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S15500 Stainless Steel vs. 7076 Aluminum

S15500 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 (5, 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 7076 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 290 to 430
160
Elastic (Young's, Tensile) Modulus, GPa 190
70
Elongation at Break, % 6.8 to 16
6.2
Fatigue Strength, MPa 350 to 650
170
Poisson's Ratio 0.28
0.32
Shear Modulus, GPa 75
27
Shear Strength, MPa 540 to 870
310
Tensile Strength: Ultimate (UTS), MPa 890 to 1490
530
Tensile Strength: Yield (Proof), MPa 590 to 1310
460

Thermal Properties

Latent Heat of Fusion, J/g 280
380
Maximum Temperature: Mechanical, °C 820
170
Melting Completion (Liquidus), °C 1430
630
Melting Onset (Solidus), °C 1380
460
Specific Heat Capacity, J/kg-K 480
860
Thermal Conductivity, W/m-K 17
140
Thermal Expansion, µm/m-K 11
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.2
35
Electrical Conductivity: Equal Weight (Specific), % IACS 2.5
100

Otherwise Unclassified Properties

Base Metal Price, % relative 13
9.5
Density, g/cm3 7.8
3.0
Embodied Carbon, kg CO2/kg material 2.7
8.0
Embodied Energy, MJ/kg 39
150
Embodied Water, L/kg 130
1110

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 98 to 120
31
Resilience: Unit (Modulus of Resilience), kJ/m3 890 to 4460
1510
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
45
Strength to Weight: Axial, points 32 to 53
49
Strength to Weight: Bending, points 26 to 37
48
Thermal Diffusivity, mm2/s 4.6
54
Thermal Shock Resistance, points 30 to 50
23

Alloy Composition


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Aluminum (Al), % 0
86.9 to 91.2
Carbon (C), % 0 to 0.070
0
Chromium (Cr), % 14 to 15.5
0
Copper (Cu), % 2.5 to 4.5
0.3 to 1.0
Iron (Fe), % 71.9 to 79.9
0 to 0.6
Magnesium (Mg), % 0
1.2 to 2.0
Manganese (Mn), % 0 to 1.0
0.3 to 0.8
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
0 to 0.4
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0
7.0 to 8.0
Residuals, % 0
0 to 0.15