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5457 Aluminum vs. S40910 Stainless Steel

5457 aluminum belongs to the aluminum alloys classification, while S40910 stainless steel belongs to the iron alloys. There are 31 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 5457 aluminum and the bottom bar is S40910 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 32 to 55
160
Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 6.0 to 22
23
Fatigue Strength, MPa 55 to 98
130
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
75
Shear Strength, MPa 85 to 130
270
Tensile Strength: Ultimate (UTS), MPa 130 to 210
430
Tensile Strength: Yield (Proof), MPa 50 to 190
190

Thermal Properties

Latent Heat of Fusion, J/g 400
270
Maximum Temperature: Mechanical, °C 180
710
Melting Completion (Liquidus), °C 660
1450
Melting Onset (Solidus), °C 630
1410
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 180
26
Thermal Expansion, µm/m-K 24
10

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 46
2.9
Electrical Conductivity: Equal Weight (Specific), % IACS 150
3.3

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
7.0
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.4
2.0
Embodied Energy, MJ/kg 160
28
Embodied Water, L/kg 1190
94

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 12 to 23
80
Resilience: Unit (Modulus of Resilience), kJ/m3 18 to 250
94
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 13 to 21
16
Strength to Weight: Bending, points 21 to 28
16
Thermal Diffusivity, mm2/s 72
6.9
Thermal Shock Resistance, points 5.7 to 9.0
16

Alloy Composition

Aluminum (Al), % 97.8 to 99.05
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0
10.5 to 11.7
Copper (Cu), % 0 to 0.2
0
Iron (Fe), % 0 to 0.1
85 to 89.5
Magnesium (Mg), % 0.8 to 1.2
0
Manganese (Mn), % 0.15 to 0.45
0 to 1.0
Nickel (Ni), % 0
0 to 0.5
Niobium (Nb), % 0
0 to 0.17
Nitrogen (N), % 0
0 to 0.030
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.080
0 to 1.0
Sulfur (S), % 0
0 to 0.020
Titanium (Ti), % 0
0 to 0.5
Vanadium (V), % 0 to 0.050
0
Zinc (Zn), % 0 to 0.050
0
Residuals, % 0 to 0.1
0