Harvey HA-7146 is an alpha-beta type titanium-base bar and forging alloy developed to combine high temperature strength and stability with good forgability. It is recommended for aircraft gas turbine engine components due to its improved stress stability and creep resistance. It responds to an age hardening heat treatment. This datasheet provides information on composition, physical properties, hardness, 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, heat treating, machining, joining, and surface treatment. Filing Code: Ti-39. Producer or source: Harvey Aluminum Company.

Ti-679 is a titanium high temperature alloy having an excellent combination of short-time strength, creep strength and stability to 900 F. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Ti-48. Producer or source: Titanium Metals Corporation of America.

MST 431 is an alpha-beta type sheet alloy presently being supplied in the solution treated, solution treated and aged, and annealed conditions. Its principal advantage is good formability in the solution treated condition with subsequent high strength capability through an aging treatment. Properties indicate good strength and thermal stability for sheet applications up to 800 F for long times. 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, joining, and surface treatment. Filing Code: Ti-30. Producer or source: Reactive Metals Corporation.

Ti-7AI-12Zr is an alpha-type titanium alloy recommended for high temperature applications in the 800-1100 F range where minimum creep and high Creep strength are required. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and bend strength 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: Ti-46. Producer or source: Reactive Metals Corporation.

Cleveland-Cliffs Thermak 17 is a ferritic stainless steel that is stabilized with both titanium and niobium. When given a high-temperature, final solution anneal, the alloy exhibits dramatic creep resistance. The dual stabilization prevents carbide sensitization exposure and makes the alloy thermally non-hardenable. Cleveland-Cliffs Thermak 17 is designed for demanding, hot-end automotive exhaust applications where intermediate or high chromium grades may not be sufficient or where down gauging for lightweighting is desired. This datasheet provides information on composition, physical properties, hardness, and tensile properties as well as creep. It also includes information on corrosion resistance as well as forming and joining. Filing Code: SS-1345. Producer or source: Cleveland-Cliffs Inc.

RMI 6Al-2Sn-4Zr-2Mo is an alpha-beta titanium alloy that provides a tensile strength of 130,000 psi in the mill-annealed condition. It is characterized by an excellent combination of tensile strength, creep strength, toughness and high-temperature stability that makes it suitable for service to 1050 F. It is recommended for use where high creep strength is required, as in components for jet engines. It has outstanding advantages for long-time use at temperature to 800 F. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and bend strength as well as creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ti-83. Producer or source: RMI Company.

Zilloy 20 is a wrought zinc-base alloy having good stability and creep resistance. It is recommended for architectural applications, and for formed articles requiring maximum creep resistance. This datasheet provides information on composition, physical properties, hardness, and tensile properties as well as creep. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Zn-9. Producer or source: New Jersey Zinc Company.

ATI 6-2-4-2 is a near-alpha, high strength, titanium alloy that exhibits a good combination of tensile strength, creep strength, toughness, and long-term stability at temperatures up to 425 °C (800 °F). Silicon up to 0.1% frequently is added to improve the creep resistance of the alloy. This datasheet provides information on composition, physical properties, hardness, and tensile properties as well as creep. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Ti-169. Producer or Source: ATI.

ATI 6-6-2 (UNS R56620) is a highly beta-stabilized, two-phase, alpha-beta titanium alloy which is a modification of the Ti-6Al- 4V system. Because of the higher beta stabilizing elements (additional vanadium plus iron and copper), this alloy has a higher strength potential than ATI Ti-6Al-4V alloy, but at a sacrifice of weldability and toughness. In most cases, the welding of ATI 6-6-2 is not recommended. It can be used in the annealed or solution treated and aged conditions. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on forming, heat treating, machining, and joining. Filing Code: Ti-189. Producer or source: ATI.

EASTERN STAINLESS TYPE 348 is a stabilized type of stainless steel free from the chromium carbide precipitates that cause intergranular corrosion. It is recommended for welded components that cannot be annealed after welding. It also is used for parts that are heated and cooled intermittently to temperatures between 800 and 1600 F. Type 348 is stabilized by an addition of columbium. Tantalum is restricted to 0.10% maximum and cobalt is restricted to 0.20% maximum. Because of these restrictions, Type 348 is recommended for use in applications such as those encountered in radioactive service. This datasheet provides information on composition, physical properties, hardness, 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, heat treating, machining, joining, and surface treatment. Filing Code: SS-447. Producer or source: Eastern Stainless Steel Company.

ALLVAC 6A1-6V-2Sn is a highly beta stabilized alpha + beta titanium alloy, a modification of the 6 A1-4V system. Added vanadium plus copper and iron produce the stabilizing effect. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ti-98. Producer or source: Teledyne Allvac.

Ed Fagan Molybdenum Lanthanum Oxide, often referred to as lanthanated molybdenum, MoLa or ML, is an oxide dispersion strengthened alloy. It is produced by combining small amounts of lanthanum oxide (La2O3) particles with molybdenum. This creates a special stacked fiber microstructure that is stable at temperatures up to 2000 °C (3630 °F). After recrystallization, the elongated grain structure with jagged grain boundaries provides a measurable increase in ductility and creep resistant strength over that seen with pure molybdenum. Ed Fagan Molybdenum Lanthanum Oxide is the preferred material when embrittlement after recrystallization must be avoided. This alloy maintains its dimensional shape stability at high-temperatures. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep. It also includes information on wear resistance as well as heat treating and machining. Filing Code: Mo-21. Producer or source: Ed Fagan Inc.

MAR-M Alloy 432 is a nickel-base alloy for castings requiring high tensile and creep strengths, excellent hot corrosion resistance and good thermal stability in the temperature range 1200-1800 F (649-982 C). 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 casting, heat treating, machining, joining, and surface treatment. Filing Code: Ni-194. Producer or source: Licensees of Martin Marietta Corporation.

Ti-11 is a super alpha litanium alloy with excellent properties up to at least 1000 F; it has useful properties as high as 1100 F. It offers a good combination of creep resistance and metallurgical and surface stability. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness and creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ti-69. Producer or source: Titanium Metals Corporation of America.

Timetal 6-2-4-2 has a combination of tensile strength, creep strength, toughness, and high-temperature stability for long-term application at temperatures up to 538 deg C (1000 deg F). 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, and joining. Filing Code: TI-140. Producer or source: Timet.

Ti-4A1-3Mo-IV is an alpha-beta type titanium alloy having a good combination of high strength, creep and stability at elevated temperatures. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and shear, bearing, and bend strength as well as creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ti-26. Producer or source: Titanium Metals Corporation of America.

REFRACTALOY 80 is a super heat and oxidation resistant alloy containing high percentages of cobalt, chromium nickel and molybdenum. It has an exceedingly low creep rate at elevated temperatures and shows marked high temperature stability. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Co-7. Producer or source: Westinghouse Electric Corporation.

ZGS 10% Rhodium-Platinum is a grain stabilized platinum-base alloy containing a small amount of highly dispersed zirconium oxide. Its production and general characteristics are closely related to those of ZGS Platinum which also is strenghtened by highly dispersed zirconium oxide (Alloy Digest Pt-2, May 1975). ZGS 10% Rhodium-Platinum is significantly stronger at high temperatures and more creep resistant than the conventional high-temperature rhodium-platinum alloys, while retaining their useful electrical and chemical properties. This datasheet provides information on composition, physical properties, microstructure, hardness, elasticity, and tensile properties as well as creep. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Pt-3. Producer or source: Matthey Bishop Inc..

HARVEY HA8116 is an alpha titanium-base alloy having outstanding creep resistance and high temperature stability. It is non-heat treatable. This datasheet provides information on composition, physical properties, and tensile properties as well as creep. It also includes information on high temperature performance as well as forming, heat treating, and machining. Filing Code: Ti-50. Producer or source: Harvey Aluminum Company.

Ti-6Al-2Sn-4Zr-2Mo is a super-alpha titanium alloy providing an excellent combination of creep strength, tensile strength, toughness and stability to 1050 F. It is recommended for airframe and gas turbine engine requirements. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive, shear, and bearing strength as well as creep. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Ti-52. Producer or source: Titanium Metals Corporation of America.