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R58150 Titanium vs. 296.0 Aluminum

R58150 titanium belongs to the titanium alloys classification, while 296.0 aluminum belongs to the aluminum alloys. There are 25 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 296.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
72
Elongation at Break, % 13
3.2 to 7.1
Fatigue Strength, MPa 330
47 to 70
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 52
27
Tensile Strength: Ultimate (UTS), MPa 770
260 to 270
Tensile Strength: Yield (Proof), MPa 550
120 to 180

Thermal Properties

Latent Heat of Fusion, J/g 410
420
Maximum Temperature: Mechanical, °C 320
170
Melting Completion (Liquidus), °C 1760
630
Melting Onset (Solidus), °C 1700
540
Specific Heat Capacity, J/kg-K 500
870
Thermal Expansion, µm/m-K 8.4
22

Otherwise Unclassified Properties

Base Metal Price, % relative 48
11
Density, g/cm3 5.4
3.0
Embodied Carbon, kg CO2/kg material 31
7.8
Embodied Energy, MJ/kg 480
150
Embodied Water, L/kg 150
1110

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
7.6 to 15
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
110 to 220
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 32
46
Strength to Weight: Axial, points 40
24 to 25
Strength to Weight: Bending, points 35
30 to 31
Thermal Shock Resistance, points 48
12

Alloy Composition


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Aluminum (Al), % 0
89 to 94
Carbon (C), % 0 to 0.1
0
Copper (Cu), % 0
4.0 to 5.0
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 1.2
Magnesium (Mg), % 0
0 to 0.050
Manganese (Mn), % 0
0 to 0.35
Molybdenum (Mo), % 14 to 16
0
Nickel (Ni), % 0
0 to 0.35
Nitrogen (N), % 0 to 0.050
0
Oxygen (O), % 0 to 0.2
0
Silicon (Si), % 0
2.0 to 3.0
Titanium (Ti), % 83.5 to 86
0 to 0.25
Zinc (Zn), % 0
0 to 0.5
Residuals, % 0
0 to 0.35