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R58150 Titanium vs. 6351 Aluminum

R58150 titanium belongs to the titanium alloys classification, while 6351 aluminum belongs to the aluminum alloys. There are 26 material properties with values for both materials. Properties with values for just one material (5, in this case) are not shown.

For each property being compared, the top bar is R58150 titanium and the bottom bar is 6351 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
69
Elongation at Break, % 13
7.8 to 18
Fatigue Strength, MPa 330
79 to 130
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 52
26
Shear Strength, MPa 470
84 to 200
Tensile Strength: Ultimate (UTS), MPa 770
140 to 310
Tensile Strength: Yield (Proof), MPa 550
95 to 270

Thermal Properties

Latent Heat of Fusion, J/g 410
410
Maximum Temperature: Mechanical, °C 320
160
Melting Completion (Liquidus), °C 1760
650
Melting Onset (Solidus), °C 1700
570
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
150
Embodied Water, L/kg 150
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
20 to 38
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
65 to 540
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 32
50
Strength to Weight: Axial, points 40
14 to 32
Strength to Weight: Bending, points 35
22 to 38
Thermal Shock Resistance, points 48
6.1 to 14

Alloy Composition

Aluminum (Al), % 0
96 to 98.5
Carbon (C), % 0 to 0.1
0
Copper (Cu), % 0
0 to 0.1
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 0.5
Magnesium (Mg), % 0
0.4 to 0.8
Manganese (Mn), % 0
0.4 to 0.8
Molybdenum (Mo), % 14 to 16
0
Nitrogen (N), % 0 to 0.050
0
Oxygen (O), % 0 to 0.2
0
Silicon (Si), % 0
0.7 to 1.3
Titanium (Ti), % 83.5 to 86
0 to 0.2
Zinc (Zn), % 0
0 to 0.2
Residuals, % 0
0 to 0.15