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6013 Aluminum vs. S17400 Stainless Steel

6013 aluminum belongs to the aluminum alloys classification, while S17400 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (6, 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 6013 aluminum and the bottom bar is S17400 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
190
Elongation at Break, % 3.4 to 22
11 to 21
Fatigue Strength, MPa 98 to 140
380 to 670
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
75
Shear Strength, MPa 190 to 240
570 to 830
Tensile Strength: Ultimate (UTS), MPa 310 to 410
910 to 1390
Tensile Strength: Yield (Proof), MPa 170 to 350
580 to 1250

Thermal Properties

Latent Heat of Fusion, J/g 410
280
Maximum Temperature: Mechanical, °C 160
850
Melting Completion (Liquidus), °C 650
1440
Melting Onset (Solidus), °C 580
1400
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 150
17
Thermal Expansion, µm/m-K 23
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 38
2.3
Electrical Conductivity: Equal Weight (Specific), % IACS 120
2.6

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
14
Density, g/cm3 2.8
7.8
Embodied Carbon, kg CO2/kg material 8.3
2.7
Embodied Energy, MJ/kg 150
39
Embodied Water, L/kg 1170
130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 13 to 58
140 to 160
Resilience: Unit (Modulus of Resilience), kJ/m3 200 to 900
880 to 4060
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 49
25
Strength to Weight: Axial, points 31 to 41
32 to 49
Strength to Weight: Bending, points 37 to 44
27 to 35
Thermal Diffusivity, mm2/s 60
4.5
Thermal Shock Resistance, points 14 to 18
30 to 46

Alloy Composition

Aluminum (Al), % 94.8 to 97.8
0
Carbon (C), % 0
0 to 0.070
Chromium (Cr), % 0 to 0.1
15 to 17
Copper (Cu), % 0.6 to 1.1
3.0 to 5.0
Iron (Fe), % 0 to 0.5
70.4 to 78.9
Magnesium (Mg), % 0.8 to 1.2
0
Manganese (Mn), % 0.2 to 0.8
0 to 1.0
Nickel (Ni), % 0
3.0 to 5.0
Niobium (Nb), % 0
0.15 to 0.45
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0.6 to 1.0
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.1
0
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0