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S13800 Stainless Steel vs. 7076 Aluminum

S13800 stainless steel belongs to the iron alloys classification, while 7076 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 7076 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 290 to 480
160
Elastic (Young's, Tensile) Modulus, GPa 200
70
Elongation at Break, % 11 to 18
6.2
Fatigue Strength, MPa 410 to 870
170
Poisson's Ratio 0.28
0.32
Shear Modulus, GPa 77
27
Shear Strength, MPa 610 to 1030
310
Tensile Strength: Ultimate (UTS), MPa 980 to 1730
530
Tensile Strength: Yield (Proof), MPa 660 to 1580
460

Thermal Properties

Latent Heat of Fusion, J/g 280
380
Maximum Temperature: Mechanical, °C 810
170
Melting Completion (Liquidus), °C 1450
630
Melting Onset (Solidus), °C 1410
460
Specific Heat Capacity, J/kg-K 470
860
Thermal Conductivity, W/m-K 16
140
Thermal Expansion, µm/m-K 11
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.3
35
Electrical Conductivity: Equal Weight (Specific), % IACS 2.6
100

Otherwise Unclassified Properties

Base Metal Price, % relative 15
9.5
Density, g/cm3 7.9
3.0
Embodied Carbon, kg CO2/kg material 3.4
8.0
Embodied Energy, MJ/kg 46
150
Embodied Water, L/kg 140
1110

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 150 to 190
31
Resilience: Unit (Modulus of Resilience), kJ/m3 1090 to 5490
1510
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
45
Strength to Weight: Axial, points 35 to 61
49
Strength to Weight: Bending, points 28 to 41
48
Thermal Diffusivity, mm2/s 4.3
54
Thermal Shock Resistance, points 33 to 58
23

Alloy Composition


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Aluminum (Al), % 0.9 to 1.4
86.9 to 91.2
Carbon (C), % 0 to 0.050
0
Chromium (Cr), % 12.3 to 13.2
0
Copper (Cu), % 0
0.3 to 1.0
Iron (Fe), % 73.6 to 77.3
0 to 0.6
Magnesium (Mg), % 0
1.2 to 2.0
Manganese (Mn), % 0 to 0.2
0.3 to 0.8
Molybdenum (Mo), % 2.0 to 3.0
0
Nickel (Ni), % 7.5 to 8.5
0
Nitrogen (N), % 0 to 0.010
0
Phosphorus (P), % 0 to 0.010
0
Silicon (Si), % 0 to 0.1
0 to 0.4
Sulfur (S), % 0 to 0.0080
0
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0
7.0 to 8.0
Residuals, % 0
0 to 0.15