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.

aerospace application, chemical composition, corrosion-resistant alloys, creep strength, elasticity, heat treatability, high-temperature alloys, oxidation resistance, physical properties, tensile properties, TIMETAL 21S, weldability, workability, thermal properties
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Copyright © ASM International® 1998
1998
ASM International
Topics
Air and spacecraft Corrosion-resistant alloys High-temperature alloys Beta and near-beta titanium alloys Chemical composition Oxidation resistance Heat treatability Weldability Workability Elastic modulus Tensile properties Creep strength Physical properties Thermal properties
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