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7050 Aluminum vs. S42300 Stainless Steel

7050 aluminum belongs to the aluminum alloys classification, while S42300 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (5, 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 S42300 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
200
Elongation at Break, % 2.2 to 12
9.1
Fatigue Strength, MPa 130 to 210
440
Poisson's Ratio 0.32
0.28
Shear Modulus, GPa 26
77
Shear Strength, MPa 280 to 330
650
Tensile Strength: Ultimate (UTS), MPa 490 to 570
1100
Tensile Strength: Yield (Proof), MPa 390 to 500
850

Thermal Properties

Latent Heat of Fusion, J/g 370
270
Maximum Temperature: Mechanical, °C 190
750
Melting Completion (Liquidus), °C 630
1470
Melting Onset (Solidus), °C 490
1420
Specific Heat Capacity, J/kg-K 860
470
Thermal Conductivity, W/m-K 140
25
Thermal Expansion, µm/m-K 24
10

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
4.5
Electrical Conductivity: Equal Weight (Specific), % IACS 100
5.2

Otherwise Unclassified Properties

Base Metal Price, % relative 10
9.5
Density, g/cm3 3.1
7.8
Embodied Carbon, kg CO2/kg material 8.2
3.2
Embodied Energy, MJ/kg 150
44
Embodied Water, L/kg 1120
110

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 10 to 55
93
Resilience: Unit (Modulus of Resilience), kJ/m3 1110 to 1760
1840
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 45
25
Strength to Weight: Axial, points 45 to 51
39
Strength to Weight: Bending, points 45 to 50
30
Thermal Diffusivity, mm2/s 54
6.8
Thermal Shock Resistance, points 21 to 25
40

Alloy Composition

Aluminum (Al), % 87.3 to 92.1
0
Carbon (C), % 0
0.27 to 0.32
Chromium (Cr), % 0 to 0.040
11 to 12
Copper (Cu), % 2.0 to 2.6
0
Iron (Fe), % 0 to 0.15
82 to 85.1
Magnesium (Mg), % 1.9 to 2.6
0
Manganese (Mn), % 0 to 0.1
1.0 to 1.4
Molybdenum (Mo), % 0
2.5 to 3.0
Nickel (Ni), % 0
0 to 0.5
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.12
0 to 0.5
Sulfur (S), % 0
0 to 0.025
Titanium (Ti), % 0 to 0.060
0
Vanadium (V), % 0
0.2 to 0.3
Zinc (Zn), % 5.7 to 6.7
0
Zirconium (Zr), % 0.080 to 0.15
0
Residuals, % 0 to 0.15
0