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EN 1.4945 Stainless Steel vs. B535.0 Aluminum

EN 1.4945 stainless steel belongs to the iron alloys classification, while B535.0 aluminum belongs to the aluminum alloys. There are 31 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 1.4945 stainless steel and the bottom bar is B535.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 200 to 220
65
Elastic (Young's, Tensile) Modulus, GPa 200
66
Elongation at Break, % 19 to 34
10
Fatigue Strength, MPa 230 to 350
62
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
25
Shear Strength, MPa 430 to 460
210
Tensile Strength: Ultimate (UTS), MPa 640 to 740
260
Tensile Strength: Yield (Proof), MPa 290 to 550
130

Thermal Properties

Latent Heat of Fusion, J/g 290
390
Maximum Temperature: Mechanical, °C 920
170
Melting Completion (Liquidus), °C 1490
630
Melting Onset (Solidus), °C 1440
550
Specific Heat Capacity, J/kg-K 470
910
Thermal Conductivity, W/m-K 14
96
Thermal Expansion, µm/m-K 17
25

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.9
24
Electrical Conductivity: Equal Weight (Specific), % IACS 3.2
82

Otherwise Unclassified Properties

Base Metal Price, % relative 30
9.5
Density, g/cm3 8.1
2.6
Embodied Carbon, kg CO2/kg material 5.0
9.4
Embodied Energy, MJ/kg 73
160
Embodied Water, L/kg 150
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 130 to 180
22
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 760
130
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 24
51
Strength to Weight: Axial, points 22 to 25
28
Strength to Weight: Bending, points 20 to 22
35
Thermal Diffusivity, mm2/s 3.7
40
Thermal Shock Resistance, points 14 to 16
11

Alloy Composition

Aluminum (Al), % 0
91.7 to 93.4
Carbon (C), % 0.040 to 0.1
0
Chromium (Cr), % 15.5 to 17.5
0
Copper (Cu), % 0
0 to 0.1
Iron (Fe), % 57.9 to 65.7
0 to 0.15
Magnesium (Mg), % 0
6.5 to 7.5
Manganese (Mn), % 0 to 1.5
0 to 0.050
Nickel (Ni), % 15.5 to 17.5
0
Niobium (Nb), % 0.4 to 1.2
0
Nitrogen (N), % 0.060 to 0.14
0
Phosphorus (P), % 0 to 0.035
0
Silicon (Si), % 0.3 to 0.6
0 to 0.15
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
0.1 to 0.25
Tungsten (W), % 2.5 to 3.5
0
Residuals, % 0
0 to 0.15