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7022 Aluminum vs. AISI 310MoLN Stainless Steel

7022 aluminum belongs to the aluminum alloys classification, while AISI 310MoLN 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 7022 aluminum and the bottom bar is AISI 310MoLN stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
200
Elongation at Break, % 6.3 to 8.0
28
Fatigue Strength, MPa 140 to 170
210
Poisson's Ratio 0.32
0.28
Shear Modulus, GPa 26
80
Shear Strength, MPa 290 to 320
400
Tensile Strength: Ultimate (UTS), MPa 490 to 540
610
Tensile Strength: Yield (Proof), MPa 390 to 460
290

Thermal Properties

Latent Heat of Fusion, J/g 380
300
Maximum Temperature: Mechanical, °C 200
1100
Melting Completion (Liquidus), °C 640
1420
Melting Onset (Solidus), °C 480
1380
Specific Heat Capacity, J/kg-K 870
470
Thermal Conductivity, W/m-K 140
14
Thermal Expansion, µm/m-K 24
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 21
2.2
Electrical Conductivity: Equal Weight (Specific), % IACS 65
2.4

Otherwise Unclassified Properties

Base Metal Price, % relative 10
28
Density, g/cm3 2.9
7.9
Embodied Carbon, kg CO2/kg material 8.5
5.0
Embodied Energy, MJ/kg 150
70
Embodied Water, L/kg 1130
200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 29 to 40
140
Resilience: Unit (Modulus of Resilience), kJ/m3 1100 to 1500
200
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 47
25
Strength to Weight: Axial, points 47 to 51
21
Strength to Weight: Bending, points 47 to 50
20
Thermal Diffusivity, mm2/s 54
3.7
Thermal Shock Resistance, points 21 to 23
14

Alloy Composition

Aluminum (Al), % 87.9 to 92.4
0
Carbon (C), % 0
0 to 0.020
Chromium (Cr), % 0.1 to 0.3
24 to 26
Copper (Cu), % 0.5 to 1.0
0
Iron (Fe), % 0 to 0.5
45.2 to 53.8
Magnesium (Mg), % 2.6 to 3.7
0
Manganese (Mn), % 0.1 to 0.4
0 to 2.0
Molybdenum (Mo), % 0
1.6 to 2.6
Nickel (Ni), % 0
20.5 to 23.5
Nitrogen (N), % 0
0.090 to 0.15
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.5
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 4.3 to 5.2
0
Zirconium (Zr), % 0 to 0.2
0
Residuals, % 0 to 0.15
0