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2025 Aluminum vs. S15500 Stainless Steel

2025 aluminum belongs to the aluminum alloys classification, while S15500 stainless steel belongs to the iron 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 2025 aluminum and the bottom bar is S15500 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 110
290 to 430
Elastic (Young's, Tensile) Modulus, GPa 72
190
Elongation at Break, % 15
6.8 to 16
Fatigue Strength, MPa 130
350 to 650
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
75
Shear Strength, MPa 240
540 to 870
Tensile Strength: Ultimate (UTS), MPa 400
890 to 1490
Tensile Strength: Yield (Proof), MPa 260
590 to 1310

Thermal Properties

Latent Heat of Fusion, J/g 400
280
Maximum Temperature: Mechanical, °C 190
820
Melting Completion (Liquidus), °C 640
1430
Melting Onset (Solidus), °C 520
1380
Specific Heat Capacity, J/kg-K 870
480
Thermal Conductivity, W/m-K 150
17
Thermal Expansion, µm/m-K 23
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 40
2.2
Electrical Conductivity: Equal Weight (Specific), % IACS 120
2.5

Otherwise Unclassified Properties

Base Metal Price, % relative 10
13
Density, g/cm3 3.0
7.8
Embodied Carbon, kg CO2/kg material 7.9
2.7
Embodied Energy, MJ/kg 150
39
Embodied Water, L/kg 1130
130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 55
98 to 120
Resilience: Unit (Modulus of Resilience), kJ/m3 450
890 to 4460
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 46
25
Strength to Weight: Axial, points 37
32 to 53
Strength to Weight: Bending, points 40
26 to 37
Thermal Diffusivity, mm2/s 58
4.6
Thermal Shock Resistance, points 18
30 to 50

Alloy Composition

Aluminum (Al), % 90.9 to 95.2
0
Carbon (C), % 0
0 to 0.070
Chromium (Cr), % 0 to 0.1
14 to 15.5
Copper (Cu), % 3.9 to 5.0
2.5 to 4.5
Iron (Fe), % 0 to 1.0
71.9 to 79.9
Magnesium (Mg), % 0 to 0.050
0
Manganese (Mn), % 0.4 to 1.2
0 to 1.0
Nickel (Ni), % 0
3.5 to 5.5
Niobium (Nb), % 0
0.15 to 0.45
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0.5 to 1.2
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0