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R58150 Titanium vs. 2025 Aluminum

R58150 titanium belongs to the titanium alloys classification, while 2025 aluminum belongs to the aluminum alloys. There are 26 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 2025 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
72
Elongation at Break, % 13
15
Fatigue Strength, MPa 330
130
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 52
27
Shear Strength, MPa 470
240
Tensile Strength: Ultimate (UTS), MPa 770
400
Tensile Strength: Yield (Proof), MPa 550
260

Thermal Properties

Latent Heat of Fusion, J/g 410
400
Maximum Temperature: Mechanical, °C 320
190
Melting Completion (Liquidus), °C 1760
640
Melting Onset (Solidus), °C 1700
520
Specific Heat Capacity, J/kg-K 500
870
Thermal Expansion, µm/m-K 8.4
23

Otherwise Unclassified Properties

Base Metal Price, % relative 48
10
Density, g/cm3 5.4
3.0
Embodied Carbon, kg CO2/kg material 31
7.9
Embodied Energy, MJ/kg 480
150
Embodied Water, L/kg 150
1130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
55
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
450
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 32
46
Strength to Weight: Axial, points 40
37
Strength to Weight: Bending, points 35
40
Thermal Shock Resistance, points 48
18

Alloy Composition


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Aluminum (Al), % 0
90.9 to 95.2
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 0
0 to 0.1
Copper (Cu), % 0
3.9 to 5.0
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 1.0
Magnesium (Mg), % 0
0 to 0.050
Manganese (Mn), % 0
0.4 to 1.2
Molybdenum (Mo), % 14 to 16
0
Nitrogen (N), % 0 to 0.050
0
Oxygen (O), % 0 to 0.2
0
Silicon (Si), % 0
0.5 to 1.2
Titanium (Ti), % 83.5 to 86
0 to 0.15
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15