Titanium Ti-6Al-6V-2Sn (Ti-6-6-2) STA 870°C/565°C
Subcategory: Titanium Alloy; Nonferrous Metal; Alpha/Beta Titanium Alloy
Close Analogs: 2 other heat treatments of this alloy are listed in MatWeb.
Key Words: Ti-662; Ti-6-6-2; UNS R56620
Material Notes: Information provided by Allvac and the references. Solution Treated 870ºC, Aged 565ºC. Alpha-Beta alloy. Applications: Airframes, jet engines, rocket engine cases, nuclear reactor components, ordnance components.
Available Properties |
- Density
- Hardness, Brinell
- Hardness, Knoop
- Hardness, Rockwell C
- Hardness, Vickers
- Tensile Strength, Ultimate
- Tensile Strength, Yield
- Elongation at Break
- Modulus of Elasticity
- Poissons Ratio
- Fatigue Strength
- Fracture Toughness
- Shear Modulus
- Electrical Resistivity
- CTE, linear 20°C
- CTE, linear 250°C
- CTE, linear 500°C
- Specific Heat Capacity
- Thermal Conductivity
- Melting Point
- Solidus
- Liquidus
- Maximum Service Temperature, Air
- Beta Transus
|
|
|
|
Property Data |
This page displays only the text
of a material data sheet.
To see MatWeb's complete data
sheet for this material (including
material property data, metal
compositions, material suppliers,
etc), please click the button below. |
|
|
|
|