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R58150 Titanium vs. 1050A Aluminum

R58150 titanium belongs to the titanium alloys classification, while 1050A 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 1050A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
68
Elongation at Break, % 13
1.1 to 33
Fatigue Strength, MPa 330
22 to 55
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 52
26
Shear Strength, MPa 470
44 to 97
Tensile Strength: Ultimate (UTS), MPa 770
68 to 170
Tensile Strength: Yield (Proof), MPa 550
22 to 150

Thermal Properties

Latent Heat of Fusion, J/g 410
400
Maximum Temperature: Mechanical, °C 320
170
Melting Completion (Liquidus), °C 1760
660
Melting Onset (Solidus), °C 1700
650
Specific Heat Capacity, J/kg-K 500
900
Thermal Expansion, µm/m-K 8.4
24

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
1200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
1.9 to 19
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
3.7 to 160
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 32
50
Strength to Weight: Axial, points 40
6.9 to 18
Strength to Weight: Bending, points 35
14 to 25
Thermal Shock Resistance, points 48
3.0 to 7.6

Alloy Composition

Aluminum (Al), % 0
99.5 to 100
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 0.4
Magnesium (Mg), % 0
0 to 0.050
Manganese (Mn), % 0
0 to 0.050
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 0.25
Titanium (Ti), % 83.5 to 86
0 to 0.050
Zinc (Zn), % 0
0 to 0.070