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7075 Aluminum vs. S32050 Stainless Steel

7075 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 (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 7075 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, % 1.8 to 12
46
Fatigue Strength, MPa 110 to 190
340
Poisson's Ratio 0.32
0.28
Shear Modulus, GPa 26
81
Shear Strength, MPa 150 to 340
540
Tensile Strength: Ultimate (UTS), MPa 240 to 590
770
Tensile Strength: Yield (Proof), MPa 120 to 510
370

Thermal Properties

Latent Heat of Fusion, J/g 380
310
Maximum Temperature: Mechanical, °C 200
1100
Melting Completion (Liquidus), °C 640
1460
Melting Onset (Solidus), °C 480
1410
Specific Heat Capacity, J/kg-K 870
470
Thermal Conductivity, W/m-K 130
12
Thermal Expansion, µm/m-K 23
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 33
1.9
Electrical Conductivity: Equal Weight (Specific), % IACS 98
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 7.8 to 44
290
Resilience: Unit (Modulus of Resilience), kJ/m3 110 to 1870
330
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 46
25
Strength to Weight: Axial, points 22 to 54
27
Strength to Weight: Bending, points 28 to 52
23
Thermal Diffusivity, mm2/s 50
3.3
Thermal Shock Resistance, points 10 to 25
17

Alloy Composition

Aluminum (Al), % 86.9 to 91.4
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0.18 to 0.28
22 to 24
Copper (Cu), % 1.2 to 2.0
0 to 0.4
Iron (Fe), % 0 to 0.5
43.1 to 51.8
Magnesium (Mg), % 2.1 to 2.9
0
Manganese (Mn), % 0 to 0.3
0 to 1.5
Molybdenum (Mo), % 0
6.0 to 6.6
Nickel (Ni), % 0
20 to 23
Nitrogen (N), % 0
0.21 to 0.32
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 0 to 0.4
0 to 1.0
Sulfur (S), % 0
0 to 0.020
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 5.1 to 6.1
0
Zirconium (Zr), % 0 to 0.25
0
Residuals, % 0 to 0.15
0