MakeItFrom.com
Menu (ESC)

EN 1.8201 Steel vs. 5059 Aluminum

EN 1.8201 steel belongs to the iron alloys classification, while 5059 aluminum belongs to the aluminum 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 1.8201 steel and the bottom bar is 5059 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
69
Elongation at Break, % 20
11 to 25
Fatigue Strength, MPa 310
170 to 240
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 74
26
Shear Strength, MPa 390
220 to 250
Tensile Strength: Ultimate (UTS), MPa 630
350 to 410
Tensile Strength: Yield (Proof), MPa 450
170 to 300

Thermal Properties

Latent Heat of Fusion, J/g 250
390
Maximum Temperature: Mechanical, °C 450
210
Melting Completion (Liquidus), °C 1500
650
Melting Onset (Solidus), °C 1450
510
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 40
110
Thermal Expansion, µm/m-K 13
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.8
29
Electrical Conductivity: Equal Weight (Specific), % IACS 8.8
95

Otherwise Unclassified Properties

Base Metal Price, % relative 7.0
9.5
Density, g/cm3 8.0
2.7
Embodied Carbon, kg CO2/kg material 2.5
9.1
Embodied Energy, MJ/kg 36
160
Embodied Water, L/kg 59
1160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110
42 to 75
Resilience: Unit (Modulus of Resilience), kJ/m3 530
220 to 650
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 22
36 to 42
Strength to Weight: Bending, points 20
41 to 45
Thermal Diffusivity, mm2/s 11
44
Thermal Shock Resistance, points 18
16 to 18

Alloy Composition

Aluminum (Al), % 0 to 0.030
89.9 to 94
Boron (B), % 0.0010 to 0.0060
0
Carbon (C), % 0.040 to 0.1
0
Chromium (Cr), % 1.9 to 2.6
0 to 0.25
Copper (Cu), % 0
0 to 0.25
Iron (Fe), % 93.6 to 96.2
0 to 0.5
Magnesium (Mg), % 0
5.0 to 6.0
Manganese (Mn), % 0.1 to 0.6
0.6 to 1.2
Molybdenum (Mo), % 0.050 to 0.3
0
Niobium (Nb), % 0.020 to 0.080
0
Nitrogen (N), % 0 to 0.015
0
Phosphorus (P), % 0 to 0.030
0
Silicon (Si), % 0 to 0.5
0 to 0.45
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0.0050 to 0.060
0 to 0.2
Tungsten (W), % 1.5 to 1.8
0
Vanadium (V), % 0.2 to 0.3
0
Zinc (Zn), % 0
0.4 to 0.9
Zirconium (Zr), % 0
0.050 to 0.25
Residuals, % 0
0 to 0.15