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R58150 Titanium vs. 710.0 Aluminum

R58150 titanium belongs to the titanium alloys classification, while 710.0 aluminum belongs to the aluminum alloys. There are 26 material properties with values for both materials. Properties with values for just one material (7, in this case) are not shown.

For each property being compared, the top bar is R58150 titanium and the bottom bar is 710.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
70
Elongation at Break, % 13
2.2 to 3.6
Fatigue Strength, MPa 330
55 to 110
Poisson's Ratio 0.32
0.32
Shear Modulus, GPa 52
26
Shear Strength, MPa 470
180
Tensile Strength: Ultimate (UTS), MPa 770
240 to 250
Tensile Strength: Yield (Proof), MPa 550
160

Thermal Properties

Latent Heat of Fusion, J/g 410
380
Maximum Temperature: Mechanical, °C 320
170
Melting Completion (Liquidus), °C 1760
650
Melting Onset (Solidus), °C 1700
610
Specific Heat Capacity, J/kg-K 500
870
Thermal Expansion, µm/m-K 8.4
24

Otherwise Unclassified Properties

Base Metal Price, % relative 48
9.5
Density, g/cm3 5.4
3.0
Embodied Carbon, kg CO2/kg material 31
8.0
Embodied Energy, MJ/kg 480
150
Embodied Water, L/kg 150
1130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
4.9 to 7.9
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
180 to 190
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 32
46
Strength to Weight: Axial, points 40
23
Strength to Weight: Bending, points 35
29
Thermal Shock Resistance, points 48
10 to 11

Alloy Composition

Aluminum (Al), % 0
90.5 to 93.1
Carbon (C), % 0 to 0.1
0
Copper (Cu), % 0
0.35 to 0.65
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 0.5
Magnesium (Mg), % 0
0.6 to 0.8
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 0.15
Titanium (Ti), % 83.5 to 86
0 to 0.25
Zinc (Zn), % 0
6.0 to 7.0
Residuals, % 0
0 to 0.15