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771.0 Aluminum vs. R58150 Titanium

771.0 aluminum belongs to the aluminum alloys classification, while R58150 titanium belongs to the titanium 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 771.0 aluminum and the bottom bar is R58150 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
140
Elongation at Break, % 1.7 to 6.5
13
Fatigue Strength, MPa 92 to 180
330
Poisson's Ratio 0.32
0.32
Shear Modulus, GPa 26
52
Tensile Strength: Ultimate (UTS), MPa 250 to 370
770
Tensile Strength: Yield (Proof), MPa 210 to 350
550

Thermal Properties

Latent Heat of Fusion, J/g 380
410
Maximum Temperature: Mechanical, °C 180
320
Melting Completion (Liquidus), °C 630
1760
Melting Onset (Solidus), °C 620
1700
Specific Heat Capacity, J/kg-K 870
500
Thermal Expansion, µm/m-K 24
8.4

Otherwise Unclassified Properties

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

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.4 to 20
94
Resilience: Unit (Modulus of Resilience), kJ/m3 310 to 900
1110
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 46
32
Strength to Weight: Axial, points 23 to 35
40
Strength to Weight: Bending, points 29 to 39
35
Thermal Shock Resistance, points 11 to 16
48

Alloy Composition

Aluminum (Al), % 90.5 to 92.5
0
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0.060 to 0.2
0
Copper (Cu), % 0 to 0.1
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0 to 0.15
0 to 0.1
Magnesium (Mg), % 0.8 to 1.0
0
Manganese (Mn), % 0 to 0.1
0
Molybdenum (Mo), % 0
14 to 16
Nitrogen (N), % 0
0 to 0.050
Oxygen (O), % 0
0 to 0.2
Silicon (Si), % 0 to 0.15
0
Titanium (Ti), % 0.1 to 0.2
83.5 to 86
Zinc (Zn), % 6.5 to 7.5
0
Residuals, % 0 to 0.15
0