EP1167914A1 - Projectile autopropulsé avec noyau perforant - Google Patents

Projectile autopropulsé avec noyau perforant Download PDF

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Publication number
EP1167914A1
EP1167914A1 EP00810536A EP00810536A EP1167914A1 EP 1167914 A1 EP1167914 A1 EP 1167914A1 EP 00810536 A EP00810536 A EP 00810536A EP 00810536 A EP00810536 A EP 00810536A EP 1167914 A1 EP1167914 A1 EP 1167914A1
Authority
EP
European Patent Office
Prior art keywords
self
core
cavity
propelled projectile
projectile according
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Withdrawn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
EP00810536A
Other languages
German (de)
English (en)
Inventor
Rolf Oechslin
Jürg Dr. Meister
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.)
SM Schweizerische Munitionsunternehmung AG
Original Assignee
SM Schweizerische Munitionsunternehmung AG
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 SM Schweizerische Munitionsunternehmung AG filed Critical SM Schweizerische Munitionsunternehmung AG
Priority to EP00810536A priority Critical patent/EP1167914A1/fr
Priority to AT01937921T priority patent/ATE339669T1/de
Priority to DE50111011T priority patent/DE50111011D1/de
Priority to PL01358748A priority patent/PL358748A1/xx
Priority to AU2001263707A priority patent/AU2001263707A1/en
Priority to IL15325801A priority patent/IL153258A0/xx
Priority to EP01937921A priority patent/EP1292804B1/fr
Priority to PCT/CH2001/000380 priority patent/WO2001098728A1/fr
Priority to JP2002504444A priority patent/JP2004501339A/ja
Publication of EP1167914A1 publication Critical patent/EP1167914A1/fr
Priority to ZA200209732A priority patent/ZA200209732B/en
Priority to US10/323,515 priority patent/US6672218B2/en
Priority to NO20026084A priority patent/NO20026084L/no
Withdrawn legal-status Critical Current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
    • 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
    • F42B12/204—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 structures, e.g. specific buildings or fortifications, ships or vehicles
    • 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
    • F42B12/06—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 hard or heavy core; Kinetic energy penetrators
    • 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
    • F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
    • F42B12/46—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing gases, vapours, powders or chemically-reactive substances
    • F42B12/50—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing gases, vapours, powders or chemically-reactive substances by dispersion

Definitions

  • the present invention relates to a self-propelled Projectile according to the preamble of claim 1 or 2.
  • an arrow projectile in particular to use a detonating arrow in such a way that a locally limited effect is achieved in the target becomes.
  • the arrow floor is said to be the usual walls of buildings, bulletproof glass but also shelters made of reinforced concrete, light armored vehicles with aluminum alloy plates or hit barricades, especially from sandbags and persons behind it unable to fight or facilities put inoperative.
  • the subject of the invention is intended to be conventional Use weapon systems and / or concepts and before can be used above all with their launchers (platforms) his.
  • the invention is intended for both non-lethal and lethal acting inserts may be suitable.
  • a puncture core penetrates Bunker target and the like, without being damaged itself, so that active substances can be introduced into the target area are set to a preselected effect.
  • a non-lethal agent is particularly useful for police operations suitable, for example, in raids or at Temporary hostage taking of one or more people temporarily combat sets claim 3.
  • the design of a floor according to claim 5 results a lethal weapon acting in a larger room.
  • a stepped tip according to claim has proven particularly useful 6, which was practically undamaged and also heavily reinforced Penetrates concrete walls.
  • a taper of the arrow shaft according to claim is advantageous 7, since this is the frictional resistance when penetrating reduced.
  • the punch core can be kept to a minimum Forces to be opened from the inside.
  • 1 denotes an arrow-like punch core. This has a cavity 2, which is the Tapered tip and merges seamlessly into a cap.
  • one Active charge 3 in the present case a desensitized one High-performance explosives stored without voids.
  • Behind the Active charge 3 is a balancing spring 7 with a central ignition channel 8; after the spring 7 is a subpoena 4 arranged with a detonator 5 'of an autonomous Ignition device 5 forms a known ignition chain.
  • a mounting flange is located at the rear of the punch core 1 6, the easy integration of the core 1 with a drive A not shown here allowed.
  • the tip 10 of the punch core 1 is towards the rear side discontinued.
  • a relatively obtuse arrow angle ⁇ 1 goes at a more acute angle ⁇ 2 in a subsequent taper shaft 11 over; towards the rear is the cylindrical one Arrow shaft 12 tapers by a small angle ⁇ , which facilitates its intrusion into the target.
  • FIG. 1 The shape of a punch core 1 shown in FIG. 1 shows a surprisingly good penetration, even in a speed range of 160 - 240 m / s. Obviously "clears" the hard tip 10 with an arrow angle ⁇ 1, on which a characteristic energy of 50,000 Joule works, most materials away. - A clean one physical explanation for the phenomenal effect of Punch core 1 is not available.
  • FIG. 2 shows in simplified form a rocket to be fired from a tube 22 in the characteristic form of a a karooka.
  • the launch speed v 0 is a maximum of 300 m / s.
  • the drive A is designed in a conventional manner, as is the rear tail unit 21.
  • the penetration core 1, which contains a non-lethal active substance 3b is placed behind the two-part ballistic hood 20 on the drive A.
  • FIG. 3 remove Further details of this embodiment are shown in FIG. 3 remove.
  • this is a purely lethal penetration core 1.
  • an explosive charge 3a in which additional a splinter-forming ring 3c (splinter matrix) is embedded is the one that detonates together with the fragmenting one Core 1 a variety of splinters of different sizes forms.
  • the mounting flange 6 is positively in the hood 20 here screwed.
  • a support ring 23 In the middle part of the hood 20 is a support ring 23 arranged, which merges into a centering ring 24 and the punch core 1 axially symmetrically centered. With an additional weight 25 the center of gravity becomes 9 - symbolized - in the same position shifted, like a conventional apelooka.
  • the resulting outside ballistics is identical to that the usual apelooka, which is known to be a Contains shaped charge.
  • FIG. 4 shows the course of the speed of a device according to the invention as a function of the trajectory (firing distance) D from the shot to the point of impact on the target a o and the detonation a z .
  • an ignition device which from the secured state via an accelleration unlocking A-E and a retardation release R-E detonator 5 'in that shown in Figs. 1 and 3 Focus pivots.
  • Suitable ignition devices with an integrated ignition generator, Security elements and a high detonator Services are commercially available (EMS-Patvag AG, CH-7013 Domat / Ems; Type PEPZ-05).
  • This detonator is said to have a shock resistance of 100,000 g.
  • the way such works Detonator is described in detail in EP -A- 104 138 in connection with U.S. Patent 5,269,223. - It follows that the igniters on almost everyone with the Subject of the invention conceivable intended use are.
  • the punch core 1 is advantageously made of an alloy Quenched and tempered steel manufactured according to DIN 34CrNiMo6 also commercially available (Gebr. Böhler & Co. AG, CH-8304 Wallisellen; Type V155).
  • the angle ⁇ 1 is preferably Embodiment 70 °; the angle ⁇ 2 is 30 ° and the ⁇ (suit) 1.4 o / oo.
  • the hardness profile is for obvious reasons of the punch core 1 decreasing from the tip to the rear set.
  • a hostage-taker is entrenched in one Counter space of a bank, so by locating (bearing) the Mobile radio a through core 1 with capsaicin 3b in the direction Hostage takers are shot without any line of sight - A suddenly through a wall or barrier penetrating projectile paralyzes it Fright so that no opposition can take place within the next second, the core 1 detonates; a relative large amount of capsaicin is sprayed and sets the hostage-taker completely out of action for a long time, so that parallel the police walk into the building unscathed and can do their job.
  • non-lethal agents such as tear gas, mist etc. only minor Amounts of explosives built into cavity 2.
  • suitable notches in the inner wall are already sufficient Centripetal forces around the active ingredient from a bursting Exit core or spray around it leave, especially if a mechanical connection (adhesive) between the drug container and the core consist.
  • the projectile and the punch core are accordingly modular and interchangeable optimized with regard to collateral damage and risk - As a rule, there is only a hole in the Size of the punch core in the target or wall to be penetrated, so that the consequential damage of a Are low.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Dispersion Chemistry (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Discharge By Other Means (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)
  • Coils Or Transformers For Communication (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Toys (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Emergency Lowering Means (AREA)
  • Catching Or Destruction (AREA)
  • Drilling Tools (AREA)
  • Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
  • Drilling And Exploitation, And Mining Machines And Methods (AREA)
EP00810536A 2000-06-19 2000-06-19 Projectile autopropulsé avec noyau perforant Withdrawn EP1167914A1 (fr)

Priority Applications (12)

Application Number Priority Date Filing Date Title
EP00810536A EP1167914A1 (fr) 2000-06-19 2000-06-19 Projectile autopropulsé avec noyau perforant
IL15325801A IL153258A0 (en) 2000-06-19 2001-06-18 Self-driven projectile with a penetrator core
DE50111011T DE50111011D1 (de) 2000-06-19 2001-06-18 Selbstangetriebenes geschoss mit einem durchschlagskern
PL01358748A PL358748A1 (en) 2000-06-19 2001-06-18 Self-driven projectile with a penetrator core
AU2001263707A AU2001263707A1 (en) 2000-06-19 2001-06-18 Self-driven projectile with a penetrator core
AT01937921T ATE339669T1 (de) 2000-06-19 2001-06-18 Selbstangetriebenes geschoss mit einem durchschlagskern
EP01937921A EP1292804B1 (fr) 2000-06-19 2001-06-18 Projectile autopropulse a noyau de penetration
PCT/CH2001/000380 WO2001098728A1 (fr) 2000-06-19 2001-06-18 Projectile autopropulse a noyau de penetration
JP2002504444A JP2004501339A (ja) 2000-06-19 2001-06-18 貫通コアを有する自己推進式発射体
ZA200209732A ZA200209732B (en) 2000-06-19 2002-11-29 Self-driven projectile with a penetrator core.
US10/323,515 US6672218B2 (en) 2000-06-19 2002-12-18 Self-propelling projectile having a penetrator core
NO20026084A NO20026084L (no) 2000-06-19 2002-12-18 Selvdrevet prosjektil med en penetrasjonskjerne

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP00810536A EP1167914A1 (fr) 2000-06-19 2000-06-19 Projectile autopropulsé avec noyau perforant

Publications (1)

Publication Number Publication Date
EP1167914A1 true EP1167914A1 (fr) 2002-01-02

Family

ID=8174763

Family Applications (2)

Application Number Title Priority Date Filing Date
EP00810536A Withdrawn EP1167914A1 (fr) 2000-06-19 2000-06-19 Projectile autopropulsé avec noyau perforant
EP01937921A Expired - Lifetime EP1292804B1 (fr) 2000-06-19 2001-06-18 Projectile autopropulse a noyau de penetration

Family Applications After (1)

Application Number Title Priority Date Filing Date
EP01937921A Expired - Lifetime EP1292804B1 (fr) 2000-06-19 2001-06-18 Projectile autopropulse a noyau de penetration

Country Status (11)

Country Link
US (1) US6672218B2 (fr)
EP (2) EP1167914A1 (fr)
JP (1) JP2004501339A (fr)
AT (1) ATE339669T1 (fr)
AU (1) AU2001263707A1 (fr)
DE (1) DE50111011D1 (fr)
IL (1) IL153258A0 (fr)
NO (1) NO20026084L (fr)
PL (1) PL358748A1 (fr)
WO (1) WO2001098728A1 (fr)
ZA (1) ZA200209732B (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102009020137A1 (de) 2009-05-06 2010-07-22 Institut für Luft- und Kältetechnik gGmbH Verfahren und Vorrichtung zum zielgenauen Applizieren von in Flüssiggas gelösten Reizstoffen über größere Entfernungen
DE10303106B4 (de) * 2002-01-29 2013-01-10 Ruag Munition Barrikadenbrecher

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU2003212584A1 (en) * 2003-03-25 2004-10-18 Ruag Munition Projectile comprising a sub-caliber penetrator core
EP1664662B1 (fr) 2003-09-17 2010-03-24 Saab Bofors Dynamics Switzerland Ltd. Projectile perforant
US7278358B2 (en) * 2004-01-22 2007-10-09 Pdt Tech, Llc. Non-lethal marking bullet for related training cartridges
US7225741B2 (en) * 2004-01-22 2007-06-05 Pdt Tech, Llc Reduced energy training cartridge for self-loading firearms
ES2276278T3 (es) * 2004-02-13 2007-06-16 Ruag Ammotec Rompedor de barricadas.
FR2871226B1 (fr) * 2004-06-08 2006-08-18 Tda Armements Sas Soc Par Acti Projectile, notamment bombe de penetration anti- infrastructure et procede de penetration d'un tel projectile a travers une paroi
US20070144393A1 (en) * 2005-12-22 2007-06-28 Maximillian Kusz Caseless ammunition with internal propellant
US7621220B1 (en) 2007-09-19 2009-11-24 Sanford Matthew J Wall penetrating, agent dispensing warhead
RU2457427C1 (ru) * 2011-02-25 2012-07-27 Открытое акционерное общество "Федеральный научно-производственный центр "Научно-исследовательский институт прикладной химии" Фугасный или осколочно-фугасный боеприпас
RU2477831C2 (ru) * 2011-05-27 2013-03-20 Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации Артиллерийский осколочно-фугасный снаряд
US8869703B1 (en) * 2012-10-19 2014-10-28 Textron Systems Corporation Techniques utilizing high performance armor penetrating round
RU2558758C1 (ru) * 2014-01-17 2015-08-10 Николай Евгеньевич Староверов Боевой поражающий элемент
RU2560230C2 (ru) * 2014-01-17 2015-08-20 Николай Евгеньевич Староверов Усиленный патрон /варианты/ и способ его изготовления
US20170138712A1 (en) * 2015-11-12 2017-05-18 Randy S. Teig Mechanically adaptable projectile and method of manufacturing the same
US20180321021A1 (en) * 2015-11-12 2018-11-08 Randy S. Teig Mechanically adaptable projectile and method of manufacturing the same
DE102016008391B4 (de) 2016-07-09 2018-05-24 Diehl Defence Gmbh & Co. Kg Geschoss
US10731955B2 (en) * 2017-04-13 2020-08-04 Lawrence Livermore National Security, Llc Modular gradient-free shaped charge
WO2019048914A1 (fr) * 2017-09-09 2019-03-14 Ruag Ammotec Ag Projectile de sécurité blindé conçu en particulier pour des applications polyvalentes
DE102018104333A1 (de) * 2018-02-26 2019-08-29 Rwm Schweiz Ag Geschoss mit pyrotechnischer Wirkladung

Citations (5)

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Publication number Priority date Publication date Assignee Title
FR1209802A (fr) * 1948-01-09 1960-03-03 Tech De Rech S Ind & Mecanique Engin offensif à réaction
US3302570A (en) * 1965-07-23 1967-02-07 Walter G Finch Armor piercing, fragmenting and incendiary projectile
DE1900604A1 (de) * 1968-02-23 1969-10-30 Oerlikon Buehrle Ag Geschoss mit Heckteil
EP0104138A2 (fr) 1982-09-16 1984-03-28 Ems-Inventa AG Dispositif pour armer et neutraliser une fusée électrique pour munition
US5269223A (en) 1992-10-06 1993-12-14 Ems-Patvag Piezoelectric fuse system with safe and arm device for ammunition

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US904255A (en) * 1907-12-07 1908-11-17 Emil Gathmann Projectile.
US3103888A (en) * 1962-03-22 1963-09-17 Rosenthal Henry Anti-pillaring smoke shell
US3935817A (en) * 1971-07-28 1976-02-03 General Dynamics Corporation Penetrating spear
FR2339833A1 (fr) * 1976-01-30 1977-08-26 Thomson Brandt Corps perforant de projectile et munition equipee d'un tel corps
USH1235H (en) * 1986-06-18 1993-10-05 The United States Of America As Represented By The Secretary Of The Navy Armor-piercing projectile
DE3940462A1 (de) * 1989-12-07 1991-06-13 Rheinmetall Gmbh Splittergeschoss
ATE168768T1 (de) * 1990-01-16 1998-08-15 Tda Armements Sas Penetratormunition für ziele mit hohem mechanischem widerstand
US6393992B1 (en) * 1996-11-18 2002-05-28 Jaycor Tactical Systems, Inc. Non-lethal projectile for delivering an inhibiting substance to a living target
US20030047105A1 (en) * 1996-11-18 2003-03-13 Jaycor Tactical Systems, Inc. Non-lethal projectile systems
US5939662A (en) * 1997-12-03 1999-08-17 Raytheon Company Missile warhead design
US6145441A (en) * 1998-04-02 2000-11-14 The United States Of America As Represented By The Secretary Of The Navy Frangible payload-dispensing projectile
US6276277B1 (en) * 1999-04-22 2001-08-21 Lockheed Martin Corporation Rocket-boosted guided hard target penetrator
US6494140B1 (en) * 1999-04-22 2002-12-17 Lockheed Martin Corporation Modular rocket boosted penetrating warhead

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1209802A (fr) * 1948-01-09 1960-03-03 Tech De Rech S Ind & Mecanique Engin offensif à réaction
US3302570A (en) * 1965-07-23 1967-02-07 Walter G Finch Armor piercing, fragmenting and incendiary projectile
DE1900604A1 (de) * 1968-02-23 1969-10-30 Oerlikon Buehrle Ag Geschoss mit Heckteil
EP0104138A2 (fr) 1982-09-16 1984-03-28 Ems-Inventa AG Dispositif pour armer et neutraliser une fusée électrique pour munition
US5269223A (en) 1992-10-06 1993-12-14 Ems-Patvag Piezoelectric fuse system with safe and arm device for ammunition

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WAFFEN REVUE, no. 7, December 1972 (1972-12-01), Journal Verlag Schwend GmbH, Schwäbisch Hall, pages 1163, XP002153615 *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10303106B4 (de) * 2002-01-29 2013-01-10 Ruag Munition Barrikadenbrecher
DE102009020137A1 (de) 2009-05-06 2010-07-22 Institut für Luft- und Kältetechnik gGmbH Verfahren und Vorrichtung zum zielgenauen Applizieren von in Flüssiggas gelösten Reizstoffen über größere Entfernungen

Also Published As

Publication number Publication date
NO20026084L (no) 2003-01-09
IL153258A0 (en) 2003-07-06
NO20026084D0 (no) 2002-12-18
ATE339669T1 (de) 2006-10-15
JP2004501339A (ja) 2004-01-15
PL358748A1 (en) 2004-08-23
DE50111011D1 (de) 2006-10-26
EP1292804B1 (fr) 2006-09-13
WO2001098728A1 (fr) 2001-12-27
AU2001263707A1 (en) 2002-01-02
ZA200209732B (en) 2004-02-25
US6672218B2 (en) 2004-01-06
EP1292804A1 (fr) 2003-03-19
US20030205160A1 (en) 2003-11-06

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