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S15500 Stainless Steel vs. 390.0 Aluminum

S15500 stainless steel belongs to the iron alloys classification, while 390.0 aluminum belongs to the aluminum 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 S15500 stainless steel and the bottom bar is 390.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 290 to 430
120
Elastic (Young's, Tensile) Modulus, GPa 190
75
Elongation at Break, % 6.8 to 16
1.0
Fatigue Strength, MPa 350 to 650
76 to 110
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 75
28
Tensile Strength: Ultimate (UTS), MPa 890 to 1490
280 to 300
Tensile Strength: Yield (Proof), MPa 590 to 1310
240 to 270

Thermal Properties

Latent Heat of Fusion, J/g 280
640
Maximum Temperature: Mechanical, °C 820
170
Melting Completion (Liquidus), °C 1430
650
Melting Onset (Solidus), °C 1380
560
Specific Heat Capacity, J/kg-K 480
880
Thermal Conductivity, W/m-K 17
130
Thermal Expansion, µm/m-K 11
18

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.2
24 to 25
Electrical Conductivity: Equal Weight (Specific), % IACS 2.5
79 to 83

Otherwise Unclassified Properties

Base Metal Price, % relative 13
11
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 2.7
7.3
Embodied Energy, MJ/kg 39
130
Embodied Water, L/kg 130
950

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 98 to 120
2.7 to 2.9
Resilience: Unit (Modulus of Resilience), kJ/m3 890 to 4460
380 to 470
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 25
52
Strength to Weight: Axial, points 32 to 53
28 to 30
Strength to Weight: Bending, points 26 to 37
35 to 36
Thermal Diffusivity, mm2/s 4.6
56
Thermal Shock Resistance, points 30 to 50
14 to 15

Alloy Composition

Aluminum (Al), % 0
74.5 to 79.6
Carbon (C), % 0 to 0.070
0
Chromium (Cr), % 14 to 15.5
0
Copper (Cu), % 2.5 to 4.5
4.0 to 5.0
Iron (Fe), % 71.9 to 79.9
0 to 1.3
Magnesium (Mg), % 0
0.45 to 0.65
Manganese (Mn), % 0 to 1.0
0 to 0.1
Nickel (Ni), % 3.5 to 5.5
0
Niobium (Nb), % 0.15 to 0.45
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 1.0
16 to 18
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.2