US3203349A - Projectile or the like, preferably for armor-piercing weapons, and a method of manufacturing such a projectile - Google Patents

Projectile or the like, preferably for armor-piercing weapons, and a method of manufacturing such a projectile Download PDF

Info

Publication number
US3203349A
US3203349A US309493A US30949363A US3203349A US 3203349 A US3203349 A US 3203349A US 309493 A US309493 A US 309493A US 30949363 A US30949363 A US 30949363A US 3203349 A US3203349 A US 3203349A
Authority
US
United States
Prior art keywords
projectile
mixture
bonding section
layer
cobalt
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 - Lifetime
Application number
US309493A
Inventor
Schonberg Nils Erik
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.)
KOHLSWA JERNVERKS AB
Original Assignee
KOHLSWA JERNVERKS AB
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 KOHLSWA JERNVERKS AB filed Critical KOHLSWA JERNVERKS AB
Application granted granted Critical
Publication of US3203349A publication Critical patent/US3203349A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/72Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material
    • F42B12/74Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material of the core or solid body
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/04Projectiles, 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
    • F42B12/06Projectiles, 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

Definitions

  • This invention relates to a projectile or the like, preferably for armor-piercing weapons. To provide such weapons with a satisfactory piercing effect, the projectile must be given considerable weight. For this reason, the projectiles are usually made of cemented carbide or heavy metal.
  • One method for reducing its splintering risk is to manufacture the projectile in several parts. This method makes, however, the manufacture more expensive at the same time as it renders the handling of the projectile more difficult. It is, for example, more complicated to grind smaller than greater parts.
  • a projectile is produced which solve the aforesaid problems and which is characterized in that it comprises two or more parts which are bonded together by one or several layers of metal binders and manufactured simultaneously in a single pressing operation, in such a manner, that the said parts are supplied in powdery state together with the binder layers to a mold and pressed in said mold.
  • the front portion of the projectile is made of heavy metal and the rear portion of the projectile is made of cemented carbide, it is possible, within a volume determined by constructional and ballistic reasons, to fit a projectile of adequate weight and suitable strength into a shell or the like.
  • the heavy metal should have a composition containing 99-80%, preferably about 90% of tungsten and 120%, preferably about of a mixture of copper and nickel.
  • the cemented carbide should have a composition containing 95-75%, preferably about 85% of tungsten carbide and 5-25 preferably about of cobalt.
  • the projectile When the projectile is manufactured on a powder metallurgical way so that it comprises one part of cemented carbide and one part of heavy metal (with the above compositions), the different parts cannot be sintered together directly, because this would cause the formation of highly brittle compounds in the boundary layer. It is neither possible to bond the two parts together only by a layer consisting of cobalt or only by a layer consisting of a mixture of copper and nickel. In such cases the invention proposes the application of two layers, one of them which is located closest to the heavy metal consisting of copper and nickel, and the second layer which is located closest to the cemented carbide consisting of cobalt.
  • the invention renders it possible to manufacture a projectile of two parts and to place the joint between them directly at the transition between a rear cylindrical portion and a conical, rounded or in a similar manner shaped front portion.
  • a material may be chosen which is 3,263,349 Patented Aug. 31, 1965 easier to work, while in the choice of the material for the cylindrical portion greater emphasis should be laid upon its impact properties.
  • the rear cylindrical portion may also be divided into two or more parts which are bonded together in the aforesaid manner.
  • the projectile according to the invention can be manufactured in a very simple manner.
  • the manufacture is based on the use of powder both for the different parts of the projectile and for the metal layer or layers required, the projectile can be made in a single pressing operation.
  • the invention provides also adavntages when a projectile made only of cemented carbide or only of heavy metal is divided and its parts joined according to the invention. It is, namely, the main object of the said method of dividing and joining to prevent the propagation of cracks caused by the impact. Furthermore, due to the joint the projectile according to the invention is given a certain small flexibility so that it shows greater tendency to turn inwards to the plate when its impact direction on the armored plate is oblique. It is, of course, also possible and in certain cases preferable to manufacture a projectile having a front portion of cemented carbide and a rear portion of heavy metal.
  • binder layer For a projectile consisting only of cemented carbide, only one binder layer is required which suitably may be cobalt.
  • the binder layer should preferably have the same mixture of copper and nickel as it is comprised in the heavy metal.
  • cemented carbide and heavy metal The invention may, however, also be worked with other materials suitable for projectiles.
  • the tungsten carbide in the cemented carbide may, for example, entirely or partly be exchanged against, for example, titanium carbide or tantalum carbide.
  • the pressing and sintering operations of the different parts of the projectile may be carried out either in the form of pressure sintering with the help of, for example, graphite tools or in the form of hydrostatic pressing with the help of a mold adapted to be compressed on all sides.
  • a pre-sintering at about 900 C. is carried out so that the different parts will not be harder than to allow their relatively easy grinding or other type of working, whereafter as the final step the product is sintered fully at about 13001400 C.
  • FIG. 1 shows by way of example a projectile according to the invention, whereof an ogival front portion is designated by 1, a cylindrical rear portion by 2 and two binder layers by 3 and 4.
  • the front portion 1 is made of heavy metal having a composition of 90% tungsten and 10% of a mixture of copper and nickel.
  • the rear portion 2, however, is made of cemented carbide having the composition of tungsten carbide and 15% cobalt.
  • the layer 3 is a mixture of copper and nickel, and the layer 4 is of cobalt.
  • the projectile shown as an example was manufactured only on the basis of powder in a single pressing operation.
  • Armor-piercing projectile comprising forward and rear portions and a bonding section joining the interfaces of said Sections together, said forward and rear sections being composed of sintered material and being of uniform composition throughout the respective portions, said bonding section being composed of a metal composition which is capable of bonding to the respective portions and of preventing diffusion in the interfaces of said portions, said forward and rear portions being of different composition and said bonding section being composed of forward and rear layers which are bondable respectively to said forward and rear portions and to each other, said forward portion being composed of a mixture of a heavy metal with copper and nickel, said rear portion being composed of a mixture of a metal carbide and cobalt, the forward layer of said bonding section being composed of a mixture of copper and nickel, and the rear layer of said bonding section being composed of cobalt.
  • Armor-piercing projectile comprising forward and rear portions and a bonding section joining the interfaces of said sections together, said forward and rear sections being composed of sintered material and being of uniform composition throughout the respective portions, said bonding section being composed of a metal composition which is capable of bonding to the respective portions and of preventing diffusion in the interfaces of said portions, said forward and rear portions being of different compositions and said bonding section being composed of forward and rear layers which are bondable respectively to said forward and rear portions and to each other, said forward section being composed of a mixture of from 8099% tungsten and from 1-20% of a mixture of copper and nickel, said rear portion being'composed of a mixture of from 75-95% of tungsten carbide and from 525% cobalt, the forward layer of said bonding section being composed of copper and nickel, and the rear layer of said bonding section being composed of cobalt.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Powder Metallurgy (AREA)

Description

1, 1965 N. E. SCHGNBERG 3,203,349
PROJECTILE OR THE LIKE, PREFERABLY FOR ARMQR-PIERCING WEAPONS, AND A METHOD OF MANUFACTURING SUCH A PROJECTILE Filed Sept. 17, 1963 A To/WVE/ United States Patent PROJECTILE OR THE LIKE, PREFERABLY FOR ARMOR-PIERCING WEAPONS, AND A METHOD OF MANUFACTURING SUCH A PROJECTILE Nils Erik Schiinberg, Kolsva, Sweden, assignor to Kohlswa Jernvel'ks Aktiebolag, Kolsva, Sweden, a Swedish jointstock company Filed Sept. 17, 1963, Ser. No. 309,493 Claims priority, application Sweden, Sept. 18, 1962, 10,0'5'3/ 62 2 Claims. (Cl. 102-52) This invention relates to a projectile or the like, preferably for armor-piercing weapons. To provide such weapons with a satisfactory piercing effect, the projectile must be given considerable weight. For this reason, the projectiles are usually made of cemented carbide or heavy metal.
For ballistic reasons, it is desired to use projectiles which are long in relation to their thickness. Long pro jectiles show, however, splintering tendency in the moment of their impact. As a result thereof, it was heretofore not possible to use projectiles having a length which exceeded their approximate circumference.
One method for reducing its splintering risk is to manufacture the projectile in several parts. This method makes, however, the manufacture more expensive at the same time as it renders the handling of the projectile more difficult. It is, for example, more complicated to grind smaller than greater parts.
According to the invention, a projectile is produced which solve the aforesaid problems and which is characterized in that it comprises two or more parts which are bonded together by one or several layers of metal binders and manufactured simultaneously in a single pressing operation, in such a manner, that the said parts are supplied in powdery state together with the binder layers to a mold and pressed in said mold.
When the front portion of the projectile is made of heavy metal and the rear portion of the projectile is made of cemented carbide, it is possible, within a volume determined by constructional and ballistic reasons, to fit a projectile of adequate weight and suitable strength into a shell or the like.
The heavy metal should have a composition containing 99-80%, preferably about 90% of tungsten and 120%, preferably about of a mixture of copper and nickel.
The cemented carbide should have a composition containing 95-75%, preferably about 85% of tungsten carbide and 5-25 preferably about of cobalt.
When the projectile is manufactured on a powder metallurgical way so that it comprises one part of cemented carbide and one part of heavy metal (with the above compositions), the different parts cannot be sintered together directly, because this would cause the formation of highly brittle compounds in the boundary layer. It is neither possible to bond the two parts together only by a layer consisting of cobalt or only by a layer consisting of a mixture of copper and nickel. In such cases the invention proposes the application of two layers, one of them which is located closest to the heavy metal consisting of copper and nickel, and the second layer which is located closest to the cemented carbide consisting of cobalt.
The invention renders it possible to manufacture a projectile of two parts and to place the joint between them directly at the transition between a rear cylindrical portion and a conical, rounded or in a similar manner shaped front portion. Hereby, grinding and similar finishing operations are facilitated. For the profiled front portion, for example a material may be chosen which is 3,263,349 Patented Aug. 31, 1965 easier to work, while in the choice of the material for the cylindrical portion greater emphasis should be laid upon its impact properties. When desired, the rear cylindrical portion may also be divided into two or more parts which are bonded together in the aforesaid manner.
The projectile according to the invention can be manufactured in a very simple manner. When the manufacture is based on the use of powder both for the different parts of the projectile and for the metal layer or layers required, the projectile can be made in a single pressing operation.
Though it is in many cases most suitable to manufacture the projectile such that it comprises a front part of heavy metal and a rear part of cemented carbide, the invention provides also adavntages when a projectile made only of cemented carbide or only of heavy metal is divided and its parts joined according to the invention. It is, namely, the main object of the said method of dividing and joining to prevent the propagation of cracks caused by the impact. Furthermore, due to the joint the projectile according to the invention is given a certain small flexibility so that it shows greater tendency to turn inwards to the plate when its impact direction on the armored plate is oblique. It is, of course, also possible and in certain cases preferable to manufacture a projectile having a front portion of cemented carbide and a rear portion of heavy metal.
For a projectile consisting only of cemented carbide, only one binder layer is required which suitably may be cobalt. The same applies to the case when the projectile is made only of heavy metal, in which case the binder layer should preferably have the same mixture of copper and nickel as it is comprised in the heavy metal.
In the aforesaid, reference was made only to cemented carbide and heavy metal. The invention may, however, also be worked with other materials suitable for projectiles. The tungsten carbide in the cemented carbide may, for example, entirely or partly be exchanged against, for example, titanium carbide or tantalum carbide.
As already mentioned, great advantages are gained by basing the manufacture of the different projectile parts and of the binder layer on powder. In certain cases, it may, however, be preferable to join a solid metal body with a sintered body made of powder.
The pressing and sintering operations of the different parts of the projectile may be carried out either in the form of pressure sintering with the help of, for example, graphite tools or in the form of hydrostatic pressing with the help of a mold adapted to be compressed on all sides. When the projectile requires working, preferably first a pre-sintering at about 900 C. is carried out so that the different parts will not be harder than to allow their relatively easy grinding or other type of working, whereafter as the final step the product is sintered fully at about 13001400 C.
The aforesaid refers only to examples showing how the invention may be applied in practice. The invention is, however, not restricted to these examples, but a plurality of modifications can be imagined Within the scope of the invention as it is defined in the following claims.
The accompanying drawing shows by way of example a projectile according to the invention, whereof an ogival front portion is designated by 1, a cylindrical rear portion by 2 and two binder layers by 3 and 4.
The front portion 1 is made of heavy metal having a composition of 90% tungsten and 10% of a mixture of copper and nickel. The rear portion 2, however, is made of cemented carbide having the composition of tungsten carbide and 15% cobalt. The layer 3 is a mixture of copper and nickel, and the layer 4 is of cobalt. The projectile shown as an example was manufactured only on the basis of powder in a single pressing operation.
What I claim is:
1. Armor-piercing projectile comprising forward and rear portions and a bonding section joining the interfaces of said Sections together, said forward and rear sections being composed of sintered material and being of uniform composition throughout the respective portions, said bonding section being composed of a metal composition which is capable of bonding to the respective portions and of preventing diffusion in the interfaces of said portions, said forward and rear portions being of different composition and said bonding section being composed of forward and rear layers which are bondable respectively to said forward and rear portions and to each other, said forward portion being composed of a mixture of a heavy metal with copper and nickel, said rear portion being composed of a mixture of a metal carbide and cobalt, the forward layer of said bonding section being composed of a mixture of copper and nickel, and the rear layer of said bonding section being composed of cobalt.
2. Armor-piercing projectile comprising forward and rear portions and a bonding section joining the interfaces of said sections together, said forward and rear sections being composed of sintered material and being of uniform composition throughout the respective portions, said bonding section being composed of a metal composition which is capable of bonding to the respective portions and of preventing diffusion in the interfaces of said portions, said forward and rear portions being of different compositions and said bonding section being composed of forward and rear layers which are bondable respectively to said forward and rear portions and to each other, said forward section being composed of a mixture of from 8099% tungsten and from 1-20% of a mixture of copper and nickel, said rear portion being'composed of a mixture of from 75-95% of tungsten carbide and from 525% cobalt, the forward layer of said bonding section being composed of copper and nickel, and the rear layer of said bonding section being composed of cobalt.
References Cited by the Examiner UNITED STATES PATENTS 2,393,648 1/46 Martin 102/52 FOREIGN PATENTS 538,276 7/41 Great Britain. 288,747 9/31 Italy.
BENJAMIN A. BORCHELT, Primary Examiner.
25 FRED C. MATTERN, JR., Examiner.

Claims (1)

1. ARMOR-PIERCING PROJECTILE COMPRISING FORWARD AND REAR PORTIONS AND A BONDING SECTION JOINING THE INTERFACES OF SAID SECTIONS TOGETHER, SAID FORWARD AND REAR SECTIONS BEING COMPOSED OF SINTERED MATERIAL AND BEING OF UNIFORM COMPOSITION THROUGHOUT THEE RESPECTIVE PORTIONS, SAID BONDING SECTION BEING COMPOSED OF A METAL COMPOSITION WHICH IS CAPABLE OF BONDING TO THE RESPECTIVE PORTIONS AND OF PREVENTING DIFFUSION IN TH EINTERFACES OF SAID PORTIONS, SAID FORWARD AND REAR POSITIONS BEING OF DIFFERENT COMPOSITION AND SAID BONDIND SECTIONS BEING COMPOSED OF FORWARD AND REAR LAYERS WHICH ARE BONDABLE RESPECTIVELY TO SAID FORWARD AND REAR POSITIONS AND TO EACH OTHER, SAID FORWARD PORTION BEING COMPOSED OF A MIXTURE OF A HEAVY METAL WITH A COPPER AND NICKEL, SAID REAR PORTIN BEING COMPOSED OF A MIXTURE OF A METAL CARBIDE AD COBALT, THE FORWARD LAYER OF SAID BONDING SECTION BEING COMPOSED OF A MIXTURE OF COPPER AND NICKEL, AND THE REAR LAYER OF SAID BONDING SECTION BEING COMPOSED OF COBALT.
US309493A 1962-09-18 1963-09-17 Projectile or the like, preferably for armor-piercing weapons, and a method of manufacturing such a projectile Expired - Lifetime US3203349A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE1005362 1962-09-18

Publications (1)

Publication Number Publication Date
US3203349A true US3203349A (en) 1965-08-31

Family

ID=20291590

Family Applications (1)

Application Number Title Priority Date Filing Date
US309493A Expired - Lifetime US3203349A (en) 1962-09-18 1963-09-17 Projectile or the like, preferably for armor-piercing weapons, and a method of manufacturing such a projectile

Country Status (4)

Country Link
US (1) US3203349A (en)
CH (1) CH423550A (en)
DE (1) DE1208656B (en)
GB (1) GB1065265A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3888636A (en) * 1971-02-01 1975-06-10 Us Health High density, high ductility, high strength tungsten-nickel-iron alloy & process of making therefor
US3946673A (en) * 1974-04-05 1976-03-30 The United States Of America As Represented By The Secretary Of The Navy Pyrophoris penetrator
US4108072A (en) * 1964-12-29 1978-08-22 Deutsch-Franzosisches Forschungsinstitut Armor-piercing projectile having spaced cores
US4970960A (en) * 1980-11-05 1990-11-20 Feldmann Fritz K Anti-material projectile
US5069138A (en) * 1989-01-02 1991-12-03 Lars Ekbom Armor-piercing projectile with spiculating core
US6845719B1 (en) * 2003-06-05 2005-01-25 Lockheed Martin Corporation Erosion resistant projectile
EP1521052A1 (en) * 2003-10-03 2005-04-06 Giat Industries Armour perforating projectile

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DK60581A (en) * 1980-03-27 1983-06-23 Rheinmetall Gmbh BREAKING BREAKING MASTER PROJECTILY WITH STACKED FORPENETRATOR
DE3030072A1 (en) * 1980-08-09 1986-06-26 Rheinmetall GmbH, 4000 Düsseldorf MOLDING MOLD, MATERIAL FOR MAKING THE SAME AND METHOD FOR ARRANGING THE MOLDING MOLD IN THE EXTENSION AREA OF AN AIRBULLET MADE OF A HEAVY METAL SINTER ALLOY
DE3037560A1 (en) * 1980-10-04 1984-11-29 Rheinmetall GmbH, 4000 Düsseldorf ARMORING BULLET
DE3301381C2 (en) * 1983-01-18 1986-03-20 Rheinmetall GmbH, 4000 Düsseldorf Explosive projectile
DE4141560C2 (en) * 1991-12-17 1996-02-22 Rheinmetall Ind Gmbh kinetic energy projectile
US6158351A (en) * 1993-09-23 2000-12-12 Olin Corporation Ferromagnetic bullet
WO1996001407A1 (en) * 1994-07-06 1996-01-18 Lockheed Martin Energy Systems, Inc. Non-lead, environmentally safe projectiles and method of making same
WO1996012154A1 (en) * 1994-10-17 1996-04-25 Olin Corporation Ferromagnetic bullet

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB538276A (en) * 1940-01-04 1941-07-28 Martin Littmann Improvements in projectiles for military weapons
US2393648A (en) * 1942-02-20 1946-01-29 Carl A Martin Projectile

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB455910A (en) * 1935-07-24 1936-10-29 British Thomson Houston Co Ltd Improvements in and relating to metal cutting tool bits
GB538268A (en) * 1939-11-10 1941-07-28 Martin Littmann Improvements in projectiles for military weapons

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB538276A (en) * 1940-01-04 1941-07-28 Martin Littmann Improvements in projectiles for military weapons
US2393648A (en) * 1942-02-20 1946-01-29 Carl A Martin Projectile

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4108072A (en) * 1964-12-29 1978-08-22 Deutsch-Franzosisches Forschungsinstitut Armor-piercing projectile having spaced cores
US3888636A (en) * 1971-02-01 1975-06-10 Us Health High density, high ductility, high strength tungsten-nickel-iron alloy & process of making therefor
US3946673A (en) * 1974-04-05 1976-03-30 The United States Of America As Represented By The Secretary Of The Navy Pyrophoris penetrator
US4970960A (en) * 1980-11-05 1990-11-20 Feldmann Fritz K Anti-material projectile
US5069138A (en) * 1989-01-02 1991-12-03 Lars Ekbom Armor-piercing projectile with spiculating core
US6845719B1 (en) * 2003-06-05 2005-01-25 Lockheed Martin Corporation Erosion resistant projectile
EP1521052A1 (en) * 2003-10-03 2005-04-06 Giat Industries Armour perforating projectile
FR2860579A1 (en) * 2003-10-03 2005-04-08 Giat Ind Sa PERFORATING MUNITION
US20050109233A1 (en) * 2003-10-03 2005-05-26 Giat Industries Perforating ammunition
US7063020B2 (en) 2003-10-03 2006-06-20 Giat Industries Perforating ammunition
EP1701131A3 (en) * 2003-10-03 2006-10-04 Giat Industries Armour perforating projectile

Also Published As

Publication number Publication date
DE1208656B (en) 1966-01-05
CH423550A (en) 1966-10-31
GB1065265A (en) 1967-04-12

Similar Documents

Publication Publication Date Title
US3203349A (en) Projectile or the like, preferably for armor-piercing weapons, and a method of manufacturing such a projectile
US2393648A (en) Projectile
US4428295A (en) High density shot
US4836108A (en) Material for multiple component penetrators and penetrators employing same
DE3830347C2 (en) Warhead
US4328925A (en) Hard surfacing for a centrifuge conveyor
US4613370A (en) Hollow charge, or plate charge, lining and method of forming a lining
US3599573A (en) Composite preformed penetrators
US4462293A (en) Wear-resistant and shock-resistant tools and method of manufacture thereof
US6355209B1 (en) Metal consolidation process applicable to functionally gradient material (FGM) compositons of tungsten, nickel, iron, and cobalt
RU2684464C2 (en) Compound roll
US4774889A (en) Armor-piercing projectile
Zagirnyak et al. New methods of obtaining materials and structures for light armor protection
CA1308221C (en) Method of making explosively bonded multi-laminar composite metal plate
DE3242591A1 (en) LOW-LENGTH / DIAMETER RATIO UNDER-CALIBRATION BULLET STOCK
US3566741A (en) Tubular, seamless, dual-hardness armor plate
US20110064600A1 (en) Co-sintered multi-system tungsten alloy composite
IL256732A (en) Penetrator incorporating a core enclosed in a ductile sheath and manufacturing process for such a penetrator
IE811872L (en) Wear resistant tool material
DE1533198B2 (en) SHOCK AND ABRASION RESISTANT COMPOSITE MATERIAL WITH A CARBIDE LAYER
EP1210551B1 (en) A projectile of sintered metal powder
GB2385907A (en) A penetrator
US2973842A (en) Friction element
US2058110A (en) Drawing die
DE19633113B3 (en) Warhead for controlling airborne target e.g. tactical ballistic missiles, has fragments which are fixedly connected to covers of facing surfaces, where fragments and covers are made of layers having different shock wave impedances