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EN 1.4958 Stainless Steel vs. 6012 Aluminum

EN 1.4958 stainless steel belongs to the iron alloys classification, while 6012 aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, 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 1.4958 stainless steel and the bottom bar is 6012 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
69
Elongation at Break, % 40
9.1 to 11
Fatigue Strength, MPa 170
55 to 100
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
26
Shear Strength, MPa 430
130 to 190
Tensile Strength: Ultimate (UTS), MPa 630
220 to 320
Tensile Strength: Yield (Proof), MPa 190
110 to 260

Thermal Properties

Latent Heat of Fusion, J/g 300
400
Maximum Temperature: Mechanical, °C 1090
170
Melting Completion (Liquidus), °C 1400
640
Melting Onset (Solidus), °C 1350
570
Specific Heat Capacity, J/kg-K 480
890
Thermal Conductivity, W/m-K 12
160
Thermal Expansion, µm/m-K 15
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.7
45
Electrical Conductivity: Equal Weight (Specific), % IACS 2.0
140

Otherwise Unclassified Properties

Base Metal Price, % relative 30
9.5
Density, g/cm3 8.0
2.9
Embodied Carbon, kg CO2/kg material 5.3
8.2
Embodied Energy, MJ/kg 75
150
Embodied Water, L/kg 200
1170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 190
21 to 28
Resilience: Unit (Modulus of Resilience), kJ/m3 95
94 to 480
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 24
48
Strength to Weight: Axial, points 22
22 to 32
Strength to Weight: Bending, points 20
29 to 37
Thermal Diffusivity, mm2/s 3.2
62
Thermal Shock Resistance, points 15
10 to 14

Alloy Composition

Aluminum (Al), % 0.2 to 0.5
92.2 to 98
Bismuth (Bi), % 0
0 to 0.7
Carbon (C), % 0.030 to 0.080
0
Chromium (Cr), % 19 to 22
0 to 0.3
Cobalt (Co), % 0 to 0.5
0
Copper (Cu), % 0 to 0.5
0 to 0.1
Iron (Fe), % 41.1 to 50.6
0 to 0.5
Lead (Pb), % 0
0.4 to 2.0
Magnesium (Mg), % 0
0.6 to 1.2
Manganese (Mn), % 0 to 1.5
0.4 to 1.0
Nickel (Ni), % 30 to 32.5
0
Niobium (Nb), % 0 to 0.1
0
Nitrogen (N), % 0 to 0.030
0
Phosphorus (P), % 0 to 0.015
0
Silicon (Si), % 0 to 0.7
0.6 to 1.4
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0.2 to 0.5
0 to 0.2
Zinc (Zn), % 0
0 to 0.3
Residuals, % 0
0 to 0.15