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R58150 Titanium vs. 852.0 Aluminum

R58150 titanium belongs to the titanium alloys classification, while 852.0 aluminum belongs to the aluminum alloys. There are 26 material properties with values for both materials. Properties with values for just one material (7, in this case) are not shown.

For each property being compared, the top bar is R58150 titanium and the bottom bar is 852.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
70
Elongation at Break, % 13
3.4
Fatigue Strength, MPa 330
73
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 52
26
Shear Strength, MPa 470
130
Tensile Strength: Ultimate (UTS), MPa 770
200
Tensile Strength: Yield (Proof), MPa 550
150

Thermal Properties

Latent Heat of Fusion, J/g 410
370
Maximum Temperature: Mechanical, °C 320
190
Melting Completion (Liquidus), °C 1760
640
Melting Onset (Solidus), °C 1700
210
Specific Heat Capacity, J/kg-K 500
840
Thermal Expansion, µm/m-K 8.4
23

Otherwise Unclassified Properties

Base Metal Price, % relative 48
15
Density, g/cm3 5.4
3.2
Embodied Carbon, kg CO2/kg material 31
8.5
Embodied Energy, MJ/kg 480
160
Embodied Water, L/kg 150
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
6.2
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
160
Stiffness to Weight: Axial, points 14
12
Stiffness to Weight: Bending, points 32
43
Strength to Weight: Axial, points 40
17
Strength to Weight: Bending, points 35
24
Thermal Shock Resistance, points 48
8.7

Alloy Composition

Aluminum (Al), % 0
86.6 to 91.3
Carbon (C), % 0 to 0.1
0
Copper (Cu), % 0
1.7 to 2.3
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 0.7
Magnesium (Mg), % 0
0.6 to 0.9
Manganese (Mn), % 0
0 to 0.1
Molybdenum (Mo), % 14 to 16
0
Nickel (Ni), % 0
0.9 to 1.5
Nitrogen (N), % 0 to 0.050
0
Oxygen (O), % 0 to 0.2
0
Silicon (Si), % 0
0 to 0.4
Tin (Sn), % 0
5.5 to 7.0
Titanium (Ti), % 83.5 to 86
0 to 0.2
Residuals, % 0
0 to 0.3