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R58150 Titanium vs. 8011A Aluminum

R58150 titanium belongs to the titanium alloys classification, while 8011A aluminum belongs to the aluminum alloys. There are 25 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 8011A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
69
Elongation at Break, % 13
1.7 to 28
Fatigue Strength, MPa 330
33 to 76
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 52
26
Tensile Strength: Ultimate (UTS), MPa 770
100 to 180
Tensile Strength: Yield (Proof), MPa 550
34 to 170

Thermal Properties

Latent Heat of Fusion, J/g 410
400
Maximum Temperature: Mechanical, °C 320
170
Melting Completion (Liquidus), °C 1760
650
Melting Onset (Solidus), °C 1700
630
Specific Heat Capacity, J/kg-K 500
900
Thermal Expansion, µm/m-K 8.4
23

Otherwise Unclassified Properties

Base Metal Price, % relative 48
9.0
Density, g/cm3 5.4
2.7
Embodied Carbon, kg CO2/kg material 31
8.2
Embodied Energy, MJ/kg 480
150
Embodied Water, L/kg 150
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
3.0 to 22
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
8.2 to 200
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 32
50
Strength to Weight: Axial, points 40
11 to 18
Strength to Weight: Bending, points 35
18 to 26
Thermal Shock Resistance, points 48
4.6 to 8.1

Alloy Composition

Aluminum (Al), % 0
97.5 to 99.1
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 0
0 to 0.1
Copper (Cu), % 0
0 to 0.1
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0.5 to 1.0
Magnesium (Mg), % 0
0 to 0.1
Manganese (Mn), % 0
0 to 0.1
Molybdenum (Mo), % 14 to 16
0
Nitrogen (N), % 0 to 0.050
0
Oxygen (O), % 0 to 0.2
0
Silicon (Si), % 0
0.4 to 0.8
Titanium (Ti), % 83.5 to 86
0 to 0.050
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15