MA-X alloy is a Ni-22Cr-18Fe-9Mo-1.5Co-0.6W (mass %) nickel alloy that has excellent strength and oxidation resistance at high temperature and with good formability. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on high temperature performance as well as forming, heat treating, and joining. Filing Code: Ni-731. Producer or source: Hitachi Metals.

INCONEL Alloy MA 6000 is a nickel-base alloy produced by mechanical alloying. It is strengthened by both oxide dispersion strengthening and precipitation hardening for high creep and rupture properties at 2000 F (1095 C) as well as at 1400 F (760 C). The alloy's composition also gives it excellent resistance to oxidation and sulfidation. Alloy MA 6000 was developed as a blade material for advanced gas turbines. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep and fatigue. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ni-288. Producer or source: Huntington Alloy Products Division, An INCO Company.

Zirconium Copper is an age hardenable electrical conductivity alloy which develops high strength when heat treated. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on forming, heat treating, machining, and joining. Filing Code: Cu-551. Producer or source: Copper and copper alloy mills.

Inconel alloy MA 754 is an oxide-dispersion-strengthened nickel-chromium alloy produced by mechanical alloying. It offers the advantages of a wrought high-temperature material in service environments where only cast alloys could be used in the past. Its strength in conjunction with its high melting point and microstructural stability makes it an attractive alloy for extreme service applications. This datasheet provides information on composition, physical properties, microstructure, elasticity, and tensile properties as well as fracture toughness, creep, and fatigue. It also includes information on high temperature performance and corrosion resistance as well as forming. Filing Code: Ni-244. Producer or source: Inco Alloys International Inc.. Originally published May 1977, revised March 1990.

MONEL alloy 401 is a copper-nickel alloy with high electrical resistance and is used primarily in specialized electrical and electronic applications. It has a negligible temperature coefficient of electrical resistance and good corrosion resistance. This datasheet provides information on composition, physical properties, hardness, and tensile properties. It also includes information on forming, heat treating, and machining. Filing Code: Cu-216. Producer or source: Huntington Alloy Products Division.

SANDVIK 253 MA is a high-temperature austenitic stainless steel with good creep strength and high-temperature corrosion resistance. It is manufactured by Sandvik under license from Avesta. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, and joining. Filing Code: SS-527. Producer or source: Sandvik.

INCOLOY Alloy MA 956 is manufactured by mechanical alloying, which uniformly disperses yttrium oxide for dispersion strengthening to the alloy's melting point. The alloy combines strength at high temperatures with excellent resistance to oxidation, carburization and hot corrosion. These attributes make it an especially suitable material for applications involving rigorous service conditions at elevated temperatures. Alloy MA 956 is available only in sheet form. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Fe-67. Producer or source: Huntington Alloy Products Division, An INCO Company.

AVESTA 353 MA is a high-temperature austenitic stainless steel with excellent scaling resistance, creep strength at elevated temperatures, with carburization and nitriding resistance. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness and creep. It also includes information on corrosion resistance as well as forming, heat treating, and joining. Filing Code: SS-532. Producer or source: Avesta Stainless Inc..

ALLOY X-40 is a cobalt-base high temperature alloy having high tensile and creep properties in precision-castings. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as heat treating, machining, and joining. Filing Code: Co-10. Producer or source: General Electric Company. Originally published December 1956, revised June 1963.

Inconel alloy MA 758 is a further development of the well-established aerospace superalloy Inconel alloy MA 754 (Alloy Digest Ni-244, March 1990) with an increased chromium content for better resistance to high-temperature corrosives. This datasheet provides information on composition, physical properties, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as machining, joining, and powder metal forms. Filing Code: Ni-511. Producer or source: Inco Alloys International Inc.

Finkl Alu-X is a modification of UNS A92618 with higher thermal conductivity than many aluminum alloys used for molds. The alloy, when forged, solution treated, and stabilized, is well suited for pressure applications. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength. It also includes information on casting, machining, joining, and surface treatment. Filing Code: AL-363. Producer or source: A. Finkl & Sons Company.

ZAMAK 2 is the strongest and hardest of the four Zamak alloys. While generally produced by die casting, ZAMAK 2 is occasionally gravity cast. It is not a widely used alloy. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well as fracture toughness and fatigue. It also includes information on corrosion resistance as well as casting, forming, heat treating, machining, and joining. Filing Code: Zn-51. Producer or source: Noranda Sales Corporation.

RA 153MA is an austenitic heat resistant stainless steel with good strength and oxidation resistance through 1800 F (982 C) This datasheet provides information on composition, physical properties, and tensile properties as well as creep. It also includes information on corrosion resistance as well as forming, heat treating, and joining. Filing Code: SS-524. Producer or source: Rolled Alloys Inc..

HASTELLOY Alloy C-4 is a nickel-chromium-molybdenum alloy with outstanding high-temperature stability as shown by high ductility and corrosion resistance even after long-time aging in the range 1200-1900 F. Alloy C-4 also has excellent resistance to stress-corrosion cracking and to oxidizing atmospheres up to 1900 F. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ni-211. Producer or source: Stellite Division, Cabot Corporation.

Carpenter Project 70 stainless type 347 is a modified version of type 347 stainless steel with improved machinability when compared to conventional type 347. The alloy is a nonhardenable austenitic chromium-nickel steel that is particularly adaptable for parts for use at temperatures between 427 and 899 C (800 and 1650 F). It is nonmagnetic in the annealed condition but is slightly magnetic in the cold-worked condition. Among its many applications are aircraft-engine exhaust manifolds, boiler shells, and high-temperature handling equipment. This datasheet provides information on composition, physical properties, and elasticity. It also includes information on corrosion resistance as well as forming. Filing Code: SS-730. Producer or source: Carpenter. Originally published October 1998, corrected November 1998.

ORVAR SUPREME is a chromium-molybdenum-vanadium alloyed steel. Special processing techniques and close control are responsible for its high purity and very fine structure. It has improved isotropic properties. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on forming, heat treating, machining, and joining. Filing Code: TS-493. Producer or source: Uddeholm Corporation.

ALLVAC 80A is an 80% Ni/20% Cr alloy which is strengthened by precipitation hardening through the addition of Ti and A1. It is produced by vacuum induction plus vacuum are remelting. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ni-379. Producer or source: Allvac Inc..

HAYNES STELLITE alloy No. 6K is a cobalt-base alloy with outstanding resistance to most types of wear. Its wear resistance is a built-in characteristic and not the result of heat-treatment, plating, nitriding, or other methods used to produce a superficial hardness on metal parts. Among its many applications are cutting knives and blades for many materials, apple-paring knives in canneries and wear strips in conveyor channels. This datasheet provides information on composition, physical properties, elasticity, and compressive strength. It also includes information on wear resistance as well as forming, heat treating, machining, and joining. Filing Code: Co-20. Producer or source: Stellite Division, Cabot Corporation. Originally published May 1960, revised July 1978.

NIMARK 300 is a vacuum melted low carbon, 18% nickel alloy steel which attains yield strengths in excess of 270,000 psi. It is recommended for high strength, shock resisting applications. 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, and joining. Filing Code: SA-254. Producer or source: Carpenter.

ALUMINUM 6066 is a heat treatable aluminum alloy having good strength and excellent fabricating characteristics. It was developed as an extrusion alloy. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-63. Producer or source: Harvey Aluminum Company.