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EN AC-51300 Aluminum vs. AISI 202 Stainless Steel

EN AC-51300 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 EN AC-51300 aluminum and the bottom bar is AISI 202 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 65
210 to 300
Elastic (Young's, Tensile) Modulus, GPa 67
200
Elongation at Break, % 3.7
14 to 45
Fatigue Strength, MPa 78
290 to 330
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 25
77
Tensile Strength: Ultimate (UTS), MPa 190
700 to 980
Tensile Strength: Yield (Proof), MPa 110
310 to 580

Thermal Properties

Latent Heat of Fusion, J/g 400
290
Maximum Temperature: Mechanical, °C 170
910
Melting Completion (Liquidus), °C 640
1400
Melting Onset (Solidus), °C 600
1360
Specific Heat Capacity, J/kg-K 910
480
Thermal Conductivity, W/m-K 110
15
Thermal Expansion, µm/m-K 24
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 31
2.4
Electrical Conductivity: Equal Weight (Specific), % IACS 100
2.9

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
13
Density, g/cm3 2.7
7.7
Embodied Carbon, kg CO2/kg material 9.1
2.8
Embodied Energy, MJ/kg 150
40
Embodied Water, L/kg 1180
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 6.1
120 to 260
Resilience: Unit (Modulus of Resilience), kJ/m3 87
250 to 840
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
25
Strength to Weight: Axial, points 20
25 to 35
Strength to Weight: Bending, points 28
23 to 29
Thermal Diffusivity, mm2/s 45
4.0
Thermal Shock Resistance, points 8.6
15 to 21

Alloy Composition


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Aluminum (Al), % 91.4 to 95.5
0
Carbon (C), % 0
0 to 0.15
Chromium (Cr), % 0
17 to 19
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.55
63.5 to 71.5
Magnesium (Mg), % 4.5 to 6.5
0
Manganese (Mn), % 0 to 0.45
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 to 0.55
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0