MATRIX I is an ultra high-strength alloy steel capable of reaching tensile strength values up to 360,000 psi and maintaining high strength levels at operating temperatures to 1000 deg F. It combines extremely high strength with ductility, toughness, fatigue and heat resistance. The alloy was formerly designated VASCOJET M-A(CVM); see Alloy Digest SA-150, July 1963. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness and fatigue. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: SA-449. Producer or source: Teledyne Vasco.

3M TITANIUM MATRIX COMPOSITES are produced by electron-beam evaporation to apply Ti-6Al-4V coating to high-strength, high-modulus silicon carbon fibers. The resulting composite has increased strength and stiffness over monolithic titanium/titanium alloy parts. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive and shear strength as well as creep and fatigue. It also includes information on surface treatment. Filing Code: TI-111. Producer or source: 3M Metal Matrix Composites Program.

DURALCAN W2A.xxA-T6 is a heat-treatable wrought aluminum alloy metal-matrix composite, where xx represents the volume percent of alumina particulate, Al2O3. The base alloy is 2014 (Alloy Digest Al-185, March 1969). This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness and fatigue. It also includes information on corrosion and wear resistance. Filing Code: AL-334. Producer or source: Duralcan USA.

DURALCAN F3D is a general purpose die casting composite with a matrix alloy similar to 380 (See Alloy Digest Al-239, July 1982). This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fatigue. It also includes information on high temperature performance and wear resistance. Filing Code: AL-331. Producer or source: Duralcan USA.

This pure aluminum matrix composite contains 60 volume% alumina. The aluminum ceramic fiber is Nextel 610. The fiber effects the longitudinal direction, resulting in a high longitudinal specific modulus and a specific strength with good off-axis properties. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive and shear strength. It also includes information on corrosion resistance as well as casting. Filing Code: AL-344. Producer or source: 3M.

The Al-2wt.%Cu matrix composite contains 60 vol.% alumina. The aluminum ceramic fiber is Nextel 610, which affects the longitudinal direction, resulting in a high longitudinal specific modulus and a specific strength with good off-axis properties. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive and shear strength as well as fatigue. It also includes information on corrosion resistance. Filing Code: AL-345. Producer or source: 3M.

DURALCAN W2F.xxA is a heat-treatable wrought aluminum alloy matrix composite, where xx represents the volume percent of alumina particulate, Al2O3. The base alloy is aluminum 2618 (Alloy Digest Al-76, February 1959). This datasheet provides information on composition, physical properties, microstructure, elasticity, and tensile properties as well as fracture toughness and fatigue. It also includes information on high temperature performance and wear resistance. Filing Code: AL-337. Producer or source: Duralcan USA.

DURALCAN F3N.xxS is an aluminum composite with virtually no Cu or Ni designed for use in corrosion-sensitive applications. The matrix alloy is similar to 360 (See Alloy Digest Al-103, May 1961, and Al-245, April 1983). This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness. It also includes information on corrosion resistance. Filing Code: AL-332. Producer or source: Duralcan USA.

VASCO MATRIX II-CVM is a highly alloyed steel having good high temperature strength and heat resistance. It has the composition and strength of the high-speed tool-steel matrix without the embrittling carbides being present. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness. It also includes information on forming, heat treating, machining, and joining. Filing Code: SA-200. Producer or source: Vanadium Alloys Steel Company.

DURALCAN W6A.xxA is a heat-treatable wrought aluminum alloy matrix composite, where xx represents the volume percent of alumina particulate, Al2O3. The base alloy is 6061 (Alloy Digest Al-205, January 1973). This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness. It also includes information on high temperature performance, corrosion and wear resistance as well as machining. Filing Code: AL-333. Producer or source: Duralcan USA.

Duralcan F3S.xxS is a heat treatable aluminum alloy-matrix gravity composite. The base alloy is similar to Aluminum 359 (Alloy Digest Al-188, July 1969); the discontinuously reinforced composite is silicon carbide. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive strength as well as fracture toughness and fatigue. It also includes information on high temperature performance. Filing Code: AL-329. Producer or source: Alcan Aluminum Corporation.

Lanxide 92-X-2050 is an aluminum-10 Silicon-1 Magnesium-1 Iron alloy with 30 vol.% of silicon carbide particulate. This metal-matrix composite is designed to outperform the unreinforced counterpart. The alloy-matrix composite is available as die castings. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fatigue. It also includes information on casting. Filing Code: AL-343. Producer or source: Lanxide Corporation.

Lanxide 93-X-3027 is an aluminum magnesium alloy with 50 or 60 vol.% of aluminum oxide. This metal-matrix composite is designed to outperform the unreinforced counterpart. This datasheet provides information on composition, physical properties, microstructure, elasticity, and tensile properties as well as fracture toughness and creep. Filing Code: AL-339. Producer or source: Lanxide Corporation.

DURALCAN F3K.xxS is a heat-treatable aluminum alloy-matrix gravity composite, where xx represents the volume percent of particulate. The base alloy is similar to 339, while the composite is silicon carbide. The metal-matrix composite is designed for use at elevated temperature. This datasheet provides information on composition, physical properties, and tensile properties as well as creep. Filing Code: AL-330. Producer or source: Alcan Aluminum Corporation.

6092/SiC/17.5P is a discontinuous metal-matrix composite fully characterized for discontinuously reinforced alloy (DRA) structural applications. The base alloy is Aluminum Association 6092, and the reinforcement material is SiC. This datasheet provides information on composition, physical properties, tensile properties, and compressive, shear, and bearing strength as well as fatigue. It also includes information on as well as machining and surface treatment. Filing Code: AL-359. Producer or source: DWA Aluminum Composites.

TRIBALOY T-700 consists of a hard, intermetallic phase in a softer, nickel-base matrix. It can be cast or hardfaced. As alloy powder it can be plasma sprayed or blended with other powders for P/M (Powder/Metallurgy) processing. It combines outstanding wear and corrosion resistance for use in pumps, extruders, bearings, mixers and particularly elements of nuclear reactors. It has excellent resistance to wear in liquid sodiium. This datasheet provides information on composition, physical properties, hardness, and compressive strength as well as fracture toughness, creep, and fatigue. It also includes information on corrosion and wear resistance as well as heat treating, machining, joining, and powder metal forms. Filing Code: Ni-221. Producer or source: E. I. DuPont de Nemours & Company Inc..

KEVLAR/J-2 is an advanced thermoplastic composite material based on J-2 copolymer reinforced with continuous KEVLAR fiber. The inherent fiber/matrix compatibility of this composite provides attractive mechanical properties. This datasheet provides information on physical properties, tensile properties, and compressive and shear strength. It also includes information on corrosion resistance. Filing Code: Cp-14. Producer or source: E. I. Dupont de Nemours & Company Inc..

KEVLAR 49 is a high-modulus para-aramid reinforcing fiber. It is a widely used organic reinforcing fiber in advanced composites. It has exceptional strength and stiffness and is a low density material. This datasheet provides information on physical properties, tensile properties, and compressive and shear strength. It also includes information on high temperature performance as well as machining. Filing Code: Cp-10. Producer or source: E. I. Dupont de Nemours & Company Inc..

AVIMID N / GRAPHITE is a carbon-fiber/polyimide, high-temperature composite tooling material developed to fabricate quality parts from prepregs based on thermoplastics. This datasheet provides information on physical properties, and tensile properties as well as fracture toughness. It also includes information on high temperature performance. Filing Code: Cp-11. Producer or source: E. I. Dupont de Nemours & Company Inc..

Columbium D43 is a columbium-base alloy with inhibited grain growth during prolonged exposure at high temperature. It is recommended for high temperature service. This datasheet provides information on composition, physical properties, microstructure, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Cb-9. Producer or source: E. I. Dupont de Nemours & Company Inc..