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EN 1.4017 Stainless Steel vs. 7178 Aluminum

EN 1.4017 stainless steel belongs to the iron alloys classification, while 7178 aluminum belongs to the aluminum alloys. There are 30 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 1.4017 stainless steel and the bottom bar is 7178 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
71
Elongation at Break, % 14
4.5 to 12
Fatigue Strength, MPa 220
120 to 210
Poisson's Ratio 0.28
0.32
Shear Modulus, GPa 77
27
Shear Strength, MPa 350
140 to 380
Tensile Strength: Ultimate (UTS), MPa 580
240 to 640
Tensile Strength: Yield (Proof), MPa 390
120 to 560

Thermal Properties

Latent Heat of Fusion, J/g 280
370
Maximum Temperature: Mechanical, °C 870
180
Melting Completion (Liquidus), °C 1440
630
Melting Onset (Solidus), °C 1390
480
Specific Heat Capacity, J/kg-K 480
860
Thermal Conductivity, W/m-K 30
130
Thermal Expansion, µm/m-K 10
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.5
31
Electrical Conductivity: Equal Weight (Specific), % IACS 2.9
91

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
10
Density, g/cm3 7.7
3.1
Embodied Carbon, kg CO2/kg material 2.2
8.2
Embodied Energy, MJ/kg 31
150
Embodied Water, L/kg 120
1110

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 71
24 to 52
Resilience: Unit (Modulus of Resilience), kJ/m3 380
110 to 2220
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
45
Strength to Weight: Axial, points 21
21 to 58
Strength to Weight: Bending, points 20
28 to 54
Thermal Diffusivity, mm2/s 8.1
47
Thermal Shock Resistance, points 20
10 to 28

Alloy Composition

Aluminum (Al), % 0
85.4 to 89.5
Carbon (C), % 0 to 0.080
0
Chromium (Cr), % 16 to 18
0.18 to 0.28
Copper (Cu), % 0
1.6 to 2.4
Iron (Fe), % 78.3 to 82.8
0 to 0.5
Magnesium (Mg), % 0
2.4 to 3.1
Manganese (Mn), % 0 to 1.0
0 to 0.3
Nickel (Ni), % 1.2 to 1.6
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 1.0
0 to 0.4
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0
6.3 to 7.3
Residuals, % 0
0 to 0.15