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EN 1.4062 Stainless Steel vs. A384.0 Aluminum

EN 1.4062 stainless steel belongs to the iron alloys classification, while A384.0 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 1.4062 stainless steel and the bottom bar is A384.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
74
Elongation at Break, % 23 to 34
2.5
Fatigue Strength, MPa 410 to 420
140
Poisson's Ratio 0.27
0.33
Shear Modulus, GPa 79
28
Shear Strength, MPa 510
200
Tensile Strength: Ultimate (UTS), MPa 770 to 800
330
Tensile Strength: Yield (Proof), MPa 530 to 600
170

Thermal Properties

Latent Heat of Fusion, J/g 290
550
Maximum Temperature: Mechanical, °C 1030
170
Melting Completion (Liquidus), °C 1430
610
Melting Onset (Solidus), °C 1380
510
Specific Heat Capacity, J/kg-K 480
880
Thermal Conductivity, W/m-K 15
96
Thermal Expansion, µm/m-K 13
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.1
23
Electrical Conductivity: Equal Weight (Specific), % IACS 2.4
73

Otherwise Unclassified Properties

Base Metal Price, % relative 12
11
Density, g/cm3 7.7
2.8
Embodied Carbon, kg CO2/kg material 2.6
7.5
Embodied Energy, MJ/kg 37
140
Embodied Water, L/kg 150
1010

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 170 to 230
6.9
Resilience: Unit (Modulus of Resilience), kJ/m3 690 to 910
180
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 28 to 29
32
Strength to Weight: Bending, points 24 to 25
38
Thermal Diffusivity, mm2/s 4.0
39
Thermal Shock Resistance, points 21 to 22
15

Alloy Composition


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Aluminum (Al), % 0
79.3 to 86.5
Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 21.5 to 24
0
Copper (Cu), % 0
3.0 to 4.5
Iron (Fe), % 69.3 to 77.3
0 to 1.3
Magnesium (Mg), % 0
0 to 0.1
Manganese (Mn), % 0 to 2.0
0 to 0.5
Molybdenum (Mo), % 0 to 0.45
0
Nickel (Ni), % 1.0 to 2.9
0 to 0.5
Nitrogen (N), % 0.16 to 0.28
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 1.0
10.5 to 12
Sulfur (S), % 0 to 0.010
0
Tin (Sn), % 0
0 to 0.35
Zinc (Zn), % 0
0 to 1.0
Residuals, % 0
0 to 0.5