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R58150 Titanium vs. 1080A Aluminum

R58150 titanium belongs to the titanium alloys classification, while 1080A aluminum belongs to the aluminum alloys. There are 26 material properties with values for both materials. Properties with values for just one material (6, in this case) are not shown.

For each property being compared, the top bar is R58150 titanium and the bottom bar is 1080A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
68
Elongation at Break, % 13
2.3 to 34
Fatigue Strength, MPa 330
18 to 50
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 52
26
Shear Strength, MPa 470
49 to 81
Tensile Strength: Ultimate (UTS), MPa 770
74 to 140
Tensile Strength: Yield (Proof), MPa 550
17 to 120

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
640
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
8.3
Embodied Energy, MJ/kg 480
160
Embodied Water, L/kg 150
1200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
3.1 to 19
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
2.1 to 100
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 32
50
Strength to Weight: Axial, points 40
7.6 to 15
Strength to Weight: Bending, points 35
14 to 22
Thermal Shock Resistance, points 48
3.3 to 6.4

Alloy Composition

Aluminum (Al), % 0
99.8 to 100
Carbon (C), % 0 to 0.1
0
Copper (Cu), % 0
0 to 0.030
Gallium (Ga), % 0
0 to 0.030
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 0.15
Magnesium (Mg), % 0
0 to 0.020
Manganese (Mn), % 0
0 to 0.020
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 0.15
Titanium (Ti), % 83.5 to 86
0 to 0.020
Zinc (Zn), % 0
0 to 0.060