TECHALLOY WASPALOY, a nickel-base austenitic precipitation-hardenable alloy, derives its high strength at elevated temperatures from additions of the solid-solution strengthening elements molybdenum, cobalt and chromium and from aluminum and titanium which produce age hardening. Boron and zirconium additions also have been made to obtain optimum stress-rupture strength. It has excellent strength and good resistance to corrosion and oxidation at least to 1600 F. 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, machining, joining, and surface treatment. Filing Code: Ni-243. Producer or source: Techalloy Company Inc..

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.

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.

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.

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.

Waspaloy (UNS N07001) is a nickel-base, age hardenable superalloy with excellent high-temperature strength and good corrosion resistance to oxidation. Special Metals offers Waspaloy made by vacuum induction melting and vacuum arc refining (VIM/VAR) or by vacuum induction melting and electroslag refining (VIM/ESR). This datasheet provides information on composition, physical properties, and elasticity. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ni-574. Producer or source: Special Metals.

UNITEMP WASPALOY is a nickel-base, austenitic precipitation-hardenable alloy. It has excellent strength and good resistance to corrosion and oxidation at temperatures at least to 1600 F. 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 low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ni-46. Producer or source: Cyclops Corporation. Originally published November 1958, revised March 1974.

ALLVAC WASPALOY, a nickel-base precipitation hardening alloy derives its high strength through the precipitation of gamma prime as a result of the aluminum and titanium additions and through the solid solution strengthening of other component elements. It is produced by vacuum induction melting followed by consummable vacuum are or electroslag remelting. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ni-404. Producer or source: Allvac Inc..

AEREX 350 is a bolt alloy with a combination high temperature creep strength, notch toughness, and thermal stability. It was designed for aerospace bolting applications. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and shear strength as well as fracture toughness, creep, and fatigue. It also includes information on high temperature performance. Filing Code: Ni-479. Producer or source: SPS Technologies.

ALLVAC 520 is a precipitation hardening nickel-base superalloy with good corrosion resistance and structural stability to about 1700 F (927 C). It has improved forgeability compared to ALLVAC 500 ZB (Alloy Digest Ni-380, March 1990). ALLVAC 520 is produced by vacuum induction melting followed by vacuum are remelting. 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 forming, heat treating, machining, and joining. Filing Code: Ni-384. Producer or source: Allvac Inc..

Aubert & Duval AD730 (NiCr16Co9Mo3W3Ti3Al2 alloy) is a cast and wrought nickel-based superalloy that withstands high temperatures (up to 750 °C, or 1380 °F) while preserving strength, creep, and fatigue resistance at a competitive cost. The breakthroughmainly comes from its unique properties-versus-cost balance, due to its recycling and forging ability. 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: Ni-782. Producer or source: Aubert & Duval S.A.

ALLVAC I-700 is a nickel-base alloy solid-solution strengthened by appreciable additions of cobalt, chromium and molybdenum. It is precipitation hardenable by virtue of aluminum and titanium additions. It is produced by vacuum induction melting followed by vacuum are remelting. 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: Ni-377. Producer or source: Allvac Inc..

Land-based turbines need to operate at high temperatures if they are to generate electricity efficiently and with fewer greenhouse gas emissions. Toward this end, alloy producers are developing nickel-base superalloys that will withstand the demanding operating conditions inside these units. The advanced, wrought, gamma-prime strengthened superalloy Haynes 282 could also potentially be used in aircraft manufacturing and other highperformance, high-temperature environments. The alloy contains 58% Ni, 19% Cr, 10% Co, 8.5% Mo, 1.5% Al, and 2.1% Ti. 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-637. Producer or source: Haynes International Inc.

Allvac 718Plus alloy is a variant of alloy 718 (Alloy Digest Ni-90, April 1964) made by adding new elements and adjusting others. The triple melting produces a stronger alloy with consistent properties in strength, stability, and forgeability. This datasheet provides information on composition, physical properties, and tensile properties. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Ni-647. Producer or source: Allvac, an Allegheny Technologies Company.

UGI KC35N is a nonmagnetic nickel-cobalt-chromium-molybdenum alloy with a fully austenitic structure. This datasheet provides information on composition, physical properties, elasticity, and shear strength. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Co-124. Producer or source: Schmolz + Bickenbach USA Inc..

CarTech MP35N is a wrought Co-Ni-Cr-Mo alloy that possesses a unique combination of ultra-high tensile strength (up to 2070 MPa, or 300 ksi), good ductility and toughness, and excellent corrosion resistance. The unique properties of CarTech MP35N are developed through work hardening, phase transformation, and aging. If the alloy is used in the fully work hardened condition, service temperatures up to 400 °C (750 °F) are suggested. This datasheet provides information on composition, physical properties, hardness, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Co-134. Producer or source: Carpenter Technology Corporation.

SPS Technologies Aerex 350 is a proprietary high-strength, corrosion-resistant nickel-based superalloy that is suitable for demanding applications up to 730 °C (1350 °F). It has the highest temperature limit of the three SPS superalloys. Like MP35N and MP159, this alloy not only undergoes the multiphase reaction, but also benefits from two additional strengthening mechanisms. Elements are also added to the chemical composition to cause precipitation of the gamma prime phase with higher temperature capability than MP159. Because this alloy is used at even higher temperatures than MP159, elements are added to the chemical composition to also cause the precipitation of eta phase during thermal treatments. This phase contributes to notch toughness at elevated temperatures. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on corrosion resistance. Filing Code: Ni-780. Producer or source: SPS Technologies, Inc.

MP159 Alloy is a member of the Multiphase family of alloys possessing the unique combination of ultra-high strength, ductility and corrosion resistance. This datasheet provides information on composition, physical properties, microstructure, elasticity, and shear strength as well as creep. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Co-68. Producer or source: Latrobe Steel Company. Originally published as Multiphase MP159 Alloy, May 1974, revised June 1990.

SPS Technologies MP35N is a multiphase cobalt-nickel alloy that possesses a unique combination of ultra-high strength, good ductility and toughness, outstanding corrosion resistance, and excellent cryogenic properties. It was the first fastener superalloy developed by SPS Technologies. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on corrosion resistance as well as heat treating, machining, and joining. Filing Code: Co-140. Producer or source: SPS Technologies, Inc.

CARPENTER MP35N alloy is a nickel/cobalt/chromium/molybdenum alloy with ultra-high strength, good ductility and toughness. It is highly resistant to corrosion including sulfidation, high-temperature oxidation and hydrogen embrittlement. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength 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, and joining. Filing Code: Co-82. Producer or source: Carpenter. Originally published October 1987, revised November 1991.