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6012 Aluminum vs. EN 1.4945 Stainless Steel

6012 aluminum belongs to the aluminum alloys classification, while EN 1.4945 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 6012 aluminum and the bottom bar is EN 1.4945 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
200
Elongation at Break, % 9.1 to 11
19 to 34
Fatigue Strength, MPa 55 to 100
230 to 350
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
77
Shear Strength, MPa 130 to 190
430 to 460
Tensile Strength: Ultimate (UTS), MPa 220 to 320
640 to 740
Tensile Strength: Yield (Proof), MPa 110 to 260
290 to 550

Thermal Properties

Latent Heat of Fusion, J/g 400
290
Maximum Temperature: Mechanical, °C 170
920
Melting Completion (Liquidus), °C 640
1490
Melting Onset (Solidus), °C 570
1440
Specific Heat Capacity, J/kg-K 890
470
Thermal Conductivity, W/m-K 160
14
Thermal Expansion, µm/m-K 23
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 45
2.9
Electrical Conductivity: Equal Weight (Specific), % IACS 140
3.2

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
30
Density, g/cm3 2.9
8.1
Embodied Carbon, kg CO2/kg material 8.2
5.0
Embodied Energy, MJ/kg 150
73
Embodied Water, L/kg 1170
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 21 to 28
130 to 180
Resilience: Unit (Modulus of Resilience), kJ/m3 94 to 480
210 to 760
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 48
24
Strength to Weight: Axial, points 22 to 32
22 to 25
Strength to Weight: Bending, points 29 to 37
20 to 22
Thermal Diffusivity, mm2/s 62
3.7
Thermal Shock Resistance, points 10 to 14
14 to 16

Alloy Composition

Aluminum (Al), % 92.2 to 98
0
Bismuth (Bi), % 0 to 0.7
0
Carbon (C), % 0
0.040 to 0.1
Chromium (Cr), % 0 to 0.3
15.5 to 17.5
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.5
57.9 to 65.7
Lead (Pb), % 0.4 to 2.0
0
Magnesium (Mg), % 0.6 to 1.2
0
Manganese (Mn), % 0.4 to 1.0
0 to 1.5
Nickel (Ni), % 0
15.5 to 17.5
Niobium (Nb), % 0
0.4 to 1.2
Nitrogen (N), % 0
0.060 to 0.14
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 0.6 to 1.4
0.3 to 0.6
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.2
0
Tungsten (W), % 0
2.5 to 3.5
Zinc (Zn), % 0 to 0.3
0
Residuals, % 0 to 0.15
0