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Amatrium Materials AI
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
  
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