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R58150 Titanium vs. 4145 Aluminum

R58150 titanium belongs to the titanium alloys classification, while 4145 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 4145 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
73
Elongation at Break, % 13
2.2
Fatigue Strength, MPa 330
48
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 52
28
Shear Strength, MPa 470
69
Tensile Strength: Ultimate (UTS), MPa 770
120
Tensile Strength: Yield (Proof), MPa 550
68

Thermal Properties

Latent Heat of Fusion, J/g 410
540
Maximum Temperature: Mechanical, °C 320
160
Melting Completion (Liquidus), °C 1760
590
Melting Onset (Solidus), °C 1700
520
Specific Heat Capacity, J/kg-K 500
880
Thermal Expansion, µm/m-K 8.4
21

Otherwise Unclassified Properties

Base Metal Price, % relative 48
10
Density, g/cm3 5.4
2.8
Embodied Carbon, kg CO2/kg material 31
7.6
Embodied Energy, MJ/kg 480
140
Embodied Water, L/kg 150
1040

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
2.3
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
31
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 32
50
Strength to Weight: Axial, points 40
12
Strength to Weight: Bending, points 35
19
Thermal Shock Resistance, points 48
5.5

Alloy Composition


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Aluminum (Al), % 0
83 to 87.4
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 0
0 to 0.15
Copper (Cu), % 0
3.3 to 4.7
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 0.8
Magnesium (Mg), % 0
0 to 0.15
Manganese (Mn), % 0
0 to 0.15
Molybdenum (Mo), % 14 to 16
0
Nitrogen (N), % 0 to 0.050
0
Oxygen (O), % 0 to 0.2
0
Silicon (Si), % 0
9.3 to 10.7
Titanium (Ti), % 83.5 to 86
0
Zinc (Zn), % 0
0 to 0.2
Residuals, % 0
0 to 0.15