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EN 1.4542 Stainless Steel vs. 705.0 Aluminum

EN 1.4542 stainless steel belongs to the iron alloys classification, while 705.0 aluminum belongs to the aluminum alloys. There are 29 material properties with values for both materials. Properties with values for just one material (5, 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 705.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
69
Elongation at Break, % 5.7 to 20
8.4 to 10
Fatigue Strength, MPa 370 to 640
63 to 98
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
26
Tensile Strength: Ultimate (UTS), MPa 880 to 1470
240 to 260
Tensile Strength: Yield (Proof), MPa 580 to 1300
130

Thermal Properties

Latent Heat of Fusion, J/g 280
390
Maximum Temperature: Mechanical, °C 860
180
Melting Completion (Liquidus), °C 1430
640
Melting Onset (Solidus), °C 1380
610
Specific Heat Capacity, J/kg-K 470
890
Thermal Conductivity, W/m-K 16
140
Thermal Expansion, µm/m-K 11
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.4
34
Electrical Conductivity: Equal Weight (Specific), % IACS 2.8
110

Otherwise Unclassified Properties

Base Metal Price, % relative 13
9.5
Density, g/cm3 7.8
2.8
Embodied Carbon, kg CO2/kg material 2.7
8.4
Embodied Energy, MJ/kg 39
150
Embodied Water, L/kg 130
1170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 62 to 160
18 to 20
Resilience: Unit (Modulus of Resilience), kJ/m3 880 to 4360
120 to 130
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
49
Strength to Weight: Axial, points 31 to 52
24 to 26
Strength to Weight: Bending, points 26 to 37
31 to 32
Thermal Diffusivity, mm2/s 4.3
55
Thermal Shock Resistance, points 29 to 49
11

Alloy Composition


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Aluminum (Al), % 0
92.3 to 98.6
Carbon (C), % 0 to 0.070
0
Chromium (Cr), % 15 to 17
0 to 0.4
Copper (Cu), % 3.0 to 5.0
0 to 0.2
Iron (Fe), % 69.6 to 79
0 to 0.8
Magnesium (Mg), % 0
1.4 to 1.8
Manganese (Mn), % 0 to 1.5
0 to 0.6
Molybdenum (Mo), % 0 to 0.6
0
Nickel (Ni), % 3.0 to 5.0
0
Niobium (Nb), % 0 to 0.45
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 0.7
0 to 0.2
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 0
0 to 3.3
Residuals, % 0
0 to 0.15