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852.0 Aluminum vs. R58150 Titanium

852.0 aluminum belongs to the aluminum alloys classification, while R58150 titanium belongs to the titanium 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 852.0 aluminum and the bottom bar is R58150 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition

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