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S35315 Stainless Steel vs. 6005A Aluminum

S35315 stainless steel belongs to the iron alloys classification, while 6005A 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 S35315 stainless steel and the bottom bar is 6005A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
69
Elongation at Break, % 46
8.6 to 17
Fatigue Strength, MPa 280
55 to 110
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 78
26
Shear Strength, MPa 520
120 to 180
Tensile Strength: Ultimate (UTS), MPa 740
190 to 300
Tensile Strength: Yield (Proof), MPa 300
100 to 270

Thermal Properties

Latent Heat of Fusion, J/g 330
410
Maximum Temperature: Mechanical, °C 1100
170
Melting Completion (Liquidus), °C 1370
650
Melting Onset (Solidus), °C 1330
600
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 12
180 to 190
Thermal Expansion, µm/m-K 16
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.7
47 to 50
Electrical Conductivity: Equal Weight (Specific), % IACS 2.0
150 to 170

Otherwise Unclassified Properties

Base Metal Price, % relative 34
9.5
Density, g/cm3 7.9
2.7
Embodied Carbon, kg CO2/kg material 5.7
8.3
Embodied Energy, MJ/kg 81
150
Embodied Water, L/kg 220
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 270
24 to 29
Resilience: Unit (Modulus of Resilience), kJ/m3 230
76 to 530
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 26
20 to 30
Strength to Weight: Bending, points 23
27 to 36
Thermal Diffusivity, mm2/s 3.1
72 to 79
Thermal Shock Resistance, points 17
8.6 to 13

Alloy Composition

Aluminum (Al), % 0
96.5 to 99.1
Carbon (C), % 0.040 to 0.080
0
Cerium (Ce), % 0.030 to 0.1
0
Chromium (Cr), % 24 to 26
0 to 0.3
Copper (Cu), % 0
0 to 0.3
Iron (Fe), % 33.6 to 40.6
0 to 0.35
Magnesium (Mg), % 0
0.4 to 0.7
Manganese (Mn), % 0 to 2.0
0 to 0.5
Nickel (Ni), % 34 to 36
0
Nitrogen (N), % 0.12 to 0.18
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 1.2 to 2.0
0.5 to 0.9
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0 to 0.1
Zinc (Zn), % 0
0 to 0.2
Residuals, % 0
0 to 0.15