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EN 1.4913 Stainless Steel vs. 5005A Aluminum

EN 1.4913 stainless steel belongs to the iron alloys classification, while 5005A 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 1.4913 stainless steel and the bottom bar is 5005A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
68
Elongation at Break, % 14 to 22
1.1 to 21
Fatigue Strength, MPa 320 to 480
38 to 82
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 75
26
Shear Strength, MPa 550 to 590
71 to 130
Tensile Strength: Ultimate (UTS), MPa 870 to 980
110 to 230
Tensile Strength: Yield (Proof), MPa 480 to 850
43 to 210

Thermal Properties

Latent Heat of Fusion, J/g 270
400
Maximum Temperature: Mechanical, °C 700
180
Melting Completion (Liquidus), °C 1460
660
Melting Onset (Solidus), °C 1410
630
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 24
200
Thermal Expansion, µm/m-K 11
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.9
52
Electrical Conductivity: Equal Weight (Specific), % IACS 3.3
170

Otherwise Unclassified Properties

Base Metal Price, % relative 9.0
9.5
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 2.9
8.3
Embodied Energy, MJ/kg 41
150
Embodied Water, L/kg 97
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 130 to 160
2.0 to 19
Resilience: Unit (Modulus of Resilience), kJ/m3 600 to 1860
14 to 310
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 31 to 35
12 to 24
Strength to Weight: Bending, points 26 to 28
19 to 31
Thermal Diffusivity, mm2/s 6.5
82
Thermal Shock Resistance, points 31 to 34
5.0 to 10

Alloy Composition

Aluminum (Al), % 0 to 0.020
97.5 to 99.3
Boron (B), % 0 to 0.0015
0
Carbon (C), % 0.17 to 0.23
0
Chromium (Cr), % 10 to 11.5
0 to 0.1
Copper (Cu), % 0
0 to 0.050
Iron (Fe), % 84.5 to 88.3
0 to 0.45
Magnesium (Mg), % 0
0.7 to 1.1
Manganese (Mn), % 0.4 to 0.9
0 to 0.15
Molybdenum (Mo), % 0.5 to 0.8
0
Nickel (Ni), % 0.2 to 0.6
0
Niobium (Nb), % 0.25 to 0.55
0
Nitrogen (N), % 0.050 to 0.1
0
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0 to 0.5
0 to 0.3
Sulfur (S), % 0 to 0.015
0
Vanadium (V), % 0.1 to 0.3
0
Zinc (Zn), % 0
0 to 0.2
Residuals, % 0
0 to 0.15

Comparable Variants