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5154A Aluminum vs. S82012 Stainless Steel

5154A aluminum belongs to the aluminum alloys classification, while S82012 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (4, 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 5154A aluminum and the bottom bar is S82012 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
200
Elongation at Break, % 1.1 to 19
40
Fatigue Strength, MPa 83 to 160
480
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
78
Shear Strength, MPa 140 to 210
550
Tensile Strength: Ultimate (UTS), MPa 230 to 370
800
Tensile Strength: Yield (Proof), MPa 96 to 320
560

Thermal Properties

Latent Heat of Fusion, J/g 400
280
Maximum Temperature: Mechanical, °C 190
950
Melting Completion (Liquidus), °C 650
1430
Melting Onset (Solidus), °C 600
1380
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 130
15
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 32
2.2
Electrical Conductivity: Equal Weight (Specific), % IACS 110
2.5

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
11
Density, g/cm3 2.7
7.7
Embodied Carbon, kg CO2/kg material 8.8
2.4
Embodied Energy, MJ/kg 150
35
Embodied Water, L/kg 1180
140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.0 to 36
290
Resilience: Unit (Modulus of Resilience), kJ/m3 68 to 760
790
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
25
Strength to Weight: Axial, points 24 to 38
29
Strength to Weight: Bending, points 31 to 43
25
Thermal Diffusivity, mm2/s 53
3.9
Thermal Shock Resistance, points 10 to 16
23

Alloy Composition

Aluminum (Al), % 93.7 to 96.9
0
Carbon (C), % 0
0 to 0.050
Chromium (Cr), % 0 to 0.25
19 to 20.5
Copper (Cu), % 0 to 0.1
0 to 1.0
Iron (Fe), % 0 to 0.5
71.3 to 77.9
Magnesium (Mg), % 3.1 to 3.9
0
Manganese (Mn), % 0 to 0.5
2.0 to 4.0
Molybdenum (Mo), % 0
0.1 to 0.6
Nickel (Ni), % 0
0.8 to 1.5
Nitrogen (N), % 0
0.16 to 0.26
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.5
0 to 0.8
Sulfur (S), % 0
0 to 0.0050
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 0 to 0.2
0
Residuals, % 0 to 0.15
0