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R58150 Titanium vs. EN AC-51100 Aluminum

R58150 titanium belongs to the titanium alloys classification, while EN AC-51100 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 EN AC-51100 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
68
Elongation at Break, % 13
4.5
Fatigue Strength, MPa 330
58
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 52
26
Tensile Strength: Ultimate (UTS), MPa 770
160
Tensile Strength: Yield (Proof), MPa 550
80

Thermal Properties

Latent Heat of Fusion, J/g 410
400
Maximum Temperature: Mechanical, °C 320
170
Melting Completion (Liquidus), °C 1760
640
Melting Onset (Solidus), °C 1700
620
Specific Heat Capacity, J/kg-K 500
900
Thermal Expansion, µm/m-K 8.4
23

Otherwise Unclassified Properties

Base Metal Price, % relative 48
9.5
Density, g/cm3 5.4
2.7
Embodied Carbon, kg CO2/kg material 31
8.7
Embodied Energy, MJ/kg 480
150
Embodied Water, L/kg 150
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
6.0
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
47
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 32
51
Strength to Weight: Axial, points 40
17
Strength to Weight: Bending, points 35
25
Thermal Shock Resistance, points 48
7.3

Alloy Composition

Aluminum (Al), % 0
94.5 to 97.5
Carbon (C), % 0 to 0.1
0
Copper (Cu), % 0
0 to 0.050
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 0.55
Magnesium (Mg), % 0
2.5 to 3.5
Manganese (Mn), % 0
0 to 0.45
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 0.55
Titanium (Ti), % 83.5 to 86
0 to 0.2
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15