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6110A Aluminum vs. AISI 202 Stainless Steel

6110A aluminum belongs to the aluminum alloys classification, while AISI 202 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 6110A aluminum and the bottom bar is AISI 202 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
200
Elongation at Break, % 11 to 18
14 to 45
Fatigue Strength, MPa 140 to 210
290 to 330
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
77
Shear Strength, MPa 220 to 280
490 to 590
Tensile Strength: Ultimate (UTS), MPa 360 to 470
700 to 980
Tensile Strength: Yield (Proof), MPa 250 to 430
310 to 580

Thermal Properties

Latent Heat of Fusion, J/g 410
290
Maximum Temperature: Mechanical, °C 190
910
Melting Completion (Liquidus), °C 650
1400
Melting Onset (Solidus), °C 600
1360
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 160
15
Thermal Expansion, µm/m-K 23
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 42
2.4
Electrical Conductivity: Equal Weight (Specific), % IACS 140
2.9

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
13
Density, g/cm3 2.8
7.7
Embodied Carbon, kg CO2/kg material 8.4
2.8
Embodied Energy, MJ/kg 150
40
Embodied Water, L/kg 1170
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 47 to 58
120 to 260
Resilience: Unit (Modulus of Resilience), kJ/m3 450 to 1300
250 to 840
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 36 to 47
25 to 35
Strength to Weight: Bending, points 41 to 48
23 to 29
Thermal Diffusivity, mm2/s 65
4.0
Thermal Shock Resistance, points 16 to 21
15 to 21

Alloy Composition

Aluminum (Al), % 94.8 to 98
0
Carbon (C), % 0
0 to 0.15
Chromium (Cr), % 0.050 to 0.25
17 to 19
Copper (Cu), % 0.3 to 0.8
0
Iron (Fe), % 0 to 0.5
63.5 to 71.5
Magnesium (Mg), % 0.7 to 1.1
0
Manganese (Mn), % 0.3 to 0.9
7.5 to 10
Nickel (Ni), % 0
4.0 to 6.0
Nitrogen (N), % 0
0 to 0.25
Phosphorus (P), % 0
0 to 0.060
Silicon (Si), % 0.7 to 1.1
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 0 to 0.2
0
Zirconium (Zr), % 0 to 0.2
0
Residuals, % 0 to 0.15
0