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EN 1.4310 Stainless Steel vs. EN AC-44000 Aluminum

EN 1.4310 stainless steel belongs to the iron alloys classification, while EN AC-44000 aluminum belongs to the aluminum 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 1.4310 stainless steel and the bottom bar is EN AC-44000 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 200 to 270
51
Elastic (Young's, Tensile) Modulus, GPa 200
71
Elongation at Break, % 14 to 45
7.3
Fatigue Strength, MPa 240 to 330
64
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
27
Tensile Strength: Ultimate (UTS), MPa 730 to 900
180
Tensile Strength: Yield (Proof), MPa 260 to 570
86

Thermal Properties

Latent Heat of Fusion, J/g 290
560
Maximum Temperature: Mechanical, °C 910
170
Melting Completion (Liquidus), °C 1420
590
Melting Onset (Solidus), °C 1380
590
Specific Heat Capacity, J/kg-K 480
910
Thermal Conductivity, W/m-K 15
140
Thermal Expansion, µm/m-K 18
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.4
36
Electrical Conductivity: Equal Weight (Specific), % IACS 2.7
130

Otherwise Unclassified Properties

Base Metal Price, % relative 14
9.5
Density, g/cm3 7.8
2.5
Embodied Carbon, kg CO2/kg material 2.9
7.8
Embodied Energy, MJ/kg 42
150
Embodied Water, L/kg 140
1070

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110 to 260
11
Resilience: Unit (Modulus of Resilience), kJ/m3 170 to 830
51
Stiffness to Weight: Axial, points 14
16
Stiffness to Weight: Bending, points 25
55
Strength to Weight: Axial, points 26 to 32
20
Strength to Weight: Bending, points 23 to 27
28
Thermal Diffusivity, mm2/s 4.0
61
Thermal Shock Resistance, points 15 to 18
8.4

Alloy Composition

Aluminum (Al), % 0
87.1 to 90
Carbon (C), % 0.050 to 0.15
0
Chromium (Cr), % 16 to 19
0
Copper (Cu), % 0
0 to 0.050
Iron (Fe), % 66.4 to 78
0 to 0.19
Magnesium (Mg), % 0
0 to 0.45
Manganese (Mn), % 0 to 2.0
0 to 0.1
Molybdenum (Mo), % 0 to 0.8
0
Nickel (Ni), % 6.0 to 9.5
0
Nitrogen (N), % 0 to 0.1
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 2.0
10 to 11.8
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
0 to 0.15
Zinc (Zn), % 0
0 to 0.070
Residuals, % 0
0 to 0.1