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518.0 Aluminum vs. S15500 Stainless Steel

518.0 aluminum belongs to the aluminum alloys classification, while S15500 stainless steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (5, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is 518.0 aluminum and the bottom bar is S15500 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 80
290 to 430
Elastic (Young's, Tensile) Modulus, GPa 67
190
Elongation at Break, % 5.0
6.8 to 16
Fatigue Strength, MPa 140
350 to 650
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 25
75
Shear Strength, MPa 200
540 to 870
Tensile Strength: Ultimate (UTS), MPa 310
890 to 1490
Tensile Strength: Yield (Proof), MPa 190
590 to 1310

Thermal Properties

Latent Heat of Fusion, J/g 390
280
Maximum Temperature: Mechanical, °C 170
820
Melting Completion (Liquidus), °C 620
1430
Melting Onset (Solidus), °C 560
1380
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 98
17
Thermal Expansion, µm/m-K 24
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 24
2.2
Electrical Conductivity: Equal Weight (Specific), % IACS 81
2.5

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
13
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 9.4
2.7
Embodied Energy, MJ/kg 150
39
Embodied Water, L/kg 1160
130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14
98 to 120
Resilience: Unit (Modulus of Resilience), kJ/m3 270
890 to 4460
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
25
Strength to Weight: Axial, points 32
32 to 53
Strength to Weight: Bending, points 38
26 to 37
Thermal Diffusivity, mm2/s 40
4.6
Thermal Shock Resistance, points 14
30 to 50

Alloy Composition

Aluminum (Al), % 88.1 to 92.5
0
Carbon (C), % 0
0 to 0.070
Chromium (Cr), % 0
14 to 15.5
Copper (Cu), % 0 to 0.25
2.5 to 4.5
Iron (Fe), % 0 to 1.8
71.9 to 79.9
Magnesium (Mg), % 7.5 to 8.5
0
Manganese (Mn), % 0 to 0.35
0 to 1.0
Nickel (Ni), % 0 to 0.15
3.5 to 5.5
Niobium (Nb), % 0
0.15 to 0.45
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.35
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Tin (Sn), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.15
0
Residuals, % 0 to 0.25
0