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R58150 Titanium vs. 771.0 Aluminum

R58150 titanium belongs to the titanium alloys classification, while 771.0 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 771.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

Latent Heat of Fusion, J/g 410
380
Maximum Temperature: Mechanical, °C 320
180
Melting Completion (Liquidus), °C 1760
630
Melting Onset (Solidus), °C 1700
620
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
4.4 to 20
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
310 to 900
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 32
46
Strength to Weight: Axial, points 40
23 to 35
Strength to Weight: Bending, points 35
29 to 39
Thermal Shock Resistance, points 48
11 to 16

Alloy Composition

Aluminum (Al), % 0
90.5 to 92.5
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 0
0.060 to 0.2
Copper (Cu), % 0
0 to 0.1
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 0.15
Magnesium (Mg), % 0
0.8 to 1.0
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
0 to 0.15
Titanium (Ti), % 83.5 to 86
0.1 to 0.2
Zinc (Zn), % 0
6.5 to 7.5
Residuals, % 0
0 to 0.15