NJZ ALLOY No. 25 is a zinc-copper-titanium alloy that offers outstanding high creep resistance and a low coefficient of expansion. It can be severely work hardened. Its applications include architectural building products, sporting equipment components, hardware and automotive trim. 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 casting, forming, heat treating, machining, and joining. Filing Code: Zn-22. Producer or source: New Jersey Zinc Company.

NJZ Alloy No. 45 is a zinc-copper alloy characterized by high hardness and strength, good ductility and high stiffness. It work hardens easily. Among its many applications are hardware, sporting-equipment components, cable wrappings and watch cases. This datasheet provides information on composition, physical properties, hardness, and tensile properties as well as creep and fatigue. It also includes information on corrosion resistance as well as casting, forming, heat treating, machining, and joining. Filing Code: Zn-25. Producer or source: New Jersey Zinc Company.

NJZ ALLOY No. 15 is a high-strength alloy with high stiffness and limited bending characteristics. It is produced from high-grade zinc base with additions of lead, copper, cadmium and magnesium. It can be severely work hardened and its applications include weather-stripping and hardware. This datasheet provides information on composition, physical properties, hardness, and tensile properties as well as creep and fatigue. It also includes information on corrosion resistance as well as casting, forming, heat treating, machining, and joining. Filing Code: Zn-21. Producer or source: New Jersey Zinc Company.

ALLEGHENY ALMAR-362 is an age-hardenable martensitic stainless steel recommended for applications requiring high strength and good corrosion resistance, such as aircraft and missile structures, hydraulic and pneumatic equipment components, and in the chemical processing industry. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive strength as well as fracture toughness. It also includes information on corrosion resistance as well as casting, forming, heat treating, machining, joining, and surface treatment. Filing Code: SS-234. Producer or source: Allegheny Ludlum Corporation.

ALUMINUM 535.0 is a high-purity aluminum alloy of the aluminum-magnesium type. It possesses a high and stable combination of strength, shock resistance and ductility in the cast condition. Among its many applications are armament, hardware, cooking utensils, highway trailers, textile machinery and marine components. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength as well as fatigue. It also includes information on high temperature performance and corrosion resistance as well as casting, forming, heat treating, machining, and surface treatment. Filing Code: Al-254. Producer or source: Various aluminum companies.

Timetal 6-4 and its variations are general-purpose, widely used alpha-beta titanium alloys. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and shear strength as well as creep and fatigue. It also includes information on forming and joining. Filing Code: TI-143. Producer or source: Timet.

Ferrium S53 was developed for use as a structural stainless steel for aircraft landing gear. S53 has a corrosion resistance equivalent to 15-5PH H900, strength equivalent to or better than 300M (AMS 6257A) and SAE 4340 (see Mechanical Properties), optimum microstructure features for maximum fatigue resistance, and a surface hardenability equal to or greater than 67 HRC for wear and fatigue. Please see updated designation and information on this alloy in Alloy Digest SA-589, December 2008. This datasheet provides information on composition, physical properties, hardness, 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-942. Producer or source: QuesTek Innovations, LLC. Originally published October 2005, revised June 2008, updated December 2008.

Carpenter titanium alloy 6Al-4V is an alpha-beta alloy that contains alpha and beta stabilizers and can be heat treated. This alloy accounts for more than 50% of total titanium usage, mostly in aerospace applications. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive, shear, and bearing strength as well as fracture toughness 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-60. Producer or source: Carpenter Technology Corporation. Originally published as Carpenter Titanium 6-4, October 1970, revised August 2002.