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EN AC-45100 Aluminum vs. S32050 Stainless Steel

EN AC-45100 aluminum belongs to the aluminum alloys classification, while S32050 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, 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 EN AC-45100 aluminum and the bottom bar is S32050 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 97 to 130
220
Elastic (Young's, Tensile) Modulus, GPa 72
210
Elongation at Break, % 1.0 to 2.8
46
Fatigue Strength, MPa 82 to 99
340
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
81
Tensile Strength: Ultimate (UTS), MPa 300 to 360
770
Tensile Strength: Yield (Proof), MPa 210 to 320
370

Thermal Properties

Latent Heat of Fusion, J/g 470
310
Maximum Temperature: Mechanical, °C 170
1100
Melting Completion (Liquidus), °C 630
1460
Melting Onset (Solidus), °C 550
1410
Specific Heat Capacity, J/kg-K 890
470
Thermal Conductivity, W/m-K 140
12
Thermal Expansion, µm/m-K 22
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 30
1.9
Electrical Conductivity: Equal Weight (Specific), % IACS 95
2.1

Otherwise Unclassified Properties

Base Metal Price, % relative 10
31
Density, g/cm3 2.8
8.0
Embodied Carbon, kg CO2/kg material 7.9
6.0
Embodied Energy, MJ/kg 150
81
Embodied Water, L/kg 1100
210

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 3.5 to 7.6
290
Resilience: Unit (Modulus of Resilience), kJ/m3 290 to 710
330
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 49
25
Strength to Weight: Axial, points 30 to 35
27
Strength to Weight: Bending, points 35 to 39
23
Thermal Diffusivity, mm2/s 54
3.3
Thermal Shock Resistance, points 14 to 16
17

Alloy Composition


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Aluminum (Al), % 88 to 92.8
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0
22 to 24
Copper (Cu), % 2.6 to 3.6
0 to 0.4
Iron (Fe), % 0 to 0.6
43.1 to 51.8
Lead (Pb), % 0 to 0.1
0
Magnesium (Mg), % 0.15 to 0.45
0
Manganese (Mn), % 0 to 0.55
0 to 1.5
Molybdenum (Mo), % 0
6.0 to 6.6
Nickel (Ni), % 0 to 0.1
20 to 23
Nitrogen (N), % 0
0.21 to 0.32
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 4.5 to 6.0
0 to 1.0
Sulfur (S), % 0
0 to 0.020
Tin (Sn), % 0 to 0.050
0
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 0.2
0
Residuals, % 0 to 0.15
0