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R58150 Titanium vs. 4015 Aluminum

R58150 titanium belongs to the titanium alloys classification, while 4015 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 4015 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
70
Elongation at Break, % 13
1.1 to 23
Fatigue Strength, MPa 330
46 to 71
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 52
26
Shear Strength, MPa 470
82 to 120
Tensile Strength: Ultimate (UTS), MPa 770
130 to 220
Tensile Strength: Yield (Proof), MPa 550
50 to 200

Thermal Properties

Latent Heat of Fusion, J/g 410
420
Maximum Temperature: Mechanical, °C 320
160
Melting Completion (Liquidus), °C 1760
640
Melting Onset (Solidus), °C 1700
600
Specific Heat Capacity, J/kg-K 500
900
Thermal Expansion, µm/m-K 8.4
23

Otherwise Unclassified Properties

Base Metal Price, % relative 48
9.5
Density, g/cm3 5.4
2.7
Embodied Carbon, kg CO2/kg material 31
8.1
Embodied Energy, MJ/kg 480
150
Embodied Water, L/kg 150
1160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
2.4 to 24
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
18 to 290
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 32
50
Strength to Weight: Axial, points 40
13 to 22
Strength to Weight: Bending, points 35
21 to 30
Thermal Shock Resistance, points 48
5.7 to 9.7

Alloy Composition

Aluminum (Al), % 0
94.9 to 97.9
Carbon (C), % 0 to 0.1
0
Copper (Cu), % 0
0 to 0.2
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 0.7
Magnesium (Mg), % 0
0.1 to 0.5
Manganese (Mn), % 0
0.6 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
1.4 to 2.2
Titanium (Ti), % 83.5 to 86
0
Zinc (Zn), % 0
0 to 0.2
Residuals, % 0
0 to 0.15