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7049 Aluminum vs. S32050 Stainless Steel

7049 aluminum belongs to the aluminum alloys classification, while S32050 stainless steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, 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 7049 aluminum and the bottom bar is S32050 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 140
220
Elastic (Young's, Tensile) Modulus, GPa 70
210
Elongation at Break, % 6.2 to 7.0
46
Fatigue Strength, MPa 160 to 170
340
Poisson's Ratio 0.32
0.28
Shear Modulus, GPa 27
81
Shear Strength, MPa 300 to 310
540
Tensile Strength: Ultimate (UTS), MPa 510 to 530
770
Tensile Strength: Yield (Proof), MPa 420 to 450
370

Thermal Properties

Latent Heat of Fusion, J/g 370
310
Maximum Temperature: Mechanical, °C 180
1100
Melting Completion (Liquidus), °C 640
1460
Melting Onset (Solidus), °C 480
1410
Specific Heat Capacity, J/kg-K 860
470
Thermal Conductivity, W/m-K 130
12
Thermal Expansion, µm/m-K 23
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 36
1.9
Electrical Conductivity: Equal Weight (Specific), % IACS 110
2.1

Otherwise Unclassified Properties

Base Metal Price, % relative 10
31
Density, g/cm3 3.1
8.0
Embodied Carbon, kg CO2/kg material 8.1
6.0
Embodied Energy, MJ/kg 140
81
Embodied Water, L/kg 1110
210

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 31 to 34
290
Resilience: Unit (Modulus of Resilience), kJ/m3 1270 to 1440
330
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 45
25
Strength to Weight: Axial, points 46 to 47
27
Strength to Weight: Bending, points 46 to 47
23
Thermal Diffusivity, mm2/s 51
3.3
Thermal Shock Resistance, points 22 to 23
17

Alloy Composition

Aluminum (Al), % 85.7 to 89.5
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0.1 to 0.22
22 to 24
Copper (Cu), % 1.2 to 1.9
0 to 0.4
Iron (Fe), % 0 to 0.35
43.1 to 51.8
Magnesium (Mg), % 2.0 to 2.9
0
Manganese (Mn), % 0 to 0.2
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 0.25
0 to 1.0
Sulfur (S), % 0
0 to 0.020
Titanium (Ti), % 0 to 0.1
0
Zinc (Zn), % 7.2 to 8.2
0
Residuals, % 0 to 0.15
0