NICROBRAZ 171 is a base filler metal with extra high strength at temperature. It is good for brazing base metals containing cobalt, tungsten, and molybdenum and has a better flow characteristic than Nicrobraz 170 (Alloy Digest Ni-476, January 1995). This datasheet provides information on composition, physical properties, and hardness. It also includes information on corrosion resistance as well as joining. Filing Code: Ni-478. Producer or source: Wall Colmonoy Corporation.

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.

WESTINGHOUSE W545 is a heat treatable iron-base alloy having good high temperature strength and oxidation resistance. It is corrosion and heat resistant. Temperature range of principal usage is 1100 F. to 1350 F. Made by Consumable Electrode Vacuum Arc Melting Only. 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: SS-87. Producer or source: Midvale-Heppenstall Company.

PYROMET 751 is an age-hardenable nickel-base alloy with good stress-rupture properties to 1600 F. Its creep rate is low under high stresses at 1200-1500 F. It is highly resistant to chemical corrosion and oxidation. 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, joining, and surface treatment. Filing Code: Ni-335. Producer or source: Carpenter Technology Corporation.

PYROMET X-751 is an age hardenable nickel-base alloy with good stress-rupture properties at 1600 F. It is highly resistant to chemical corrosion and oxidation. 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-190. Producer or source: Carpenter Technology Corporation.

PYROMET 90 is a precipitation-hardenable nickel-base alloy with high strength at high temperatures. It is highly resistant to oxidation, scaling, heat and corrosion. 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: Ni-192. Producer or source: Carpenter Technology Corporation.

TIMETAL 1100, a near alpha alloy, was developed for elevated temperature use around 1100 F (600 C). The alloy is to be used in the beta processed condition. The alloy offers the highest combination of strength, creep resistance, fracture toughness, and stability of any commercially available titanium alloy. This datasheet provides information on composition, physical properties, and tensile properties as well as creep and fatigue. It also includes information on high temperature performance as well as forming and heat treating. Filing Code: TI-104. Producer or source: Timet.

P/M RENE 95 is a high strength, high temperature alloy used for rotating jet turbine components. Supersolvus P/M Rene 95 provides even higher temperature creep and stress-rupture resistance than standard Rene 95. Both are available as-HIP performs. A typical application is a high pressure turbine disc. This datasheet provides information on composition and tensile properties as well as creep. It also includes information on high temperature performance as well as heat treating and powder metal forms. Filing Code: Ni-434. Producer or source: Crucible Compaction Metals.

HPM beryllium-nickel alloy is capable of achieving high strength through precipitation heat treatment with excellent spring characteristics at temperatures to 550 deg F. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on heat treating and joining. Filing Code: Ni-527. Producer or source: Hamilton Precision Metals Inc.

Unimach No. 1 is a 5% chromium hot work steel recommended for construction equipment operating in the temperature range of 400-1000 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 high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: TS-115. Producer or source: Cyclops Corporation.

NiMark I is a vacuum melted low-carbon alloy steel in which yield strengths in excess of 240,000 psi can be developed. It is readily weldable and exhibits good ductility at high strength levels. This datasheet provides information on composition, physical properties, hardness, and tensile properties. 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-177. Producer or source: Carpenter.

AISI No. 631 is chromium-nickel-aluminum precipitation hardening stainless steel recommended for aircraft, missile and jet engine parts. This datasheet provides information on composition, physical properties, hardness, 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, joining, and surface treatment. Filing Code: SS-168. Producer or source: Alloy steel mills and foundries.

NiMark II is a vacuum melted low-carbon alloy steel in which yield strength in excess of 250,000 psi can be developed. It is readily weldable and exhibits good ductility at high strength levels and excellent notch ductility. 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, joining, and surface treatment. Filing Code: SA-184. Producer or source: Carpenter.

PYROMET alloy 88 is an age hardenable nickel-base alloy with high strength good corrosion and oxidation resistance. It possesses low creep rate in the temperature range 1200-1500 F (650-820 C). Above 1500 F (820 C), the effect of age hardening is lost and the alloy is used in the annealed condition. 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, and machining. Filing Code: Ni-185. Producer or source: Carpenter Technology Corporation. Originally published February 1973, revised August 1989.

ARMCO 17-14 Cu-Mo is an austenitic stainless steel which responds favorably to an age-hardening heat treatment. It is recommended for highly stressed stainless steel parts requiring long service at temperatures up to 1500 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 high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: SS-68. Producer or source: Armco Inc., Eastern Steel Division.

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.

STOODY 4 is a cobalt-chromium-tungsten alloy with excellent high-temperature strength and excellent resistance to corrosion. This alloy derives its high-temperature strength from the high tungsten-to-carbon ratio which allows a large percentage of tungsten to remain in solid solution. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive strength. It also includes information on high temperature performance and corrosion resistance as well as heat treating, machining, and joining. Filing Code: Co-75. Producer or source: WRAP Division, Stoody Company.

CARPENTER 21-12N is an austenitic chromium-nickel stainless steel for valves. It offers excellent high-temperature strength and hardness as well as corrosion resistance to combustion products. This alloy contains 0.15-0.25% nitrogen for increased high-temperature strength. It is widely used as the head material in two piece exhaust valves for both diesel and gasoline engines. 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, and joining. Filing Code: SS-316. Producer or source: Carpenter.

Anviloy 1150 is tungsten-bearing sintered alloy of high density and high strength. It is a PM product and one of a series of alloys with densities 50% greater than that of lead. Anviloy 1150 is a material developed specifically for its high-temperature strength and excellent thermal conductivity. It is used to best advantage in place of lower-conductivity, high-temperature tool steels. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and bend strength as well as fracture toughness. It also includes information on high temperature performance and corrosion resistance as well as machining and joining. Filing Code: W-16. Producer or source: CMW Inc. Originally published February 1970, revised November 2000.

INCOLOY ALLOY 800HT has improved creep and rupture strength due to closely controlled aluminum + titanium and carbon contents. In mill processing it receives a high-temperature grain-coarsening anneal which further contributes to high-temperature strength. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and shear strength 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: SS-482. Producer or source: Inco Alloys International Inc..