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EN 1.4935 Stainless Steel vs. 8011A Aluminum

EN 1.4935 stainless steel belongs to the iron alloys classification, while 8011A aluminum belongs to the aluminum alloys. There are 29 material properties with values for both materials. Properties with values for just one material (4, 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 1.4935 stainless steel and the bottom bar is 8011A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
69
Elongation at Break, % 16 to 18
1.7 to 28
Fatigue Strength, MPa 350 to 400
33 to 76
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
26
Tensile Strength: Ultimate (UTS), MPa 780 to 880
100 to 180
Tensile Strength: Yield (Proof), MPa 570 to 670
34 to 170

Thermal Properties

Latent Heat of Fusion, J/g 270
400
Maximum Temperature: Mechanical, °C 740
170
Melting Completion (Liquidus), °C 1460
650
Melting Onset (Solidus), °C 1420
630
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 24
210
Thermal Expansion, µm/m-K 11
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.9
56
Electrical Conductivity: Equal Weight (Specific), % IACS 3.3
180

Otherwise Unclassified Properties

Base Metal Price, % relative 9.0
9.0
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 2.9
8.2
Embodied Energy, MJ/kg 42
150
Embodied Water, L/kg 100
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 130
3.0 to 22
Resilience: Unit (Modulus of Resilience), kJ/m3 830 to 1160
8.2 to 200
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 28 to 31
11 to 18
Strength to Weight: Bending, points 24 to 26
18 to 26
Thermal Diffusivity, mm2/s 6.5
86
Thermal Shock Resistance, points 27 to 30
4.6 to 8.1

Alloy Composition

Aluminum (Al), % 0
97.5 to 99.1
Carbon (C), % 0.17 to 0.24
0
Chromium (Cr), % 11 to 12.5
0 to 0.1
Copper (Cu), % 0
0 to 0.1
Iron (Fe), % 83 to 86.7
0.5 to 1.0
Magnesium (Mg), % 0
0 to 0.1
Manganese (Mn), % 0.3 to 0.8
0 to 0.1
Molybdenum (Mo), % 0.8 to 1.2
0
Nickel (Ni), % 0.3 to 0.8
0
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0.1 to 0.5
0.4 to 0.8
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
0 to 0.050
Tungsten (W), % 0.4 to 0.6
0
Vanadium (V), % 0.2 to 0.35
0
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15

Comparable Variants