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EN 1.4962 Stainless Steel vs. 360.0 Aluminum

EN 1.4962 stainless steel belongs to the iron alloys classification, while 360.0 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 1.4962 stainless steel and the bottom bar is 360.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 190 to 210
75
Elastic (Young's, Tensile) Modulus, GPa 200
72
Elongation at Break, % 22 to 34
2.5
Fatigue Strength, MPa 210 to 330
140
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
27
Shear Strength, MPa 420 to 440
190
Tensile Strength: Ultimate (UTS), MPa 630 to 690
300
Tensile Strength: Yield (Proof), MPa 260 to 490
170

Thermal Properties

Latent Heat of Fusion, J/g 280
530
Maximum Temperature: Mechanical, °C 910
170
Melting Completion (Liquidus), °C 1480
590
Melting Onset (Solidus), °C 1440
570
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 14
130
Thermal Expansion, µm/m-K 16
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.3
34
Electrical Conductivity: Equal Weight (Specific), % IACS 2.6
110

Otherwise Unclassified Properties

Base Metal Price, % relative 23
9.5
Density, g/cm3 8.1
2.6
Embodied Carbon, kg CO2/kg material 4.1
7.8
Embodied Energy, MJ/kg 59
140
Embodied Water, L/kg 150
1070

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140 to 170
6.4
Resilience: Unit (Modulus of Resilience), kJ/m3 170 to 610
200
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 24
53
Strength to Weight: Axial, points 21 to 24
32
Strength to Weight: Bending, points 20 to 21
38
Thermal Diffusivity, mm2/s 3.7
55
Thermal Shock Resistance, points 14 to 16
14

Alloy Composition

Aluminum (Al), % 0
85.1 to 90.6
Boron (B), % 0.0015 to 0.0060
0
Carbon (C), % 0.070 to 0.15
0
Chromium (Cr), % 15.5 to 17.5
0
Copper (Cu), % 0
0 to 0.6
Iron (Fe), % 62.1 to 69
0 to 2.0
Magnesium (Mg), % 0
0.4 to 0.6
Manganese (Mn), % 0 to 1.5
0 to 0.35
Nickel (Ni), % 12.5 to 14.5
0 to 0.5
Phosphorus (P), % 0 to 0.035
0
Silicon (Si), % 0 to 0.5
9.0 to 10
Sulfur (S), % 0 to 0.015
0
Tin (Sn), % 0
0 to 0.15
Titanium (Ti), % 0.4 to 0.7
0
Tungsten (W), % 2.5 to 3.0
0
Zinc (Zn), % 0
0 to 0.5
Residuals, % 0
0 to 0.25