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R58150 Titanium vs. 772.0 Aluminum

R58150 titanium belongs to the titanium alloys classification, while 772.0 aluminum belongs to the aluminum alloys. There are 25 material properties with values for both materials. Properties with values for just one material (6, in this case) are not shown.

For each property being compared, the top bar is R58150 titanium and the bottom bar is 772.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
69
Elongation at Break, % 13
6.3 to 8.4
Fatigue Strength, MPa 330
94 to 160
Poisson's Ratio 0.32
0.32
Shear Modulus, GPa 52
26
Tensile Strength: Ultimate (UTS), MPa 770
260 to 320
Tensile Strength: Yield (Proof), MPa 550
220 to 250

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
580
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
1140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
16 to 25
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
350 to 430
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 32
46
Strength to Weight: Axial, points 40
25 to 31
Strength to Weight: Bending, points 35
31 to 36
Thermal Shock Resistance, points 48
11 to 14

Alloy Composition


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Aluminum (Al), % 0
91.2 to 93.2
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
0.6 to 0.8
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
6.0 to 7.0
Residuals, % 0
0 to 0.15