ATI Ti-5Al-2Sn-2Zr-4Cr-4Mo is known as Ti-17 alloy and is a beta-rich material for large aerospace components. 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, and joining. Filing Code: Ti-149. Producer or source: ATI Allvac.

Carpenter Touralloy 230 Plus stainless was originally developed for high-strength aerospace components, however, it may provide improved bar cycle fatigue durability, compared to other traditional golf face plate alloys. 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 joining. Filing Code: SS-1084. Producer or source: Carpenter Specialty Alloys.

Ferrium C69 is a case/core steel with a case hardness of 69 HRC and a core hardness of 50 HRC. It is used in racing applications, where rolling contact fatigue is an issue, and will be undergoing testing by the National Aeronautics and Space Administration (NASA) for aerospace gear applications. This datasheet provides information on hardness, and tensile properties as well as fatigue. It also includes information on forming and heat treating. Filing Code: SA-553. Producer or source: QuesTek Innovations, LLC.

Rotelloy 3 has the same composition as Permandur 49 and was specifically developed for aircraft generator rotor and stator laminations. In addition to a slightly improved magnetic performance, this grade is supplied with guaranteed minimum mechanical properties. This alloy complies with requirements of ASTM A 801. It is available in strip form only. This datasheet provides information on composition, physical properties, and tensile properties. It also includes information on machining. Filing Code: FE-128. Producer or source: Carpenter Technology Corporation.

Carpenter Stainless Type 304HN is the high-nitrogen version of Type 304 and 304H stainless steels. Interstitial strengthening with both carbon and nitrogen provides this alloy with significantly higher yield and tensile strength as annealed. Typical applications include aerospace and power components, as well as marine shafting. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: SS-763. Producer or source: Carpenter. See also Alloy Digest SS-368, October 1979.

LESCALLOY 300M VAC ARC is a low-alloy steel with an excellent combination of high hardenability and high strength coupled with good ductility and good toughness. Its tensile strength ranges from 280,000 to 300,000 psi. It is produced by the vacuum consumable electrode melting process to provide optimum cleanliness and preferred ingot structure. Its applications include aircraft components, pressure vessels and fasteners. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness. It also includes information on forming, heat treating, machining, joining, and surface treatment. Filing Code: SA-321. Producer or source: Latrobe Steel Company. Originally published March 1976, revised February 1993.

UNS No. A02060 is an aluminum-mold casting alloy that responds to an age-hardening heat treatment. It is recommended for applications that require a combination of high tensile properties and good machinability. Among its many uses are fuel pump bodies, aircraft fittings and seat frames for railway passenger cars. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well as fatigue. It also includes information on high temperature performance as well as casting, heat treating, machining, and joining. Filing Code: Al-285. Producer or source: Various aluminum companies.

RMI 6AI-4V is an alpha-beta type of titanium-base alloy that can be strengthened by age hardening. In the mill-annealed condition it has a guaranteed minimum room-temperature yield strength of 120,000 psi and this can be increased to as much as 160,000 psi by solution treating and aging. This alloy is tough and has attractive elevated-temperature properties. It is used widely for applications at temperatures up to 800 F. Typical applications are parts for jet engines, aircraft components and pressure vessels. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and bend 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, joining, and surface treatment. Filing Code: Ti-88. Producer or source: RMI Company.

AL TECH POTOMAC A has well-balanced strength and toughness which make it especially suitable for a wide variety of hot-die steel applications, including those involving severe coolants. Its outstanding mechanical properties make it useful for many non-tooling requirements such as aerospace components. For more specialized needs, the manufacturer offers special melting processes that enhance this steel's fatigue properties and transverse tensile ductility. This datasheet provides information on composition, physical properties, microstructure, hardness, elasticity, and tensile properties as well as fracture toughness. It also includes information on high temperature performance as well as forming, heat treating, and machining. Filing Code: TS-478. Producer or source: AL Tech Specialty Steel Corporation.

BRUSH WELLMAN SR-200E is a grade of beryllium strengthened by a dispersion of beryllium oxide (2.0%). It has relatively high strength and ductility (a minimum of 10% elongation). Its uses include missiles, space vehicles, structural parts on both commercial and military satellites and optical support benches. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Be-5. Producer or source: Brush Wellman Inc..

APEX TERNALLOY 7 is one of a family of three APEX TERNALLOYS; see also APEX TERNALLOY 5 (Alloy Digest A1-273, revised March 1987) and APEX TERNALLOY 6 (Alloy Digest A1-277, February 1987). It can be hardened by aging at room temperature without a solution treatment and offers high mechanical properties. It has good castability, excellent machinability and high resistance to corrosion. TERNALLOY 7 has many uses including aircraft components, gears machinery parts, fittings, valves and ornamental products. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as casting, heat treating, machining, joining, and surface treatment. Filing Code: Al-279. Producer or source: Apex International Alloys Inc..

APEX TERNALLOY 6 is one of a family of three APEX aluminum casting alloys (See APEX TERNALLOY 5, A1-273, November 1986.). It can be hardened by aging at room temperature and offers high mechanical properties. It has good castability, excellent machinability and high resistance to corrosion. Its many uses include aircraft components, gears, machinery parts, fittings, valves and ornamental products. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as casting, heat treating, machining, joining, and surface treatment. Filing Code: Al-277. Producer or source: Apex International Alloys Inc..

UNS No. A03560 is a heat-treatable aluminum casting alloy. Normally it is used only when heat-treated (aged) strengths are required. It is recommended for high-strength, pressure-tight castings, intricate shapes and where good resistance to corrosion is needed. Its many applications include crank cases, gear cases, oil pans, airframe fittings and instrument housings. 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 casting, heat treating, machining, and joining. Filing Code: Al-274. Producer or source: Various aluminum companies.

ENPLATE NI-423 is a nickel-phosphorus alloy deposited by chemical reduction without electric current. It is deposited by a stable, relatively high-speed functional electroless nickel process that produces a low-stress coating with good ductility and excellent resistance to corrosion. Its many uses include equipment for chemicals and food, aerospace components, molds and electronic devices. This datasheet provides information on composition, physical properties, and hardness. It also includes information on corrosion and wear resistance as well as heat treating, machining, joining, and surface treatment. Filing Code: Ni-343. Producer or source: Enthone Inc..

ALUMINUM 296.0 is an aluminum permanent-mold casting alloy that is recommended for applications requiring a combination of good machinability and high tensile properties. It can be age hardened by heat treatment. Among its uses are aerospace fittings and parts, compressor connecting rods and bodies for fuel pumps. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well as fatigue. It also includes information on high temperature performance as well as casting, heat treating, machining, and joining. Filing Code: Al-261. Producer or source: Various aluminum companies. See also Alloy Digest Al-241, November 1982.

ALUMINUM 707.0 is an aluminum-base foundry alloy that can be hardened by aging at room temperature without a solution treatment. It offers good strength in the cast-and-aged condition. It has relatively good castability, excellent machinability and high resistance to corrosion. Its many uses include aircraft and aerospace components, gears, machinery parts, manifolds, valves and fittings. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Al-260. Producer or source: Various aluminum companies.

ALUMINUM 705.0 is an aluminum-zinc-magnesium-manganese-chromium casting alloy that is hardened by aging at room temperature. It offers high mechanical properties in the cast-and-aged condition. It has good castability and high resistance to corrosion. Among its many users are high-pressure oxygen valves, aerospace components, gears, fittings and washing machine agitators. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as casting, heat treating, and machining. Filing Code: Al-259. Producer or source: Various aluminum companies.

SAE 4820 is a low-carbon (nominally 0.20%) carburizing steel containing nominally 3.5% nickel and 0.25% molybdenum. It is deal for used that require a strong, tough core along with a highly wear-resistant carburized case. In addition, it offers a good combination of strength and low-temperature toughness for non-carburized applications. It is recommended for a wide range of moderately heavy-duty applications. Among its many uses are carburized gears, carburized aerospace components and non-carburized machinery parts. 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, machining, and joining. Filing Code: SA-409. Producer or source: Alloy steel mills and foundries.

ALUMINUM A356.0 is a sand and permanent-mold casting alloy. It responds to an age-hardening heat treatment. This alloy has a relatively good combination of strength and ductility in the solution-treated and aged condition. Aluminum A356.0 is recommended for aircraft and missile components where high strength and resistance to corrosion are required. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well as fatigue. It also includes information on corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Al-258. Producer or source: Various aluminum companies.

UNILOY 13-8 has high strength, ductility and toughness in large cross sections in both longitudinal and transverse directions. The alloy has excellent mechanical property uniformity; this is the result of a well-balanced chemical composition. Because of its excellent general corrosion resistance (nearly equal to AISI Type 304 stainless steel) and its high degree of resistance to stress-corrosion cracking, it is used in a variety of environments. Typical uses are aircraft structural components, shafts, valve parts and fittings. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness. 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-457. Producer or source: Cytemp Cyclops.