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7010 Aluminum vs. S32050 Stainless Steel

7010 aluminum belongs to the aluminum alloys classification, while S32050 stainless steel belongs to the iron alloys. There are 30 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 7010 aluminum and the bottom bar is S32050 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
210
Elongation at Break, % 3.9 to 6.8
46
Fatigue Strength, MPa 160 to 190
340
Poisson's Ratio 0.32
0.28
Shear Modulus, GPa 26
81
Shear Strength, MPa 300 to 340
540
Tensile Strength: Ultimate (UTS), MPa 520 to 590
770
Tensile Strength: Yield (Proof), MPa 410 to 540
370

Thermal Properties

Latent Heat of Fusion, J/g 380
310
Maximum Temperature: Mechanical, °C 200
1100
Melting Completion (Liquidus), °C 630
1460
Melting Onset (Solidus), °C 480
1410
Specific Heat Capacity, J/kg-K 860
470
Thermal Conductivity, W/m-K 150
12
Thermal Expansion, µm/m-K 24
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 40
1.9
Electrical Conductivity: Equal Weight (Specific), % IACS 120
2.1

Otherwise Unclassified Properties

Base Metal Price, % relative 10
31
Density, g/cm3 3.0
8.0
Embodied Carbon, kg CO2/kg material 8.3
6.0
Embodied Energy, MJ/kg 150
81
Embodied Water, L/kg 1120
210

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 22 to 33
290
Resilience: Unit (Modulus of Resilience), kJ/m3 1230 to 2130
330
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 45
25
Strength to Weight: Axial, points 47 to 54
27
Strength to Weight: Bending, points 47 to 52
23
Thermal Diffusivity, mm2/s 58
3.3
Thermal Shock Resistance, points 22 to 26
17

Alloy Composition

Aluminum (Al), % 87.9 to 90.6
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0 to 0.050
22 to 24
Copper (Cu), % 1.5 to 2.0
0 to 0.4
Iron (Fe), % 0 to 0.15
43.1 to 51.8
Magnesium (Mg), % 2.1 to 2.6
0
Manganese (Mn), % 0 to 0.1
0 to 1.5
Molybdenum (Mo), % 0
6.0 to 6.6
Nickel (Ni), % 0 to 0.050
20 to 23
Nitrogen (N), % 0
0.21 to 0.32
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 0 to 0.12
0 to 1.0
Sulfur (S), % 0
0 to 0.020
Titanium (Ti), % 0 to 0.060
0
Zinc (Zn), % 5.7 to 6.7
0
Zirconium (Zr), % 0.1 to 0.16
0
Residuals, % 0 to 0.15
0