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R58150 Titanium vs. 354.0 Aluminum

R58150 titanium belongs to the titanium alloys classification, while 354.0 aluminum belongs to the aluminum alloys. There are 25 material properties with values for both materials. Properties with values for just one material (6, in this case) are not shown.

For each property being compared, the top bar is R58150 titanium and the bottom bar is 354.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
71
Elongation at Break, % 13
2.4 to 3.0
Fatigue Strength, MPa 330
92 to 120
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 52
27
Tensile Strength: Ultimate (UTS), MPa 770
360 to 380
Tensile Strength: Yield (Proof), MPa 550
280 to 310

Thermal Properties

Latent Heat of Fusion, J/g 410
530
Maximum Temperature: Mechanical, °C 320
170
Melting Completion (Liquidus), °C 1760
600
Melting Onset (Solidus), °C 1700
550
Specific Heat Capacity, J/kg-K 500
900
Thermal Expansion, µm/m-K 8.4
21

Otherwise Unclassified Properties

Base Metal Price, % relative 48
9.5
Density, g/cm3 5.4
2.7
Embodied Carbon, kg CO2/kg material 31
7.8
Embodied Energy, MJ/kg 480
150
Embodied Water, L/kg 150
1070

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
8.6 to 9.8
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
540 to 670
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 32
52
Strength to Weight: Axial, points 40
37 to 39
Strength to Weight: Bending, points 35
42 to 44
Thermal Shock Resistance, points 48
17 to 18

Alloy Composition

Aluminum (Al), % 0
87.3 to 89.4
Carbon (C), % 0 to 0.1
0
Copper (Cu), % 0
1.6 to 2.0
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 0.2
Magnesium (Mg), % 0
0.4 to 0.6
Manganese (Mn), % 0
0 to 0.1
Molybdenum (Mo), % 14 to 16
0
Nitrogen (N), % 0 to 0.050
0
Oxygen (O), % 0 to 0.2
0
Silicon (Si), % 0
8.6 to 9.4
Titanium (Ti), % 83.5 to 86
0 to 0.2
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15