* Titanium Grade 6 *
Chemical composition (weight %) (Maximum values unless range is shown)
O
N
C
H
Fe
A1
V
Sn
Mo
Others
Residuals
0.20
0.05
0.08
0.02
0.50
4.0-6.0
2.0-3.0
0.4
An alloy for airframe and jet engine applications requiring good weldability, stability and strength at elevated temperatures.
Mechanical properties at room temperature
Minimum values
Typical values
Yield Strength
795 MPa
900 MPa
Ultimate Strength
825 MPa
970 MPa
Elongation in 50 mm, A5
10%
16%
Reduction in Area
25%
%
Hardness
330-350 HV
Modulus of elasticity
110 GPa
Charpy V-Notch Impact
14 J
