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5005 Aluminum vs. S35315 Stainless Steel

5005 aluminum belongs to the aluminum alloys classification, while S35315 stainless steel belongs to the iron alloys. There are 31 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 5005 aluminum and the bottom bar is S35315 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 28 to 64
190
Elastic (Young's, Tensile) Modulus, GPa 68
200
Elongation at Break, % 1.1 to 23
46
Fatigue Strength, MPa 38 to 86
280
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
78
Shear Strength, MPa 70 to 130
520
Tensile Strength: Ultimate (UTS), MPa 110 to 230
740
Tensile Strength: Yield (Proof), MPa 41 to 210
300

Thermal Properties

Latent Heat of Fusion, J/g 400
330
Maximum Temperature: Mechanical, °C 180
1100
Melting Completion (Liquidus), °C 650
1370
Melting Onset (Solidus), °C 630
1330
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 200
12
Thermal Expansion, µm/m-K 24
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 52
1.7
Electrical Conductivity: Equal Weight (Specific), % IACS 170
2.0

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
34
Density, g/cm3 2.7
7.9
Embodied Carbon, kg CO2/kg material 8.3
5.7
Embodied Energy, MJ/kg 150
81
Embodied Water, L/kg 1190
220

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.3 to 22
270
Resilience: Unit (Modulus of Resilience), kJ/m3 12 to 320
230
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 11 to 23
26
Strength to Weight: Bending, points 19 to 31
23
Thermal Diffusivity, mm2/s 82
3.1
Thermal Shock Resistance, points 4.9 to 10
17

Alloy Composition

Aluminum (Al), % 97 to 99.5
0
Carbon (C), % 0
0.040 to 0.080
Cerium (Ce), % 0
0.030 to 0.1
Chromium (Cr), % 0 to 0.1
24 to 26
Copper (Cu), % 0 to 0.2
0
Iron (Fe), % 0 to 0.7
33.6 to 40.6
Magnesium (Mg), % 0.5 to 1.1
0
Manganese (Mn), % 0 to 0.2
0 to 2.0
Nickel (Ni), % 0
34 to 36
Nitrogen (N), % 0
0.12 to 0.18
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.3
1.2 to 2.0
Sulfur (S), % 0
0 to 0.030
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0