Allegheny Ludlum AL 15-7 Alloy is a chromium-nickel-molybdenum-aluminum semi-austenitic stainless steel. It is heat treatable to high strength and it has a moderate level of corrosion resistance. It is available both as a conventionally melted product and as vacuum arc or electroslag refined material. 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: SS-496. Producer or source: Allegheny Ludlum Corporation.

17Cr-4Ni EZ is a precipitation hardening stainless steel offering engineers and designers a wide selection of strength and hardness levels. A simple one-step aging treatment provides end users a unique combination of strength, toughness, and corrosion resistance. 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, and joining. Filing Code: SS-551. Producer or source: AL Tech Specialty Steel Corporation.

Armco PH 15-7 Mo stainless steel is a Cr-Ni-Mo-Al semi-austenitic stainless steel. It is heat treatable to high strength and hardness, maintains good corrosion resistance, and undergoes minimal distortion from heat treatment. The alloy has applications in the aerospace and other industries where high strength at elevated temperatures is required. 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, and joining. Filing Code: SS-693. Producer or source: Armco Inc., Specialty Steels Division.

NICORROS AL is age-hardenable by virtue of the alloying additions of aluminum and titanium. The alloy shows excellent corrosion resistance over a wide range of conditions, including stress-corrosion cracking. The high mechanical properties can be used to 1200 F (650 C). 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: Ni-473. Producer or source: VDM Technologies Corporation.

UNITEMP 718 is a nickel-base austenitic precipitation-hardenable alloy for extended service at temperatures up to 1200 F. For short periods the alloy performs well to about 1300 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, joining, and surface treatment. Filing Code: Ni-201. Producer or source: Cyclops Corporation.

ENDURO 18-8STi is the titanium-type 304 stainless steel stabilized by titanium. It is not made sensitive to intergranular corrosion by heating within the carbide precipitation range. It is recommended for use at temperatures up to 1600 F. 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-149. Producer or source: Republic Steel Corporation.

UNILOY 15-5 can be annealed (solution treated) to produce a martensite-austenite mixture and then aged to various levels of hardness and strength. It offers a broad range of mechanical properties. It is consumable remelted to improve cleanliness and mechanical properties. Normally, bars are supplied solution-treated (Condition A), machined very near to the finished dimensions and then age hardened. The many applications of Uniloy 15-5 include valves and fittings, gears, shafting, springs, and bearings. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness. It also includes information on corrosion resistance as well as forming, heat treating, and machining. Filing Code: SS-434. Producer or source: Cyclops.

Nicrofer 5120 CoTi is a precipitation-hardening alloy developed by Rolls-Royce. The alloy has good oxidation resistance with excellent creep-rupture values. This datasheet provides information on composition, physical properties, and elasticity. It also includes information on forming, heat treating, machining, and joining. Filing Code: Ni-438. Producer or source: VDM Technologies Corporation.

MAR-M alloy 246 is a vacuum-cast nickel-base alloy combining precipitation hardening and solid solution strengthening. It has high rupture strength and adequate ductility in the recommended operating temperature range of 1200-1900 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 casting, heat treating, machining, joining, and surface treatment. Filing Code: Ni-134. Producer or source: Martin Metals Division.

Nicrofer 7016 TiNb is an austenitic age-hardening Ni-Cr-Fe alloy containing Ti, Nb, and Al. High tensile strength is combined with good weldability. This aerospace alloy finds applications in rocket exhaust heat exchangers, springs, bellows, and bolts. 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, machining, and joining. Filing Code: Ni-534. Producer or source: VDM Technologies Corporation.

AA 6063 is a precipitation hardenable alloy; the hardening constituent being Mg2Si. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength as well as 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: Al-320. Producer or source: Various aluminum companies.

ARMCO 15-5 PH VAC CE is a vacuum-arc, consumable-electrode remelted stainless steel that is precipitation hardenable to the stringent requirements demanded by the aerospace and nuclear industries. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: SS-204. Producer or source: Armco Advanced Materials Corporation. Originally published as ARMCO 15-5 PH, January 1968, revised November 1989.

ALUMINUM 7075 is a wrought precipitation-hardenable aluminum alloy having excellent mechanical properties, workability and response to heat treatment and refrigeration. (This alloy is covered under its previous designation, ALUMINUM 75S, in Alloy Digest Al-5, February 1953). This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength as well as 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: Al-179. Producer or source: Various aluminum companies.

PYROMET alloy 41, a precipitation hardening nickel-base alloy possesses high strength in the 1200/1800 F (649/986 C) temperature range 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-237. Producer or source: Carpenter Technology Corporation. Originally published December 1976, revised October 1991.

U.S.S. 18-8 Ti is an austenitic chromium nickel steel containing titanium. It is recommended for parts fabricated by welding which cannot be subsequently annealed. It is also recommended for parts to be used at temperatures between 800 and 1650 deg. F. 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-43. Producer or source: United States Steel Corporation.

Olin 170 (UNIS C17000) has a relatively high beryllium content compared to the whole class of beryllium coppers and has the ability to reach tensile strengths near 1380 MPa (200 ksi). This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on forming and heat treating. Filing Code: CU-615. Producer or source: Olin Brass.

Hiduminium RR.77 is a precipitation hardening aluminum alloy possessing specific strength properties equal to or exceeding those of high tensile steel alloys. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fatigue. It also includes information on forming, heat treating, machining, and joining. Filing Code: Al-26. Producer or source: High Duty Alloys Ltd.

NI-VEE TYPE E is a precipitation hardening leaded-nickel bearing bronze suitable for bearings and acid-resisting castings. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive strength as well as deformation. It also includes information on corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Cu-44. Producer or source: The International Nickel Company Inc..

AA 7075 is the outstanding alloy of the 7000 series heat-treatable wrought aluminum alloys. It is used for highly stressed parts. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive strength. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-309. Producer or source: Various aluminum companies.

Uranus 800 HT is a variant of a high chromium and nickel austenitic alloy that combines good corrosion and creep resistance. The alloy is solution annealed to produce a large grain size and remains stable, not being embrittled by the precipitation of sigma phase. 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 heat treating and joining. Filing Code: SS-655. Producer or source: Creusot-Marrel.