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R58150 Titanium vs. 204.0 Aluminum

R58150 titanium belongs to the titanium alloys classification, while 204.0 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 204.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
71
Elongation at Break, % 13
5.7 to 7.8
Fatigue Strength, MPa 330
63 to 77
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 52
27
Tensile Strength: Ultimate (UTS), MPa 770
230 to 340
Tensile Strength: Yield (Proof), MPa 550
180 to 220

Thermal Properties

Latent Heat of Fusion, J/g 410
390
Maximum Temperature: Mechanical, °C 320
170
Melting Completion (Liquidus), °C 1760
650
Melting Onset (Solidus), °C 1700
580
Specific Heat Capacity, J/kg-K 500
880
Thermal Expansion, µm/m-K 8.4
19

Otherwise Unclassified Properties

Base Metal Price, % relative 48
11
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
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
12 to 23
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
220 to 350
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 32
46
Strength to Weight: Axial, points 40
21 to 31
Strength to Weight: Bending, points 35
28 to 36
Thermal Shock Resistance, points 48
12 to 18

Alloy Composition


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Aluminum (Al), % 0
93.4 to 95.5
Carbon (C), % 0 to 0.1
0
Copper (Cu), % 0
4.2 to 5.0
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 0.35
Magnesium (Mg), % 0
0.15 to 0.35
Manganese (Mn), % 0
0 to 0.1
Molybdenum (Mo), % 14 to 16
0
Nickel (Ni), % 0
0 to 0.050
Nitrogen (N), % 0 to 0.050
0
Oxygen (O), % 0 to 0.2
0
Silicon (Si), % 0
0 to 0.2
Tin (Sn), % 0
0 to 0.050
Titanium (Ti), % 83.5 to 86
0.15 to 0.3
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15