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R58150 Titanium vs. Grade 20 Titanium

Both R58150 titanium and grade 20 titanium are titanium alloys. They have 78% of their average alloy composition in common. There are 26 material properties with values for both materials. Properties with values for just one material (1, in this case) are not shown.

For each property being compared, the top bar is R58150 titanium and the bottom bar is grade 20 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
120
Elongation at Break, % 13
5.7 to 17
Fatigue Strength, MPa 330
550 to 630
Poisson's Ratio 0.32
0.32
Reduction in Area, % 68
23
Shear Modulus, GPa 52
47
Shear Strength, MPa 470
560 to 740
Tensile Strength: Ultimate (UTS), MPa 770
900 to 1270
Tensile Strength: Yield (Proof), MPa 550
850 to 1190

Thermal Properties

Latent Heat of Fusion, J/g 410
400
Maximum Temperature: Mechanical, °C 320
370
Melting Completion (Liquidus), °C 1760
1660
Melting Onset (Solidus), °C 1700
1600
Specific Heat Capacity, J/kg-K 500
520
Thermal Expansion, µm/m-K 8.4
9.6

Otherwise Unclassified Properties

Density, g/cm3 5.4
5.0
Embodied Carbon, kg CO2/kg material 31
52
Embodied Energy, MJ/kg 480
860
Embodied Water, L/kg 150
350

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
71 to 150
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
2940 to 5760
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 32
33
Strength to Weight: Axial, points 40
50 to 70
Strength to Weight: Bending, points 35
41 to 52
Thermal Shock Resistance, points 48
55 to 77

Alloy Composition

Aluminum (Al), % 0
3.0 to 4.0
Carbon (C), % 0 to 0.1
0 to 0.050
Chromium (Cr), % 0
5.5 to 6.5
Hydrogen (H), % 0 to 0.015
0 to 0.020
Iron (Fe), % 0 to 0.1
0 to 0.3
Molybdenum (Mo), % 14 to 16
3.5 to 4.5
Nitrogen (N), % 0 to 0.050
0 to 0.030
Oxygen (O), % 0 to 0.2
0 to 0.12
Palladium (Pd), % 0
0.040 to 0.080
Titanium (Ti), % 83.5 to 86
71 to 77
Vanadium (V), % 0
7.5 to 8.5
Zirconium (Zr), % 0
3.5 to 4.5
Residuals, % 0
0 to 0.4