CABOT Ti-3A1-2.5V alloy is both lightweight and strong. It has a high strength-to-weight ratio which provides a major design advantage saving weight. It can be formed readily and it has good weldability. Seamless tubing of CABOT Ti-3A1-2.5V was developed for aircraft hydraulic and fuel systems and its performance has been proved by use in various types of aircraft and aerospace vehicles. CABOT Ti-3A1-2.5V is available as plate, sheet and seamless tubing and pipe. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on forming, heat treating, machining, and joining. Filing Code: Ti-85. Producer or source: Cabot Wrought Products.

ALUMINUM A206.0 is a high-strength aluminum casting alloy. It provides an optimum combination of strength, light weight and economy. Its performance approaches that of forged steel, yet it may be less expensive to use because its lower tooling costs often offset the price difference. In automotive applications, the lighter weight of A206.0 can save fuel and increase range. See also Aluminum A201, Alloy Digest Al-234, April 1979. This datasheet provides information on composition, physical properties, 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, joining, and surface treatment. Filing Code: Al-244. Producer or source: Various aluminum companies.

TIMETAL 15-3 is a metastable beta titanium alloy that offers substantial weight reductions over other engineering materials. In the solution treated condition, it has excellent cold formability; in the aged condition, it has high strength. TIMETAL 15-3 is usually acceptable for use at temperatures up to 550 F. This datasheet provides information on composition, physical properties, and tensile properties. It also includes information on forming and heat treating. Filing Code: Ti-101. Producer or source: Titanium Metals Corporation (Timet).

ATI 425 was originally developed for hot-rolled armor plate to provide ballistic protection comparable to Ti-6Al-4V and has been evaluated against a variety of projectile threats for use as armor. While processing the alloy for armor plate applications, it was observed that the material exhibited very good hot workability, permitting a more lenient window of processing parameters than necessary for Ti-6Al-4V. Versatility then expanded, and applications now exist in the chemical process industry (CPI) and in the aerospace industry. This datasheet provides information on composition, physical properties, and tensile properties as well as fracture toughness and fatigue. It also includes information on corrosion resistance. Filing Code: TI-133. Producer or source: ATI Wah Chang, Allegheny Technologies. Originally published March 2004, revised July 2004.

COLUMBIUM ALLOY SU-31 is a columbium-base alloy designed to operate at temperatures up to 1300 C (2372 F). This datasheet provides information on composition, physical properties, 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, and joining. Filing Code: Cb-18. Producer or source: Kawecki Berylco Industries Inc..

Kaiser Aluminum Alloy 2219 has good machinability and good mechanical properties. The alloy is typically used in high-temperature structural applications and is also used in high-strength weldments where postweld heat treatment can be employed. This datasheet provides information on composition, physical properties, hardness, and tensile properties as well as fatigue. It also includes information on corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: AL-358. Producer or source: Tennalum, A Division of Kaiser Aluminum.

Aluminum 7002 is a heat treatable, weldable, high strength aluminum alloy recommended for space equipment and cryogenic applications. 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 low temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-159. Producer or source: Aluminum Company of America.

CM 681 LC is a high-performance integral cast turbine wheel alloy. The alloy is an improvement over CM 247 LC and MAR M 247. This datasheet provides information on composition, physical properties, and tensile properties as well as creep. It also includes information on casting. Filing Code: Ni-636. Producer or source: Cannon-Muskegon Corporation.

HAYNES Alloy No. 188 is a cobalt-base alloy which has excellent high-temperature strength, outstanding oxidation resistance, and good post-aging ductility. It is recommended for aircraft engine components. (U.S. Pat. 3,418,111 This datasheet provides information on composition, physical properties, 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, and joining. Filing Code: Co-62. Producer or source: Stellite Division, Cabot Corporation.