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6351 Aluminum vs. R58150 Titanium

6351 aluminum belongs to the aluminum alloys classification, while R58150 titanium belongs to the titanium 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 6351 aluminum and the bottom bar is R58150 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

Latent Heat of Fusion, J/g 410
410
Maximum Temperature: Mechanical, °C 160
320
Melting Completion (Liquidus), °C 650
1760
Melting Onset (Solidus), °C 570
1700
Specific Heat Capacity, J/kg-K 900
500
Thermal Expansion, µm/m-K 23
8.4

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
48
Density, g/cm3 2.7
5.4
Embodied Carbon, kg CO2/kg material 8.3
31
Embodied Energy, MJ/kg 150
480
Embodied Water, L/kg 1180
150

Common Calculations

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

Alloy Composition

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