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S13800 Stainless Steel vs. 4032 Aluminum

S13800 stainless steel belongs to the iron alloys classification, while 4032 aluminum belongs to the aluminum 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 S13800 stainless steel and the bottom bar is 4032 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 290 to 480
120
Elastic (Young's, Tensile) Modulus, GPa 200
73
Elongation at Break, % 11 to 18
6.7
Fatigue Strength, MPa 410 to 870
110
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
28
Shear Strength, MPa 610 to 1030
260
Tensile Strength: Ultimate (UTS), MPa 980 to 1730
390
Tensile Strength: Yield (Proof), MPa 660 to 1580
320

Thermal Properties

Latent Heat of Fusion, J/g 280
570
Maximum Temperature: Mechanical, °C 810
180
Melting Completion (Liquidus), °C 1450
570
Melting Onset (Solidus), °C 1410
530
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 16
140
Thermal Expansion, µm/m-K 11
19

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.3
34
Electrical Conductivity: Equal Weight (Specific), % IACS 2.6
120

Otherwise Unclassified Properties

Base Metal Price, % relative 15
10
Density, g/cm3 7.9
2.6
Embodied Carbon, kg CO2/kg material 3.4
7.8
Embodied Energy, MJ/kg 46
140
Embodied Water, L/kg 140
1030

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 150 to 190
25
Resilience: Unit (Modulus of Resilience), kJ/m3 1090 to 5490
700
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 25
53
Strength to Weight: Axial, points 35 to 61
41
Strength to Weight: Bending, points 28 to 41
45
Thermal Diffusivity, mm2/s 4.3
59
Thermal Shock Resistance, points 33 to 58
20

Alloy Composition

Aluminum (Al), % 0.9 to 1.4
81.1 to 87.2
Carbon (C), % 0 to 0.050
0
Chromium (Cr), % 12.3 to 13.2
0 to 0.1
Copper (Cu), % 0
0.5 to 1.3
Iron (Fe), % 73.6 to 77.3
0 to 1.0
Magnesium (Mg), % 0
0.8 to 1.3
Manganese (Mn), % 0 to 0.2
0
Molybdenum (Mo), % 2.0 to 3.0
0
Nickel (Ni), % 7.5 to 8.5
0.5 to 1.3
Nitrogen (N), % 0 to 0.010
0
Phosphorus (P), % 0 to 0.010
0
Silicon (Si), % 0 to 0.1
11 to 13.5
Sulfur (S), % 0 to 0.0080
0
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15