MakeItFrom.com
Menu (ESC)

7022 Aluminum vs. S31260 Stainless Steel

7022 aluminum belongs to the aluminum alloys classification, while S31260 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 7022 aluminum and the bottom bar is S31260 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
200
Elongation at Break, % 6.3 to 8.0
23
Fatigue Strength, MPa 140 to 170
370
Poisson's Ratio 0.32
0.27
Shear Modulus, GPa 26
80
Shear Strength, MPa 290 to 320
500
Tensile Strength: Ultimate (UTS), MPa 490 to 540
790
Tensile Strength: Yield (Proof), MPa 390 to 460
540

Thermal Properties

Latent Heat of Fusion, J/g 380
300
Maximum Temperature: Mechanical, °C 200
1100
Melting Completion (Liquidus), °C 640
1450
Melting Onset (Solidus), °C 480
1400
Specific Heat Capacity, J/kg-K 870
480
Thermal Conductivity, W/m-K 140
16
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 21
2.2
Electrical Conductivity: Equal Weight (Specific), % IACS 65
2.5

Otherwise Unclassified Properties

Base Metal Price, % relative 10
20
Density, g/cm3 2.9
7.8
Embodied Carbon, kg CO2/kg material 8.5
3.9
Embodied Energy, MJ/kg 150
53
Embodied Water, L/kg 1130
180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 29 to 40
160
Resilience: Unit (Modulus of Resilience), kJ/m3 1100 to 1500
720
Stiffness to Weight: Axial, points 13
15
Stiffness to Weight: Bending, points 47
25
Strength to Weight: Axial, points 47 to 51
28
Strength to Weight: Bending, points 47 to 50
24
Thermal Diffusivity, mm2/s 54
4.3
Thermal Shock Resistance, points 21 to 23
22

Alloy Composition

Aluminum (Al), % 87.9 to 92.4
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0.1 to 0.3
24 to 26
Copper (Cu), % 0.5 to 1.0
0.2 to 0.8
Iron (Fe), % 0 to 0.5
59.6 to 67.6
Magnesium (Mg), % 2.6 to 3.7
0
Manganese (Mn), % 0.1 to 0.4
0 to 1.0
Molybdenum (Mo), % 0
2.5 to 3.5
Nickel (Ni), % 0
5.5 to 7.5
Nitrogen (N), % 0
0.1 to 0.3
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.5
0 to 0.75
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.2
0
Tungsten (W), % 0
0.1 to 0.5
Zinc (Zn), % 4.3 to 5.2
0
Zirconium (Zr), % 0 to 0.2
0
Residuals, % 0 to 0.15
0