KEVLAR/J-2 is an advanced thermoplastic composite material based on J-2 copolymer reinforced with continuous KEVLAR fiber. The inherent fiber/matrix compatibility of this composite provides attractive mechanical properties. This datasheet provides information on physical properties, tensile properties, and compressive and shear strength. It also includes information on corrosion resistance. Filing Code: Cp-14. Producer or source: E. I. Dupont de Nemours & Company Inc..

The Al-2wt.%Cu matrix composite contains 60 vol.% alumina. The aluminum ceramic fiber is Nextel 610, which affects the longitudinal direction, resulting in a high longitudinal specific modulus and a specific strength with good off-axis properties. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive and shear strength as well as fatigue. It also includes information on corrosion resistance. Filing Code: AL-345. Producer or source: 3M.

This pure aluminum matrix composite contains 60 volume% alumina. The aluminum ceramic fiber is Nextel 610. The fiber effects the longitudinal direction, resulting in a high longitudinal specific modulus and a specific strength with good off-axis properties. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive and shear strength. It also includes information on corrosion resistance as well as casting. Filing Code: AL-344. Producer or source: 3M.

METCO 505 is a high-molybdenum powder designed to produce plasma flame spray coatings for use as hard bearing surfaces with low coefficient of friction and for resisting wear by abrasive grains or hard surfaces. Its coatings have excellent non-scuffing properties and are compatible with many mating materials, particularly cast iron and iron-base alloys. This datasheet provides information on composition, physical properties, hardness, and tensile properties. It also includes information on corrosion resistance as well as surface treatment. Filing Code: Mo-12. Producer or source: Metco Inc..

AUSTEMPERED DUCTILE IRON has high strength with excellent toughness and ductility. Its strength is twice that of conventional ductile irons, comparable to heat-treated wrought steels. Composition is balanced to provide foundry compatibility, minimal segregation and good response to austempering. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness. It also includes information on heat treating and machining. Filing Code: CI-53. Producer or source: AMAX.

TRISTELLE ALLOY TS-1 is a 30Cr-10Ni-12Co alloy developed to withstand both corrosion and galling. This alloy relies on the formation of chromium-rich carbides during solidification. It is the lowest in carbon of the Tristelle Family. The alloy is recommended for valve services. This datasheet provides information on composition, physical properties, and hardness as well as fracture toughness. It also includes information on corrosion and wear resistance as well as joining. Filing Code: SS-662. Producer or source: Stoody Deloro Stellite Inc.

TIMETAL 21S (Ti-15%Mo-3%Nb-3%Al-0.2Si) offers the good cold formability and weldability of a beta strip alloy, but with greatly improved oxidation resistance and creep strength. Aerospace applications include engine exhaust plug and nozzle assemblies. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on high temperature performance and corrosion resistance as well as forming and heat treating. Filing Code: TI-105. Producer or source: Titanium Metals Corporation (Timet). Originally published March 1993, revised October 1998.

Tristelle alloy TS-2 is an alloy of 35Cr-10Ni-12Co developed to withstand both corrosion and galling. This alloy relies on the formation of chromium-rich carbides during solidification. It is the intermediate carbon content alloy in this family, (See TS-1, Alloy Digest SS-662, December 1996, and TS-3, Alloy Digest SS-672, January 1997) and is recommended for valve service. This datasheet provides information on composition, physical properties, and hardness as well as fracture toughness. It also includes information on corrosion and wear resistance as well as joining. Filing Code: SS-668. Producer or source: Stoody Deloro Stellite Inc.

DURIMET 20 is a special austenitic stainless steel alloy of nickel, chromium, molybdenum, and copper. It is highly resistant to hot and cold strong acids and is supplied in the form of castings to the grade CN7M. This datasheet provides information on composition, physical properties, and elasticity. It also includes information on corrosion resistance as well as heat treating, machining, and joining. Filing Code: SS-5. Producer or source: The Duriron Company Inc. Originally published January 1953, revised March 1962, March 1996.

TYPE HX is a nickel-base austenitic casting, similar to HW (See Alloy Digest Ni-449, April 1994), but containing more nickel and chromium, thus having better oxidation resistance. It is used in applications up to 1150 C (2100 F). 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 machining and joining. Filing Code: Ni-454. Producer or source: Steel Founders Society.

The CLIMAX 15-3 type alloys are martensitic white irons having an excellent combination of abrasion resistance and thoughness. For specific purposes, the use of four carbon ranges is recommended. These are: (1) Extra High Carbon (XHC), (2) High Carbon (HC), (3) Medium Carbon (MC), and (4) Low Carbon (LC). This datasheet provides information on composition, physical properties, hardness, and elasticity. It also includes information on wear resistance as well as casting, heat treating, machining, and joining. Filing Code: CI-43. Producer or source: Climax Molybdenum Company.

Superplast 300, also known as SP 300, is a prehardened steel for mold service. It is designed to provide improved weldability and machinability compared to conventional P20 steel. 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: TS-643. Producer or source: Industeel USA, LLC.

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.

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.

1008 and C8C are wrought low-carbon (carbon ≤ 0.10%) non-alloy steels that are used in the as-rolled, annealed, normalized, or cold worked condition. These steels are characterized by low strength, high ductility, excellent cold formability, and excellent weldability. Within the carbon range of these steel grades, strength and hardness will increase with increase in carbon and with cold work. Such increases in strength are at the sacrifice of ductility or the ability to withstand cold deformation. 1008 and C8C are widely used for lightly stressed parts where cold formability or drawability is the primary requisite. In general, they are not intended for heat treatment after cold working. 1008 may, however, be used in the carburized or carbonitrided, and subsequently quench hardened and tempered condition for parts requiring a hard, wear-resistant surface, but with little need for increased mechanical properties in the core. This datasheet provides information on composition, physical properties, microstructure, hardness, elasticity, and tensile properties as well as fatigue. It also includes information on corrosion resistance as well as casting, forming, heat treating, machining, and joining. Filing Code: CS-228. Producer or source: Data Survey.