 2020152165 A1 WO2020152165 A1 WO 2020152165A1 EP 2020051409 W EP2020051409 W EP 2020051409W WO 2020152165 A1 WO2020152165 A1 WO 2020152165A1
Authority
WO
WIPO (PCT)
Prior art keywords
charge
explosive
arrangement according
fragment
shaped
Prior art date
Application number
PCT/EP2020/051409
Other languages
German (de)
English (en)
Inventor
Aubrey SIMON
Fakhree MAJIET
Jean TERBLANCHE
Original Assignee
Rheinmetall Denel Munition (Pty) Ltd.
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 Denel Munition (Pty) Ltd. filed Critical Rheinmetall Denel Munition (Pty) Ltd.
Publication of WO2020152165A1 publication Critical patent/WO2020152165A1/fr

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/20—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
    • F42B12/201—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type characterised by target class
    • F42B12/202—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type characterised by target class for attacking land area or area targets, e.g. airburst
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/04—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type
    • F42B12/10—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with shaped or hollow charge
    • F42B12/14—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with shaped or hollow charge the symmetry axis of the hollow charge forming an angle with the longitudinal axis of the projectile
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/04—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type
    • F42B12/10—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with shaped or hollow charge
    • F42B12/16—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with shaped or hollow charge in combination with an additional projectile or charge, acting successively on the target
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/20—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
    • F42B12/22—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type with fragmentation-hull construction
    • F42B12/32—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type with fragmentation-hull construction the hull or case comprising a plurality of discrete bodies, e.g. steel balls, embedded therein or disposed around the explosive charge

Definitions

  • the invention relates to an explosive charge arrangement of a rocket with the features of the preamble of claim 1.
  • a warhead for a missile in the form of a multi-purpose warhead is known from the generic DE 33 36 853 A1.
  • the multi-purpose warhead has a tube-like shell, with at least three active parts being arranged one behind the other within the shell.
  • the tip of the multi-purpose warhead forms a first active part with a shaped charge and with a conical shaped charge lining arranged rotationally symmetrically to the longitudinal axis.
  • a second active part configured as a projectile is arranged between the first active part and a third active part containing fragment fragments.
  • the second active part has conical recesses open on both sides symmetrically to a longitudinal axis.
  • Each active part is equipped with an explosive charge specific to the respective type of assignment, which can differ in composition and explosive effect.
  • Each active part is equipped with a separate ignition device.
  • a warhead with a hollow and a fragmentary charge is known from DE 27 46 666.
  • the warhead has a cylindrical shell and a conical hood which form a housing for the warhead.
  • An explosive charge is arranged inside this housing, namely in the area of the casing.
  • a shaped charge lining is arranged in the center.
  • Two splinter zones are arranged in the shape of a cylinder segment on the inner circumference of the cylindrical shell. These splinter zones are arranged axially symmetrical to one another with respect to the longitudinal axis.
  • the shaped charge is aligned with the hood and thus acts in the direction of flight of the rocket.
  • the generic explosive charge arrangement is not yet optimal.
  • the invention has for its object to improve the generic explosive charge arrangement.
  • the explosive charge arrangement is part of a rocket and has a shaped charge and a fragment charge, the shaped charge having an explosive and a metal insert, the fragment charge having a further explosive and several fragment fragments.
  • the shaped charge and the fragmentary charge are oriented transversely to a longitudinal direction of the rocket, the shaped charge emerging laterally from the rocket after the one explosive and the fragmentary charge after the other explosive.
  • targets can be combated in the flyby.
  • Armored targets can also be fought with a hollow charge escaping from the side when the missile is flying by.
  • the rocket is aligned during flight, namely rotated about its longitudinal axis, that the shaped charge and the fragmentary charge point towards the target at the moment of the flyby.
  • the missile is equipped with several explosive charge arrangements, the hollow charge and the fragmentary charge being directed from different explosive charge arrangements in different transverse directions in order to To increase the probability of hits or to have to rotate the rocket through a smaller angle during the flight.
  • This explosive charge arrangement is particularly suitable for combating other missiles.
  • this explosive charge arrangement can be used to combat slow-flying objects, such as UAVs and in particular drones.
  • the shaped charge and the fragmentary charge occur transversely to the flight direction, i.e. laterally across the longitudinal axis of the rocket.
  • the shaped charge and the fragment fragments emerge in the radial direction relative to the longitudinal axis of the rocket.
  • the fragmentary charge is preferably arranged circumferentially around the shaped charge.
  • the fragmentary charge forms a passage in which the shaped charge is arranged. This has the advantage that even if the shaped charge misses the target, a relatively large effective range is covered by the fragment fragments, so that the probability of destroying the target is increased.
  • the emerging fragment fragments preferably do not cover the full angular range of 360 °, but in particular an angular range of less than 180 °.
  • the fragment fragments can in particular cover an angular range of up to 135 ° of the circumference of the rocket.
  • the hollow charge is preferably arranged within a housing, the housing having a cylindrical region and a cup-like region adjoining the cylindrical region.
  • the open end of the cylindrical region faces the shell of the missile.
  • the shaped charge emerges through the open end of the cylindrical region.
  • the explosive of the shaped charge is arranged inside the housing.
  • the fragmentation charge is preferably arranged around the housing.
  • the fragment fragments can be stacked in the transverse direction, whereby several layers of fragment fragments are formed. As a result, many fragment fragments can be arranged in a compact volume.
  • the housing is preferably made of aluminum. There are different ways of arranging the shaped charge and the fragment charge.
  • the fragment fragments are arranged within a shell of the rocket along a cylindrical ring segment, the cylindrical ring segment extending concentrically to the shell.
  • the cylindrical ring segment preferably has a circumferential opening angle of at least 90 °.
  • the fragment fragments and the explosive of the fragment charge are arranged around the cylindrical region of the housing.
  • the fragment fragments can thus be arranged as close as possible to the shell.
  • the fragmentary charge surrounds a head end of the
  • the fragmentary charge can be arranged in a ring around the head end of the shaped charge.
  • the fragment fragments are preferably arranged between the explosive and the shell of the missile. This ring forms a circular passage, the shaped charge being arranged in the passage.
  • the fragment fragments can be arranged in a ring around the shaped charge, the ring shape not following the inner contour of the shell of the missile.
  • a major part of the explosive of the fragmentary charge is preferably arranged around the pot-like area of the housing.
  • a cavity can thus be formed between the shell and the fragmentary charges.
  • the fragmentary charge essentially surrounds the base end of the shaped charge in a circular manner.
  • the fragment fragments are arranged in a circle around the shaped charge on one end face of the explosive of the fragment charge.
  • the fragment fragments are stacked in the ejection direction. It is conceivable that an empty space remains between the housing. With this arrangement, the effective range of the fragment charge is narrower and the fragment waves are shot out essentially parallel to the shaped charge beam.
  • the fragment fragments can be formed with their own explosive charge, which detonates at the latest when it hits the target.
  • This explosive charge of the fragment fragments can be used, for example, to trigger an ignition of an explosive of the target.
  • the Splinter fragments can be arranged separately from one another in individual housings, which has the advantage that explosive charges can be arranged within the individual housings. If the individual casings with the explosive charges hit the target, the explosive charges detonate, which can lead to the destruction of the target.
  • the fragment fragments are preferably cube-shaped or spherical. This facilitates the manufacture of the fragment fragments.
  • the fragment fragments can have steel and / or tungsten.
  • the metal insert of the shaped charge is preferably designed as a shaped charge cone.
  • the shaped charge cone is preferably made of copper.
  • the explosives associated with the shaped charge and the fragmentary charge have different detonation speeds.
  • the explosive of the shaped charge preferably has a higher detonation speed than the explosive of the fragmentary charge.
  • the shaped charge and the fragmentary charge have different explosives, whereby according to the invention the explosive of the shaped charge detonates faster than the explosive of the fragmentary charge.
  • the shaped charge preferably has an octogen explosive (HMX) and the fragment charge has a hexogen explosive (RDX). Both explosives are detonated using a detonator at the base of the shaped charge. Due to the different detonation speeds of the explosives, the shaped charge jet can escape completely before the fragment charge detonates. An interaction between the two detonations can thereby be avoided.
  • FIG. 2 shows the first explosive charge illustration from FIG. 1 in a schematic, sectional illustration
  • FIG. 3 shows the first explosive charge arrangement according to FIGS. 1 and 2 in a schematic, longitudinal and cross-sectional representation
  • FIG. 4 shows a rocket with a second explosive charge arrangement in a schematic representation
  • FIG. 5 shows a schematic representation of the second explosive charge arrangement in a longitudinal section
  • FIG. 6 shows the second explosive charge arrangement in a cross-sectional illustration.
  • the wings 4 are circumferentially spaced in a rear area and in a front area. Eight wings 4 are preferably provided. It is conceivable that fewer than eight, for example three, four or six, wings are also present.
  • the missile 1 from FIG. 1 now has an explosive charge arrangement 5 and the missile 1 from FIG. 4 has an explosive charge arrangement 6.
  • Each of the explosive charge arrangements 5, 6 has a shaped charge 7 and one
  • the explosive charge arrangements 5, 6 do not have to be arranged on the head of the missile, but are in particular arranged in a central fuselage area of the missile 1.
  • the explosive charge arrangement 5, 6 are designed such that the shaped charge 7 and the fragmentary charge 8 can emerge from the missile 1 and act in a lateral direction. With the lateral direction here is a transverse direction to the longitudinal axis of the missile 1 designated.
  • the shaped charge 7 and the fragmentary charge 8 act essentially in the radial direction relative to the longitudinal axis of the rocket 1, ie also radially to the direction of flight of the rocket 1.
  • the shaped charge 7 and the fragmentary charge 8 are arranged within the shell 2 of the rocket 1.
  • the hollow charge 7 and the fragmentary charge 8 act transversely to the longitudinal direction 1 of the missile 1, targets in the flyby can be combated very well. In particular, missiles can be combated as a bypass by flying.
  • the hollow charge 7 and the fragment charge 8 are each assigned a separate explosive 9, 10.
  • the shaped charge 7 and the fragmentary charge 8 have explosives 9, 10, the explosive 9 of the shaped charge 7 detonating faster than the explosive
  • the explosive 9 has a higher detonation speed than the explosive 10. Both explosives 9, 10 are detonated by means of a detonator (not shown) at the base of the shaped charge 7. Due to the different detonation speeds of the explosives 9, 10, the shaped charge jet (not shown) can escape completely before the fragmentary charge 8 detonates and emerges. An interaction between the two detonations can thereby be avoided.
  • the shaped charge 7 has a metal insert 11 in the form of a shaped charge cone
  • the shaped charge cone 11 preferably has copper.
  • the axis of symmetry (not shown) of the shaped charge cone 11 is aligned in the radial direction of the rocket 1.
  • the shaped charge cone 11 thus points in the radial direction on the inner peripheral surface of the cylindrical shell 2.
  • the fragment charge 8 has a plurality of fragment fragments 12.
  • the fragment fragments 12 are preferably made of steel or tungsten.
  • the fragment fragments 12 are arranged between the shell 2 and the corresponding explosive 10. Viewed in the axial direction, the shaped charge 7 is arranged centrally to the fragment charge 8.
  • the fragmentary charge 8 surrounds the shaped charge 7.
  • the explosive charge arrangement 5 is characterized in that the fragmentary charge 8 is arranged near a head end 13 of the shaped charge 7.
  • the fragment fragments 12 are arranged between the explosive 10 and the shell 2 of the rocket 1.
  • the fragment charge 8 has a preferably circular passage 14 for the shaped charge 7.
  • the splinters 12 cover an angular range of preferably 135 ° of the circumference of the missile 1.
  • the fragment fragments 12 are arranged in an annular cylinder segment with an opening angle of preferably 135 °. No fragment fragments 12 are arranged in the area of the passage 14.
  • the explosive 10 is arranged in a cylinder segment, the cylinder segment likewise having the same opening angle as the cylinder ring segment of the fragmentation charge 8.
  • the explosive 10 likewise has a passage 15, the hollow charge 7 with the corresponding explosive 9 being arranged within the passage 15.
  • the explosive 9 is arranged within a housing 16.
  • the shaped charge cone 11 is arranged within the housing 16.
  • the space between the shaped charge cone 11 and the housing 16 is filled with the explosive 9.
  • the housing 16 has a cylindrical region which engages in the passage 15.
  • the passage 15 is designed to match the outer circumference of the housing 16. Up to the igniter (not shown in detail), the housing 16 tapers like a pot outside the passage 15.
  • the housing is made in particular of aluminum. A relatively large effective range can be generated by this arrangement of the fragment charge 8.
  • the individual fragment fragments 12 are each preferably arranged in further individual housings (not shown in more detail). Individual explosive charges of the fragment fragments 12 are thereby separated from one another.
  • the fragment fragments 12 can thus be designed with their own explosive charge, which is arranged within the individual housing. These explosive charges can detonate when they hit the target.
  • the explosive charge of the fragment fragments 12 can trigger an ignition of a further explosive charge of the target, whereby the target is destroyed.
  • FIGS. 2 and 3 there is no space between the fragment charge 8 and the shell 2.
  • the fragmentary charge 8 lies on the circumference of the shell 2.
  • a cavity 17 is present between the splinter arrangement 8 and the inner peripheral surface of the shell 2, ie the fragment fragments 12 are arranged here spaced apart from the inner peripheral surface of the shell 2.
  • the shaped charge arrangement 7 is designed as shown in FIGS. 2 and 3 and also has a housing 16. However, the explosive 10 is no longer arranged exclusively in the region of the passage 15, ie in the region of the cylindrical section of the housing 16, but in particular also in the region of the pot-like region of the housing 16.
  • the fragment charge 8 is here ring-shaped around the sleeve-shaped region of the housing 16 arranged.
  • the fragment fragments are not arranged here on a cylinder segment in the course of the inner circumferential surface of the shell 2, but only in the form of a ring.
  • the fragment fragments 12 are arranged on a face of the explosive 10 in a circle around the shaped charge 7.
  • the fragment fragments 12 are stacked in the transverse or ejection direction.
  • Two levels of fragment fragments 12 are arranged here, ie two circular layers of fragment fragments 12 are arranged around the shaped charge 7. With this arrangement, the effective range of the fragment charge 8 is narrower and the fragment fragments 12 are shot out essentially parallel to the shaped charge beam.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Toys (AREA)

Abstract

L'invention concerne un système de charge explosive (5, 6) d'un missile (1), ledit système de charge explosive comportant une charge creuse (7) et une charge à fragmentation (8), la charge creuse (7) présentant une matière explosive (9) et un insert métallique (11), la charge à fragmentation (8) présentant une matière explosive (10) et plusieurs fragments de fragmentation (12). La tête explosive générique est améliorée en ce que la charge creuse (7) et la charge à fragmentation (8) sont orientées transversalement à la direction longitudinale du missile (1), la charge creuse (8) et la charge à fragmentation (8) sortant chacune latéralement du missile (1) après une mise à feu.
PCT/EP2020/051409 2019-01-24 2020-01-21 Système de charge explosive d'un missile comportant une charge creuse à action latérale et une charge à fragmentation à action latérale WO2020152165A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102019101761.0A DE102019101761A1 (de) 2019-01-24 2019-01-24 Sprengladungsanordnung einer Rakete mit einer seitlich wirkenden Hohlladung mit einer seitlich wirkenden Splitterladung
DE102019101761.0 2019-01-24

Publications (1)

Publication Number Publication Date
WO2020152165A1 true WO2020152165A1 (fr) 2020-07-30

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PCT/EP2020/051409 WO2020152165A1 (fr) 2019-01-24 2020-01-21 Système de charge explosive d'un missile comportant une charge creuse à action latérale et une charge à fragmentation à action latérale

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Country Link
DE (1) DE102019101761A1 (fr)
WO (1) WO2020152165A1 (fr)

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Publication number Priority date Publication date Assignee Title
CN115046436B (zh) * 2022-06-15 2024-03-12 重庆大学 一种适用于复杂构形破片阵列式设计的破片分布规划及其铺贴控制方法
CN115046435B (zh) * 2022-06-15 2024-03-12 重庆大学 一种弹筒内腔体点阵式破片智能铺贴平台及控制方法

Citations (6)

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Publication number Priority date Publication date Assignee Title
US3474731A (en) * 1966-06-30 1969-10-28 Franz Rudolf Thomanek Warhead containing a hollow charge and a fragmentation section
DE2746666A1 (de) 1977-10-18 1979-04-26 Messerschmitt Boelkow Blohm Rotationssymmetrische hohlladung
DE3336853A1 (de) 1983-10-11 1985-04-25 Rheinmetall GmbH, 4000 Düsseldorf Mehrzweckgefechtskopf
DE3525147C1 (de) * 1985-07-13 1987-01-15 Diehl Gmbh & Co Sturz-Flugkoerper zum Bekaempfen von insbesondere Radarstellungen
DE3906098A1 (de) * 1988-02-29 1989-09-07 Deutsch Franz Forsch Inst Hohlladungsgeschoss fuer den angriff im ueberflug
DE102007021401A1 (de) 2006-05-05 2007-11-15 Siemens Canada Ltd., Mississauga Detektor mit magnetischer Dämpfung für eine natürliche Vakuumleckage

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Publication number Priority date Publication date Assignee Title
DE3506225A1 (de) * 1985-02-22 1986-08-28 Diehl GmbH & Co, 8500 Nürnberg Gefechtskopfanordnung
DE3737231A1 (de) * 1987-11-03 1989-05-18 Rheinmetall Gmbh Geschoss
US20120186482A1 (en) * 2010-04-02 2012-07-26 Lloyd Richard M Kinetic energy rod warhead with blast fragmentation
DE102014010180A1 (de) * 2014-07-09 2016-01-14 TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH Vorrichtung an einer zylindrischen Hohlladung

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3474731A (en) * 1966-06-30 1969-10-28 Franz Rudolf Thomanek Warhead containing a hollow charge and a fragmentation section
DE2746666A1 (de) 1977-10-18 1979-04-26 Messerschmitt Boelkow Blohm Rotationssymmetrische hohlladung
DE3336853A1 (de) 1983-10-11 1985-04-25 Rheinmetall GmbH, 4000 Düsseldorf Mehrzweckgefechtskopf
DE3525147C1 (de) * 1985-07-13 1987-01-15 Diehl Gmbh & Co Sturz-Flugkoerper zum Bekaempfen von insbesondere Radarstellungen
DE3906098A1 (de) * 1988-02-29 1989-09-07 Deutsch Franz Forsch Inst Hohlladungsgeschoss fuer den angriff im ueberflug
DE102007021401A1 (de) 2006-05-05 2007-11-15 Siemens Canada Ltd., Mississauga Detektor mit magnetischer Dämpfung für eine natürliche Vakuumleckage

Non-Patent Citations (1)

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Title
ANONYMOUS: "Projektilbildende Ladung - Wikipedia", 24 October 2018 (2018-10-24), XP055683513, Retrieved from the Internet <URL:https://de.wikipedia.org/w/index.php?title=Projektilbildende_Ladung&oldid=182087106> [retrieved on 20200406] *

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