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EN 1.4982 Stainless Steel vs. 7178 Aluminum

EN 1.4982 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 (4, 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 1.4982 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, % 28
4.5 to 12
Fatigue Strength, MPa 420
120 to 210
Poisson's Ratio 0.28
0.32
Shear Modulus, GPa 76
27
Shear Strength, MPa 490
140 to 380
Tensile Strength: Ultimate (UTS), MPa 750
240 to 640
Tensile Strength: Yield (Proof), MPa 570
120 to 560

Thermal Properties

Latent Heat of Fusion, J/g 290
370
Maximum Temperature: Mechanical, °C 860
180
Melting Completion (Liquidus), °C 1430
630
Melting Onset (Solidus), °C 1390
480
Specific Heat Capacity, J/kg-K 470
860
Thermal Conductivity, W/m-K 13
130
Thermal Expansion, µm/m-K 16
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.3
31
Electrical Conductivity: Equal Weight (Specific), % IACS 2.7
91

Otherwise Unclassified Properties

Base Metal Price, % relative 22
10
Density, g/cm3 7.8
3.1
Embodied Carbon, kg CO2/kg material 4.9
8.2
Embodied Energy, MJ/kg 71
150
Embodied Water, L/kg 150
1110

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 190
24 to 52
Resilience: Unit (Modulus of Resilience), kJ/m3 830
110 to 2220
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
45
Strength to Weight: Axial, points 27
21 to 58
Strength to Weight: Bending, points 23
28 to 54
Thermal Diffusivity, mm2/s 3.4
47
Thermal Shock Resistance, points 17
10 to 28

Alloy Composition


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Aluminum (Al), % 0
85.4 to 89.5
Boron (B), % 0.0030 to 0.0090
0
Carbon (C), % 0.070 to 0.13
0
Chromium (Cr), % 14 to 16
0.18 to 0.28
Copper (Cu), % 0
1.6 to 2.4
Iron (Fe), % 61.8 to 69.7
0 to 0.5
Magnesium (Mg), % 0
2.4 to 3.1
Manganese (Mn), % 5.5 to 7.0
0 to 0.3
Molybdenum (Mo), % 0.8 to 1.2
0
Nickel (Ni), % 9.0 to 11
0
Niobium (Nb), % 0.75 to 1.3
0
Nitrogen (N), % 0 to 0.1
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 1.0
0 to 0.4
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0 to 0.2
Vanadium (V), % 0.15 to 0.4
0
Zinc (Zn), % 0
6.3 to 7.3
Residuals, % 0
0 to 0.15