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EN AC-45100 Aluminum vs. EN 1.4659 Stainless Steel

EN AC-45100 aluminum belongs to the aluminum alloys classification, while EN 1.4659 stainless steel belongs to the iron alloys. There are 30 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 EN AC-45100 aluminum and the bottom bar is EN 1.4659 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 97 to 130
260
Elastic (Young's, Tensile) Modulus, GPa 72
210
Elongation at Break, % 1.0 to 2.8
49
Fatigue Strength, MPa 82 to 99
460
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
81
Tensile Strength: Ultimate (UTS), MPa 300 to 360
900
Tensile Strength: Yield (Proof), MPa 210 to 320
480

Thermal Properties

Latent Heat of Fusion, J/g 470
300
Maximum Temperature: Mechanical, °C 170
1100
Melting Completion (Liquidus), °C 630
1480
Melting Onset (Solidus), °C 550
1430
Specific Heat Capacity, J/kg-K 890
460
Thermal Conductivity, W/m-K 140
12
Thermal Expansion, µm/m-K 22
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 30
1.7
Electrical Conductivity: Equal Weight (Specific), % IACS 95
1.9

Otherwise Unclassified Properties

Base Metal Price, % relative 10
37
Density, g/cm3 2.8
8.2
Embodied Carbon, kg CO2/kg material 7.9
6.5
Embodied Energy, MJ/kg 150
89
Embodied Water, L/kg 1100
220

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 3.5 to 7.6
370
Resilience: Unit (Modulus of Resilience), kJ/m3 290 to 710
550
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 49
24
Strength to Weight: Axial, points 30 to 35
31
Strength to Weight: Bending, points 35 to 39
25
Thermal Diffusivity, mm2/s 54
3.2
Thermal Shock Resistance, points 14 to 16
19

Alloy Composition

Aluminum (Al), % 88 to 92.8
0
Carbon (C), % 0
0 to 0.020
Chromium (Cr), % 0
23 to 25
Copper (Cu), % 2.6 to 3.6
1.0 to 2.0
Iron (Fe), % 0 to 0.6
35.7 to 45.7
Lead (Pb), % 0 to 0.1
0
Magnesium (Mg), % 0.15 to 0.45
0
Manganese (Mn), % 0 to 0.55
2.0 to 4.0
Molybdenum (Mo), % 0
5.5 to 6.5
Nickel (Ni), % 0 to 0.1
21 to 23
Nitrogen (N), % 0
0.35 to 0.5
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 4.5 to 6.0
0 to 0.7
Sulfur (S), % 0
0 to 0.010
Tin (Sn), % 0 to 0.050
0
Titanium (Ti), % 0 to 0.25
0
Tungsten (W), % 0
1.5 to 2.5
Zinc (Zn), % 0 to 0.2
0
Residuals, % 0 to 0.15
0