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5005A Aluminum vs. S43932 Stainless Steel

5005A aluminum belongs to the aluminum alloys classification, while S43932 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 5005A aluminum and the bottom bar is S43932 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 29 to 64
160
Elastic (Young's, Tensile) Modulus, GPa 68
200
Elongation at Break, % 1.1 to 21
25
Fatigue Strength, MPa 38 to 82
160
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
77
Shear Strength, MPa 71 to 130
300
Tensile Strength: Ultimate (UTS), MPa 110 to 230
460
Tensile Strength: Yield (Proof), MPa 43 to 210
230

Thermal Properties

Latent Heat of Fusion, J/g 400
280
Maximum Temperature: Mechanical, °C 180
890
Melting Completion (Liquidus), °C 660
1440
Melting Onset (Solidus), °C 630
1400
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 200
23
Thermal Expansion, µm/m-K 24
10

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 52
2.7
Electrical Conductivity: Equal Weight (Specific), % IACS 170
3.2

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
12
Density, g/cm3 2.7
7.7
Embodied Carbon, kg CO2/kg material 8.3
2.7
Embodied Energy, MJ/kg 150
40
Embodied Water, L/kg 1190
120

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.0 to 19
96
Resilience: Unit (Modulus of Resilience), kJ/m3 14 to 310
140
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 12 to 24
17
Strength to Weight: Bending, points 19 to 31
17
Thermal Diffusivity, mm2/s 82
6.3
Thermal Shock Resistance, points 5.0 to 10
16

Alloy Composition


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Aluminum (Al), % 97.5 to 99.3
0 to 0.15
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0 to 0.1
17 to 19
Copper (Cu), % 0 to 0.050
0
Iron (Fe), % 0 to 0.45
76.7 to 83
Magnesium (Mg), % 0.7 to 1.1
0
Manganese (Mn), % 0 to 0.15
0 to 1.0
Nickel (Ni), % 0
0 to 0.5
Niobium (Nb), % 0
0.2 to 0.75
Nitrogen (N), % 0
0 to 0.030
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.3
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0
0.2 to 0.75
Zinc (Zn), % 0 to 0.2
0
Residuals, % 0 to 0.15
0