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R58150 Titanium vs. 2011A Aluminum

R58150 titanium belongs to the titanium alloys classification, while 2011A aluminum belongs to the aluminum alloys. There are 26 material properties with values for both materials. Properties with values for just one material (5, in this case) are not shown.

For each property being compared, the top bar is R58150 titanium and the bottom bar is 2011A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
70
Elongation at Break, % 13
6.8 to 16
Fatigue Strength, MPa 330
75 to 100
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 52
26
Shear Strength, MPa 470
190 to 250
Tensile Strength: Ultimate (UTS), MPa 770
310 to 410
Tensile Strength: Yield (Proof), MPa 550
140 to 310

Thermal Properties

Latent Heat of Fusion, J/g 410
390
Maximum Temperature: Mechanical, °C 320
190
Melting Completion (Liquidus), °C 1760
660
Melting Onset (Solidus), °C 1700
550
Specific Heat Capacity, J/kg-K 500
870
Thermal Expansion, µm/m-K 8.4
23

Otherwise Unclassified Properties

Base Metal Price, % relative 48
11
Density, g/cm3 5.4
3.1
Embodied Carbon, kg CO2/kg material 31
7.9
Embodied Energy, MJ/kg 480
150
Embodied Water, L/kg 150
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
20 to 40
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
140 to 670
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 32
44
Strength to Weight: Axial, points 40
28 to 37
Strength to Weight: Bending, points 35
33 to 40
Thermal Shock Resistance, points 48
14 to 18

Alloy Composition

Aluminum (Al), % 0
91.5 to 95.1
Bismuth (Bi), % 0
0.2 to 0.6
Carbon (C), % 0 to 0.1
0
Copper (Cu), % 0
4.5 to 6.0
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 0.5
Lead (Pb), % 0
0.2 to 0.6
Molybdenum (Mo), % 14 to 16
0
Nitrogen (N), % 0 to 0.050
0
Oxygen (O), % 0 to 0.2
0
Silicon (Si), % 0
0 to 0.4
Titanium (Ti), % 83.5 to 86
0
Zinc (Zn), % 0
0 to 0.3
Residuals, % 0
0 to 0.15