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R58150 Titanium vs. ASTM B817 Type I

Both R58150 titanium and ASTM B817 type I are titanium alloys. They have 85% of their average alloy composition in common. There are 26 material properties with values for both materials. Properties with values for just one material (5, in this case) are not shown.

For each property being compared, the top bar is R58150 titanium and the bottom bar is ASTM B817 type I.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
100
Elongation at Break, % 13
4.0 to 13
Fatigue Strength, MPa 330
360 to 520
Poisson's Ratio 0.32
0.32
Reduction in Area, % 68
5.0 to 29
Shear Modulus, GPa 52
40
Tensile Strength: Ultimate (UTS), MPa 770
770 to 960
Tensile Strength: Yield (Proof), MPa 550
700 to 860

Thermal Properties

Latent Heat of Fusion, J/g 410
410
Maximum Temperature: Mechanical, °C 320
340
Melting Completion (Liquidus), °C 1760
1600
Melting Onset (Solidus), °C 1700
1550
Specific Heat Capacity, J/kg-K 500
560
Thermal Expansion, µm/m-K 8.4
9.6

Otherwise Unclassified Properties

Base Metal Price, % relative 48
36
Density, g/cm3 5.4
4.4
Embodied Carbon, kg CO2/kg material 31
38
Embodied Energy, MJ/kg 480
610
Embodied Water, L/kg 150
200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
30 to 120
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
2310 to 3540
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 32
35
Strength to Weight: Axial, points 40
48 to 60
Strength to Weight: Bending, points 35
42 to 49
Thermal Shock Resistance, points 48
54 to 68

Alloy Composition

Aluminum (Al), % 0
5.5 to 6.8
Carbon (C), % 0 to 0.1
0 to 0.1
Chlorine (Cl), % 0
0 to 0.2
Hydrogen (H), % 0 to 0.015
0 to 0.015
Iron (Fe), % 0 to 0.1
0 to 0.4
Molybdenum (Mo), % 14 to 16
0
Nitrogen (N), % 0 to 0.050
0 to 0.040
Oxygen (O), % 0 to 0.2
0 to 0.3
Silicon (Si), % 0
0 to 0.1
Sodium (Na), % 0
0 to 0.2
Titanium (Ti), % 83.5 to 86
87 to 91
Vanadium (V), % 0
3.5 to 4.5
Residuals, % 0
0 to 0.4