TIMET TIMETAL® 17 Titanium Alloy (Ti-5Al-2Sn-4Mo-2Zr-6Mo); STA

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TIMET TIMETAL® 17 Titanium Alloy (Ti-5Al-2Sn-4Mo-2Zr-6Mo); STA
Categories:	Metal; Nonferrous Metal; Titanium Alloy; Alpha/Beta Titanium Alloy
Material Notes:	High strength, deep hardenable forging near-beta alloy primarily for jet engines. Allows heat treatment to a variety of strength levels in sections up to 6 inches. Offers good ductility and toughness, as well as good low cycle and high cycle fatigue properties. Typical heat treatment: Solution treat 1475°F for 4 hr and water quench. Age 1175°F for 8 hr and air cool. Data provided by TIMET.
Key Words:	UNS R52252
Vendors:

Available Properties

Density
Tensile Strength, Ultimate
Tensile Strength, Ultimate
Tensile Strength, Ultimate
Tensile Strength, Ultimate
Tensile Strength, Ultimate
Tensile Strength, Yield
Tensile Strength, Yield
Tensile Strength, Yield
Tensile Strength, Yield
Tensile Strength, Yield
Elongation at Break
Elongation at Break
Elongation at Break
Elongation at Break
Elongation at Break
Reduction of Area
Reduction of Area
Reduction of Area
Reduction of Area
Reduction of Area
Creep Strength, 0.2% creep
Creep Strength, 0.2% creep
Creep Strength, 0.2% creep
Creep Strength, 0.2% creep
Creep Strength, 0.2% creep
Creep Strength, 0.2% creep
Rupture Strength
Rupture Strength
Rupture Strength
Rupture Strength
Rupture Strength
Rupture Strength
Rupture Strength
Modulus of Elasticity
Notched Tensile Strength
Notched Tensile Strength
Notched Tensile Strength
Notched Tensile Strength
Notched Tensile Strength
Fatigue Strength, Maximum Stress (Load Control A = 0.95)
Fatigue Strength, Maximum Stress (Load Control A = 0.95)
Fatigue Strength, Maximum Stress (Load Control A = 0.95)
Fatigue Strength, Maximum Stress (Load Control A = 0.95)
Fatigue Strength, Maximum Stress (Load Control A = 0.95)
Fatigue Strength, Maximum Stress (Load Control A = 0.95)
Fatigue Strength, Maximum Stress (Load Control A = 0.95)
Fracture Toughness, Yield Strength = 1158 MPa (168 ksi)
Fracture Toughness, Yield Strength = 1054 MPa (153 ksi)
Fracture Toughness, Yield Strength = 1110 MPa (161 ksi)
Beta Transus
Solution Temperature
Aging Temperature
Aluminum, Al
Chromium, Cr
Molybdenum, Mo
Other, each
Other, total
Tin, Sn
Titanium, Ti, Calculated as remainder
Zirconium, Zr

Property Data

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