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6262A Aluminum vs. AISI 202 Stainless Steel

6262A 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 6262A aluminum and the bottom bar is AISI 202 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
200
Elongation at Break, % 4.5 to 11
14 to 45
Fatigue Strength, MPa 94 to 110
290 to 330
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
77
Shear Strength, MPa 190 to 240
490 to 590
Tensile Strength: Ultimate (UTS), MPa 310 to 410
700 to 980
Tensile Strength: Yield (Proof), MPa 270 to 370
310 to 580

Thermal Properties

Latent Heat of Fusion, J/g 400
290
Maximum Temperature: Mechanical, °C 160
910
Melting Completion (Liquidus), °C 640
1400
Melting Onset (Solidus), °C 580
1360
Specific Heat Capacity, J/kg-K 890
480
Thermal Conductivity, W/m-K 170
15
Thermal Expansion, µm/m-K 23
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 45
2.4
Electrical Conductivity: Equal Weight (Specific), % IACS 140
2.9

Otherwise Unclassified Properties

Base Metal Price, % relative 11
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 1190
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 17 to 34
120 to 260
Resilience: Unit (Modulus of Resilience), kJ/m3 540 to 1000
250 to 840
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 49
25
Strength to Weight: Axial, points 31 to 41
25 to 35
Strength to Weight: Bending, points 36 to 44
23 to 29
Thermal Diffusivity, mm2/s 67
4.0
Thermal Shock Resistance, points 14 to 18
15 to 21

Alloy Composition

Aluminum (Al), % 94.2 to 97.8
0
Bismuth (Bi), % 0.4 to 0.9
0
Carbon (C), % 0
0 to 0.15
Chromium (Cr), % 0.040 to 0.14
17 to 19
Copper (Cu), % 0.15 to 0.4
0
Iron (Fe), % 0 to 0.7
63.5 to 71.5
Magnesium (Mg), % 0.8 to 1.2
0
Manganese (Mn), % 0 to 0.15
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), % 0.4 to 0.8
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Tin (Sn), % 0.4 to 1.0
0
Titanium (Ti), % 0 to 0.1
0
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0