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R58150 Titanium vs. 2618 Aluminum

R58150 titanium belongs to the titanium alloys classification, while 2618 aluminum belongs to the aluminum alloys. There are 26 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 2618 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
71
Elongation at Break, % 13
5.8
Fatigue Strength, MPa 330
110
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 52
27
Shear Strength, MPa 470
260
Tensile Strength: Ultimate (UTS), MPa 770
420
Tensile Strength: Yield (Proof), MPa 550
350

Thermal Properties

Latent Heat of Fusion, J/g 410
390
Maximum Temperature: Mechanical, °C 320
210
Melting Completion (Liquidus), °C 1760
640
Melting Onset (Solidus), °C 1700
550
Specific Heat Capacity, J/kg-K 500
880
Thermal Expansion, µm/m-K 8.4
22

Otherwise Unclassified Properties

Base Metal Price, % relative 48
11
Density, g/cm3 5.4
2.9
Embodied Carbon, kg CO2/kg material 31
8.3
Embodied Energy, MJ/kg 480
150
Embodied Water, L/kg 150
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
23
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
850
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 32
47
Strength to Weight: Axial, points 40
40
Strength to Weight: Bending, points 35
42
Thermal Shock Resistance, points 48
19

Alloy Composition

Aluminum (Al), % 0
92.4 to 94.9
Carbon (C), % 0 to 0.1
0
Copper (Cu), % 0
1.9 to 2.7
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0.9 to 1.3
Magnesium (Mg), % 0
1.3 to 1.8
Molybdenum (Mo), % 14 to 16
0
Nickel (Ni), % 0
0.9 to 1.2
Nitrogen (N), % 0 to 0.050
0
Oxygen (O), % 0 to 0.2
0
Silicon (Si), % 0
0.1 to 0.25
Titanium (Ti), % 83.5 to 86
0.040 to 0.1
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15