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EN 1.4945 Stainless Steel vs. 2025 Aluminum

EN 1.4945 stainless steel belongs to the iron alloys classification, while 2025 aluminum belongs to the aluminum alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, 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 EN 1.4945 stainless steel and the bottom bar is 2025 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 200 to 220
110
Elastic (Young's, Tensile) Modulus, GPa 200
72
Elongation at Break, % 19 to 34
15
Fatigue Strength, MPa 230 to 350
130
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
27
Shear Strength, MPa 430 to 460
240
Tensile Strength: Ultimate (UTS), MPa 640 to 740
400
Tensile Strength: Yield (Proof), MPa 290 to 550
260

Thermal Properties

Latent Heat of Fusion, J/g 290
400
Maximum Temperature: Mechanical, °C 920
190
Melting Completion (Liquidus), °C 1490
640
Melting Onset (Solidus), °C 1440
520
Specific Heat Capacity, J/kg-K 470
870
Thermal Conductivity, W/m-K 14
150
Thermal Expansion, µm/m-K 17
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.9
40
Electrical Conductivity: Equal Weight (Specific), % IACS 3.2
120

Otherwise Unclassified Properties

Base Metal Price, % relative 30
10
Density, g/cm3 8.1
3.0
Embodied Carbon, kg CO2/kg material 5.0
7.9
Embodied Energy, MJ/kg 73
150
Embodied Water, L/kg 150
1130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 130 to 180
55
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 760
450
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 24
46
Strength to Weight: Axial, points 22 to 25
37
Strength to Weight: Bending, points 20 to 22
40
Thermal Diffusivity, mm2/s 3.7
58
Thermal Shock Resistance, points 14 to 16
18

Alloy Composition

Aluminum (Al), % 0
90.9 to 95.2
Carbon (C), % 0.040 to 0.1
0
Chromium (Cr), % 15.5 to 17.5
0 to 0.1
Copper (Cu), % 0
3.9 to 5.0
Iron (Fe), % 57.9 to 65.7
0 to 1.0
Magnesium (Mg), % 0
0 to 0.050
Manganese (Mn), % 0 to 1.5
0.4 to 1.2
Nickel (Ni), % 15.5 to 17.5
0
Niobium (Nb), % 0.4 to 1.2
0
Nitrogen (N), % 0.060 to 0.14
0
Phosphorus (P), % 0 to 0.035
0
Silicon (Si), % 0.3 to 0.6
0.5 to 1.2
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
0 to 0.15
Tungsten (W), % 2.5 to 3.5
0
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15