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7050 Aluminum vs. S36200 Stainless Steel

7050 aluminum belongs to the aluminum alloys classification, while S36200 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 7050 aluminum and the bottom bar is S36200 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 2.2 to 12
3.4 to 4.6
Fatigue Strength, MPa 130 to 210
450 to 570
Poisson's Ratio 0.32
0.28
Shear Modulus, GPa 26
76
Shear Strength, MPa 280 to 330
680 to 810
Tensile Strength: Ultimate (UTS), MPa 490 to 570
1180 to 1410
Tensile Strength: Yield (Proof), MPa 390 to 500
960 to 1240

Thermal Properties

Latent Heat of Fusion, J/g 370
280
Maximum Temperature: Mechanical, °C 190
820
Melting Completion (Liquidus), °C 630
1440
Melting Onset (Solidus), °C 490
1400
Specific Heat Capacity, J/kg-K 860
480
Thermal Conductivity, W/m-K 140
16
Thermal Expansion, µm/m-K 24
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
2.3
Electrical Conductivity: Equal Weight (Specific), % IACS 100
2.6

Otherwise Unclassified Properties

Base Metal Price, % relative 10
12
Density, g/cm3 3.1
7.8
Embodied Carbon, kg CO2/kg material 8.2
2.8
Embodied Energy, MJ/kg 150
40
Embodied Water, L/kg 1120
120

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 10 to 55
46 to 51
Resilience: Unit (Modulus of Resilience), kJ/m3 1110 to 1760
2380 to 3930
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 45
25
Strength to Weight: Axial, points 45 to 51
42 to 50
Strength to Weight: Bending, points 45 to 50
32 to 36
Thermal Diffusivity, mm2/s 54
4.3
Thermal Shock Resistance, points 21 to 25
40 to 48

Alloy Composition

Aluminum (Al), % 87.3 to 92.1
0 to 0.1
Carbon (C), % 0
0 to 0.050
Chromium (Cr), % 0 to 0.040
14 to 14.5
Copper (Cu), % 2.0 to 2.6
0
Iron (Fe), % 0 to 0.15
75.4 to 79.5
Magnesium (Mg), % 1.9 to 2.6
0
Manganese (Mn), % 0 to 0.1
0 to 0.5
Molybdenum (Mo), % 0
0 to 0.3
Nickel (Ni), % 0
6.5 to 7.0
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.12
0 to 0.3
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.060
0.6 to 0.9
Zinc (Zn), % 5.7 to 6.7
0
Zirconium (Zr), % 0.080 to 0.15
0
Residuals, % 0 to 0.15
0