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S13800 Stainless Steel vs. 4007 Aluminum

S13800 stainless steel belongs to the iron alloys classification, while 4007 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 4007 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 290 to 480
32 to 44
Elastic (Young's, Tensile) Modulus, GPa 200
71
Elongation at Break, % 11 to 18
5.1 to 23
Fatigue Strength, MPa 410 to 870
46 to 88
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
27
Shear Strength, MPa 610 to 1030
80 to 90
Tensile Strength: Ultimate (UTS), MPa 980 to 1730
130 to 160
Tensile Strength: Yield (Proof), MPa 660 to 1580
50 to 120

Thermal Properties

Latent Heat of Fusion, J/g 280
410
Maximum Temperature: Mechanical, °C 810
170
Melting Completion (Liquidus), °C 1450
650
Melting Onset (Solidus), °C 1410
590
Specific Heat Capacity, J/kg-K 470
890
Thermal Conductivity, W/m-K 16
170
Thermal Expansion, µm/m-K 11
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.3
42
Electrical Conductivity: Equal Weight (Specific), % IACS 2.6
140

Otherwise Unclassified Properties

Base Metal Price, % relative 15
9.5
Density, g/cm3 7.9
2.8
Embodied Carbon, kg CO2/kg material 3.4
8.1
Embodied Energy, MJ/kg 46
150
Embodied Water, L/kg 140
1160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 150 to 190
7.4 to 23
Resilience: Unit (Modulus of Resilience), kJ/m3 1090 to 5490
18 to 110
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
49
Strength to Weight: Axial, points 35 to 61
12 to 15
Strength to Weight: Bending, points 28 to 41
20 to 23
Thermal Diffusivity, mm2/s 4.3
67
Thermal Shock Resistance, points 33 to 58
5.5 to 6.7

Alloy Composition


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Aluminum (Al), % 0.9 to 1.4
94.1 to 97.6
Carbon (C), % 0 to 0.050
0
Chromium (Cr), % 12.3 to 13.2
0.050 to 0.25
Cobalt (Co), % 0
0 to 0.050
Copper (Cu), % 0
0 to 0.2
Iron (Fe), % 73.6 to 77.3
0.4 to 1.0
Magnesium (Mg), % 0
0 to 0.2
Manganese (Mn), % 0 to 0.2
0.8 to 1.5
Molybdenum (Mo), % 2.0 to 3.0
0
Nickel (Ni), % 7.5 to 8.5
0.15 to 0.7
Nitrogen (N), % 0 to 0.010
0
Phosphorus (P), % 0 to 0.010
0
Silicon (Si), % 0 to 0.1
1.0 to 1.7
Sulfur (S), % 0 to 0.0080
0
Titanium (Ti), % 0
0 to 0.1
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15