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R58150 Titanium vs. C355.0 Aluminum

R58150 titanium belongs to the titanium alloys classification, while C355.0 aluminum belongs to the aluminum alloys. There are 25 material properties with values for both materials. Properties with values for just one material (8, in this case) are not shown.

For each property being compared, the top bar is R58150 titanium and the bottom bar is C355.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
70
Elongation at Break, % 13
2.7 to 3.8
Fatigue Strength, MPa 330
76 to 84
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 52
26
Tensile Strength: Ultimate (UTS), MPa 770
290 to 310
Tensile Strength: Yield (Proof), MPa 550
200 to 230

Thermal Properties

Latent Heat of Fusion, J/g 410
470
Maximum Temperature: Mechanical, °C 320
170
Melting Completion (Liquidus), °C 1760
620
Melting Onset (Solidus), °C 1700
570
Specific Heat Capacity, J/kg-K 500
900
Thermal Expansion, µm/m-K 8.4
22

Otherwise Unclassified Properties

Base Metal Price, % relative 48
9.5
Density, g/cm3 5.4
2.7
Embodied Carbon, kg CO2/kg material 31
8.0
Embodied Energy, MJ/kg 480
150
Embodied Water, L/kg 150
1120

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
7.5 to 9.8
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
290 to 380
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 32
51
Strength to Weight: Axial, points 40
30 to 32
Strength to Weight: Bending, points 35
36 to 37
Thermal Shock Resistance, points 48
13 to 14

Alloy Composition

Aluminum (Al), % 0
91.7 to 94.1
Carbon (C), % 0 to 0.1
0
Copper (Cu), % 0
1.0 to 1.5
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 0.2
Magnesium (Mg), % 0
0.4 to 0.6
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
4.5 to 5.5
Titanium (Ti), % 83.5 to 86
0 to 0.2
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15