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EN 1.4542 Stainless Steel vs. A413.0 Aluminum

EN 1.4542 stainless steel belongs to the iron alloys classification, while A413.0 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 1.4542 stainless steel and the bottom bar is A413.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
73
Elongation at Break, % 5.7 to 20
3.5
Fatigue Strength, MPa 370 to 640
130
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
27
Shear Strength, MPa 550 to 860
170
Tensile Strength: Ultimate (UTS), MPa 880 to 1470
240
Tensile Strength: Yield (Proof), MPa 580 to 1300
130

Thermal Properties

Latent Heat of Fusion, J/g 280
570
Maximum Temperature: Mechanical, °C 860
170
Melting Completion (Liquidus), °C 1430
590
Melting Onset (Solidus), °C 1380
580
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 16
120
Thermal Expansion, µm/m-K 11
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.4
31
Electrical Conductivity: Equal Weight (Specific), % IACS 2.8
110

Otherwise Unclassified Properties

Base Metal Price, % relative 13
9.5
Density, g/cm3 7.8
2.6
Embodied Carbon, kg CO2/kg material 2.7
7.6
Embodied Energy, MJ/kg 39
140
Embodied Water, L/kg 130
1040

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 62 to 160
7.1
Resilience: Unit (Modulus of Resilience), kJ/m3 880 to 4360
120
Stiffness to Weight: Axial, points 14
16
Stiffness to Weight: Bending, points 25
54
Strength to Weight: Axial, points 31 to 52
25
Strength to Weight: Bending, points 26 to 37
33
Thermal Diffusivity, mm2/s 4.3
52
Thermal Shock Resistance, points 29 to 49
11

Alloy Composition


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Aluminum (Al), % 0
82.9 to 89
Carbon (C), % 0 to 0.070
0
Chromium (Cr), % 15 to 17
0
Copper (Cu), % 3.0 to 5.0
0 to 1.0
Iron (Fe), % 69.6 to 79
0 to 1.3
Magnesium (Mg), % 0
0 to 0.1
Manganese (Mn), % 0 to 1.5
0 to 0.35
Molybdenum (Mo), % 0 to 0.6
0
Nickel (Ni), % 3.0 to 5.0
0 to 0.5
Niobium (Nb), % 0 to 0.45
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 0.7
11 to 13
Sulfur (S), % 0 to 0.015
0
Tin (Sn), % 0
0 to 0.15
Zinc (Zn), % 0
0 to 0.5
Residuals, % 0
0 to 0.25