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851.0 Aluminum vs. S21460 Stainless Steel

851.0 aluminum belongs to the aluminum alloys classification, while S21460 stainless steel belongs to the iron alloys. There are 21 material properties with values for both materials. Properties with values for just one material (13, 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 851.0 aluminum and the bottom bar is S21460 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
200
Elongation at Break, % 3.9 to 9.1
46
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
77
Tensile Strength: Ultimate (UTS), MPa 130 to 140
830

Thermal Properties

Latent Heat of Fusion, J/g 410
290
Maximum Temperature: Mechanical, °C 180
920
Melting Completion (Liquidus), °C 630
1380
Melting Onset (Solidus), °C 360
1330
Specific Heat Capacity, J/kg-K 850
480
Thermal Expansion, µm/m-K 23
18

Otherwise Unclassified Properties

Base Metal Price, % relative 14
14
Density, g/cm3 3.1
7.6
Embodied Carbon, kg CO2/kg material 8.4
3.0
Embodied Energy, MJ/kg 160
43
Embodied Water, L/kg 1140
160

Common Calculations

Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 45
25
Strength to Weight: Axial, points 12 to 13
30
Strength to Weight: Bending, points 19 to 20
26
Thermal Shock Resistance, points 6.1 to 6.3
17

Alloy Composition


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Aluminum (Al), % 86.6 to 91.5
0
Carbon (C), % 0
0 to 0.12
Chromium (Cr), % 0
17 to 19
Copper (Cu), % 0.7 to 1.3
0
Iron (Fe), % 0 to 0.7
57.3 to 63.7
Magnesium (Mg), % 0 to 0.1
0
Manganese (Mn), % 0 to 0.1
14 to 16
Nickel (Ni), % 0.3 to 0.7
5.0 to 6.0
Nitrogen (N), % 0
0.35 to 0.5
Phosphorus (P), % 0
0 to 0.060
Silicon (Si), % 2.0 to 3.0
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Tin (Sn), % 5.5 to 7.0
0
Titanium (Ti), % 0 to 0.2
0
Residuals, % 0 to 0.3
0