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S32053 Stainless Steel vs. EN AC-45100 Aluminum

S32053 stainless steel belongs to the iron alloys classification, while EN AC-45100 aluminum belongs to the aluminum alloys. There are 30 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 S32053 stainless steel and the bottom bar is EN AC-45100 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 190
97 to 130
Elastic (Young's, Tensile) Modulus, GPa 210
72
Elongation at Break, % 46
1.0 to 2.8
Fatigue Strength, MPa 310
82 to 99
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 80
27
Tensile Strength: Ultimate (UTS), MPa 730
300 to 360
Tensile Strength: Yield (Proof), MPa 330
210 to 320

Thermal Properties

Latent Heat of Fusion, J/g 310
470
Maximum Temperature: Mechanical, °C 1100
170
Melting Completion (Liquidus), °C 1450
630
Melting Onset (Solidus), °C 1400
550
Specific Heat Capacity, J/kg-K 470
890
Thermal Conductivity, W/m-K 13
140
Thermal Expansion, µm/m-K 16
22

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.8
30
Electrical Conductivity: Equal Weight (Specific), % IACS 2.0
95

Otherwise Unclassified Properties

Base Metal Price, % relative 33
10
Density, g/cm3 8.1
2.8
Embodied Carbon, kg CO2/kg material 6.1
7.9
Embodied Energy, MJ/kg 83
150
Embodied Water, L/kg 210
1100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 270
3.5 to 7.6
Resilience: Unit (Modulus of Resilience), kJ/m3 270
290 to 710
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 24
49
Strength to Weight: Axial, points 25
30 to 35
Strength to Weight: Bending, points 22
35 to 39
Thermal Diffusivity, mm2/s 3.3
54
Thermal Shock Resistance, points 16
14 to 16

Alloy Composition


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Aluminum (Al), % 0
88 to 92.8
Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 22 to 24
0
Copper (Cu), % 0
2.6 to 3.6
Iron (Fe), % 41.7 to 48.8
0 to 0.6
Lead (Pb), % 0
0 to 0.1
Magnesium (Mg), % 0
0.15 to 0.45
Manganese (Mn), % 0 to 1.0
0 to 0.55
Molybdenum (Mo), % 5.0 to 6.0
0
Nickel (Ni), % 24 to 26
0 to 0.1
Nitrogen (N), % 0.17 to 0.22
0
Phosphorus (P), % 0 to 0.030
0
Silicon (Si), % 0 to 1.0
4.5 to 6.0
Sulfur (S), % 0 to 0.010
0
Tin (Sn), % 0
0 to 0.050
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 0
0 to 0.2
Residuals, % 0
0 to 0.15