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EN 1.4110 Stainless Steel vs. 7108A Aluminum

EN 1.4110 stainless steel belongs to the iron alloys classification, while 7108A 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 1.4110 stainless steel and the bottom bar is 7108A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
69
Elongation at Break, % 11 to 14
11 to 13
Fatigue Strength, MPa 250 to 730
120 to 130
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
26
Shear Strength, MPa 470 to 1030
210
Tensile Strength: Ultimate (UTS), MPa 770 to 1720
350
Tensile Strength: Yield (Proof), MPa 430 to 1330
290 to 300

Thermal Properties

Latent Heat of Fusion, J/g 280
380
Maximum Temperature: Mechanical, °C 790
210
Melting Completion (Liquidus), °C 1440
630
Melting Onset (Solidus), °C 1400
520
Specific Heat Capacity, J/kg-K 480
870
Thermal Conductivity, W/m-K 30
150
Thermal Expansion, µm/m-K 11
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.8
36
Electrical Conductivity: Equal Weight (Specific), % IACS 3.2
110

Otherwise Unclassified Properties

Base Metal Price, % relative 8.0
10
Density, g/cm3 7.7
2.9
Embodied Carbon, kg CO2/kg material 2.3
8.3
Embodied Energy, MJ/kg 33
150
Embodied Water, L/kg 110
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 90 to 180
38 to 44
Resilience: Unit (Modulus of Resilience), kJ/m3 480 to 4550
610 to 640
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
47
Strength to Weight: Axial, points 28 to 62
33 to 34
Strength to Weight: Bending, points 24 to 41
38
Thermal Diffusivity, mm2/s 8.1
59
Thermal Shock Resistance, points 27 to 60
15 to 16

Alloy Composition

Aluminum (Al), % 0
91.6 to 94.4
Carbon (C), % 0.48 to 0.6
0
Chromium (Cr), % 13 to 15
0 to 0.040
Copper (Cu), % 0
0 to 0.050
Gallium (Ga), % 0
0 to 0.030
Iron (Fe), % 81.4 to 86
0 to 0.3
Magnesium (Mg), % 0
0.7 to 1.5
Manganese (Mn), % 0 to 1.0
0 to 0.050
Molybdenum (Mo), % 0.5 to 0.8
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 1.0
0 to 0.2
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
0 to 0.030
Vanadium (V), % 0 to 0.15
0
Zinc (Zn), % 0
4.8 to 5.8
Zirconium (Zr), % 0
0.15 to 0.25
Residuals, % 0
0 to 0.15