TIMET TIMETAL® 15-3 Titanium Alloy (Ti-15V-3Cr-3Sn-3Al); Aged at 538°C/8 hr.

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TIMET TIMETAL® 15-3 Titanium Alloy (Ti-15V-3Cr-3Sn-3Al); Aged at 538°C/8 hr.
Categories:	Metal; Nonferrous Metal; Titanium Alloy; Beta Titanium Alloy
Material Notes:	High-Strength, Cold Formable Strip Alloy Industry Specifications: USA Aerospace: AMS 4914A. Features: Cold formable and weldable, this strip alloy is primarily used for aircraft ducting, pressure vessels and other fabricated sheet metal structures up to 300°C. Mechanical property data reported Typical heat treatment for this alloy: Solution Treatment: 790°C for 3-20 min, air cool. Age Treatment: 480-620°C for 4-16 hrs. Data provided by TIMET.
Key Words:	15-3-3-3
Vendors:

Available Properties

Density, Typical
Tensile Strength, Ultimate, specified minimum
Tensile Strength, Ultimate, Typical
Tensile Strength, Ultimate
Tensile Strength, Ultimate
Tensile Strength, Ultimate
Tensile Strength, Ultimate
Tensile Strength, Ultimate
Tensile Strength, Ultimate
Tensile Strength, Yield, specified minimum
Tensile Strength, Yield, Typical
Tensile Strength, Yield
Tensile Strength, Yield
Tensile Strength, Yield
Tensile Strength, Yield
Tensile Strength, Yield
Tensile Strength, Yield
Elongation at Break, specified minimum
Elongation at Break, Typical
Elongation at Break
Elongation at Break
Elongation at Break
Elongation at Break
Elongation at Break
Elongation at Break
Modulus of Elasticity
Fatigue Strength, Limit; test specifics not reported
CTE, linear
CTE, linear
CTE, linear
CTE, linear
CTE, linear
CTE, linear
CTE, linear
Specific Heat Capacity
Specific Heat Capacity
Specific Heat Capacity
Specific Heat Capacity
Specific Heat Capacity
Thermal Conductivity
Thermal Conductivity
Thermal Conductivity
Thermal Conductivity
Thermal Conductivity
Maximum Service Temperature, Air
Beta Transus
Aluminum, Al
Carbon, C
Chromium, Cr
Hydrogen, H
Iron, Fe
Nitrogen, N
Other, each
Other, total
Oxygen, O
Tin, Sn
Titanium, Ti, Calculated as remainder
Vanadium, V

Property Data

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