Crucible CG27 is a forgeable iron-nickel base alloy having an excellent combination of high temperature stress-rupture and tensile properties. It resists oxidation up to 1500 F and is recommended for gas turbine engines and turbine wheels. 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 and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: SS-219. Producer or source: Crucible Materials Corporation.

UDIMET WASPALOY is a nickel-base, austenitic, precipitation-hardenable alloy. It features outstanding tensile and stress-rupture strength up to 1400 F and high oxidation resistance up to 1600 F. It is used widely in gas turbine engines, airframe assemblies and missile systems. 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: Ni-257. Producer or source: Special Metals Corporation.

ALUMINUM A201 offers high strength, high impact resistance, a good combination of room and elevated-temperature performance, and good ballistic properties. Its ballistic properties are comparable to those of the standard wrought aluminum alloys. Among its many application are components for military aircraft and missiles, and impellers for gas turbine engines. This datasheet provides information on composition, physical properties, 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 casting, heat treating, machining, joining, and surface treatment. Filing Code: Al-234. Producer or source: Consolidated Aluminum Corporation.

AISI No. 685 is a nickel-base, austenitic, precipitation-hardenable alloy. It has excellent tensile and stress-rupture strength to 1400 F and high resistance to corrosion and oxidation at temperatures at least to 1600 F. It is used widely in airframe assemblies, gas turbine engines and missile systems. This datasheet provides information on composition, physical properties, hardness, and tensile properties as well as fracture toughness and creep. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-271. Producer or source: Nickel alloy mills.

CARPENTER WASPALOY is a precipitation-hardening nickel-base alloy designed for use at elevated temperatures. It is used for gas turbine engine parts requiring considerable strength and corrosion resistance up to 1600 F. The alloy is usually vacuum-induction melted or vacuum induction plus vacuum-arc remelted. This datasheet provides information on composition, physical properties, 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: Ni-328. Producer or source: Carpenter.

Pyromet CTX-1 is a high-strength, precipitation-hardenable superalloy exhibiting a low coefficient of thermal expansion and high strength up to about 1200 deg F. The alloy possesses high hot hardness and good thermal fatigue resistance. Its applications include components for gas turbine engines, hot-work die applications and high-pressure hydrogen environments. 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 and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: FE-56. Producer or source: Carpenter. Originally published February 1976, revised May 1997.

The CMSX-10 superalloy is a proprietary, third-generation, single-crystal (SX) casting material. It is characterized by a 6 wt.% Re content, a relatively high refractory element level (W+Ta+Re+Mo), and a low chromium level. CMSX-10 is a production status material that has been actively evaluated for gas turbine engine applications. This datasheet provides information on composition, physical properties, and tensile properties as well as fracture toughness, creep, and fatigue. It also includes information on corrosion resistance as well as forming and heat treating. Filing Code: Ni-533. Producer or source: Cannon-Muskegon Corporation.

AISI No. 615 is a hardenable chromium-nickel-tungsten martensitic corrosion resistant steel used primarily at temperatures up to 1050 F. It is used for compressor blades, vanes, discs, and other gas turbine engine components. 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 high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: SS-175. Producer or source: Alloy steel mills and foundries.

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.

WASPALOY is a vacuum induction melted nickel-base alloy having outstanding tensil and stress-rupture strength up to 1400 F combined with high oxidation resistance up to 1600 F. It is recommended for gas turbine engines, airframe assemblies and missile systems. 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 low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-129. Producer or source: Union Carbide Corporation, Materials Systems Division.

PYROMET CTX-3 is a high-strength precipitation-hardenable low-expansion superalloy. It exhibits a low coefficient of thermal expansion over a broad temperature range combined with high strength. The alloy possesses high hot hardness and good resistance to thermal fatigue. It is brazable, weldable and can be plated with chromium. CTX-3 uses comprise compressor and exhaust casings, seals and other components for gas turbine engines. 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: Fe-78. Producer or source: Carpenter.

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.

Haynes alloy 75 is an 80 nickel-20 chromium alloy with both good oxidation resistance and good mechanical properties at high temperatures. It is amenable to all forms of fabrication and welding. A typical application for sheet metal is fabrications in gas turbine engines. 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 and heat treating. Filing Code: Ni-557. Producer or source: Haynes International Inc.

Haynes Waspaloy is a specially vacuum melted, nickel-base alloy having outstanding tensile and stress-rupture strength up to 760 deg C (1400 deg F) combined with high oxidation resistance up to 871 deg C (1600 deg F). It is recommended for gas turbine engines, airframe assemblies, and missile systems. 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 and machining. Filing Code: Ni-560. Producer or source: Haynes International Inc.

TIMETAL 829 is a Ti-5.5Al-3.5Sn-3Zr-1Nb-0.25Mo-0.3Si near-alpha titanium alloy that is weldable and has high strength and is a creep resistant high temperature alloy. The major application is as gas turbine engine components. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness, creep, and fatigue. It also includes information on forming and heat treating. Filing Code: TI-118. Producer or source: Timet.

Timetal 551 is an improved-strength version of Timetal 550 alloy that retains good forging characteristics. The alpha-beta alloy has a nominal composition of Ti-4Al-4Mo-4Sn-0.5 Si, and it is used in gas turbine engine parts. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and shear strength as well as creep. It also includes information on high temperature performance as well as forming and heat treating. Filing Code: TI-138. Producer or source: Timet.

UPM Nickel Alloy 188 (UNS R30188 / Werkstoff Number 2.4683) is a low-carbon, cobalt-nickel-chromium-tungsten alloy that combines excellent high-temperature strength with very good oxidation resistance up to 1095 °C (2000 °F). It is widely used in commercial and military aircraft gas turbine engines. This datasheet provides information on composition and physical properties. It also includes information on forming and joining. Filing Code: Co-130. Producer or source: United Performance Metals.

MAR-M Alloy 918 is a cobalt-base alloy for service in applications where high strength and oxidation resistance are required. 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, machining, and joining. Filing Code: Co-63. Producer or source: Martin Metals Division, Martin Marietta Corporation.

MAR-M Alloy 200 is a nickel-base alloy designed primarily as a cast turbine blade material which retains useful strength up to 1900 F. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on high temperature performance as well as heat treating and joining. Filing Code: Ni-107. Producer or source: Martin Metals Company.

CMSX-11B is a non-rhenium containing single-crystal (SX) superalloy defined primarily for industrial turbine applications. The material develops a unique and extremely good blend of hot corrosion and oxidation resistance. It exhibits extremely good castability, employs relatively simple solution heat treatments, and provides creep strength that is as good or better than other first generation SX materials such as CMSX-2 (Alloy Digest Ni-417, November 1992), CMSX-3 (Alloy Digest Ni-420, January 1993), CMSX-4 (Alloy Digest Ni-447, March 1994), CMSX-6 (Alloy Digest Ni-418, December 1992), PWA 1480, and Rene N4. This datasheet provides information on composition and physical properties as well as creep. It also includes information on corrosion resistance as well as casting and heat treating. Filing Code: Ni-537. Producer or source: Cannon-Muskegon Corporation.