MakeItFrom.com
Menu (ESC)

EN 1.4662 Stainless Steel vs. 5252 Aluminum

EN 1.4662 stainless steel belongs to the iron alloys classification, while 5252 aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, 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 1.4662 stainless steel and the bottom bar is 5252 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
68
Elongation at Break, % 28
4.5 to 11
Fatigue Strength, MPa 430 to 450
100 to 110
Poisson's Ratio 0.27
0.33
Shear Modulus, GPa 79
25
Shear Strength, MPa 520 to 540
140 to 160
Tensile Strength: Ultimate (UTS), MPa 810 to 830
230 to 290
Tensile Strength: Yield (Proof), MPa 580 to 620
170 to 240

Thermal Properties

Latent Heat of Fusion, J/g 290
400
Maximum Temperature: Mechanical, °C 1090
180
Melting Completion (Liquidus), °C 1430
650
Melting Onset (Solidus), °C 1380
610
Specific Heat Capacity, J/kg-K 480
910
Thermal Conductivity, W/m-K 15
140
Thermal Expansion, µm/m-K 13
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.2
34
Electrical Conductivity: Equal Weight (Specific), % IACS 2.5
120

Otherwise Unclassified Properties

Base Metal Price, % relative 16
9.5
Density, g/cm3 7.7
2.7
Embodied Carbon, kg CO2/kg material 3.2
8.7
Embodied Energy, MJ/kg 45
160
Embodied Water, L/kg 170
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 210
12 to 23
Resilience: Unit (Modulus of Resilience), kJ/m3 840 to 940
210 to 430
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 25
51
Strength to Weight: Axial, points 29 to 30
23 to 30
Strength to Weight: Bending, points 25
31 to 36
Thermal Diffusivity, mm2/s 3.9
57
Thermal Shock Resistance, points 22
10 to 13

Alloy Composition

Aluminum (Al), % 0
96.6 to 97.8
Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 23 to 25
0
Copper (Cu), % 0.1 to 0.8
0 to 0.1
Iron (Fe), % 62.6 to 70.2
0 to 0.1
Magnesium (Mg), % 0
2.2 to 2.8
Manganese (Mn), % 2.5 to 4.0
0 to 0.1
Molybdenum (Mo), % 1.0 to 2.0
0
Nickel (Ni), % 3.0 to 4.5
0
Nitrogen (N), % 0.2 to 0.3
0
Phosphorus (P), % 0 to 0.035
0
Silicon (Si), % 0 to 0.7
0 to 0.080
Sulfur (S), % 0 to 0.0050
0
Vanadium (V), % 0
0 to 0.050
Zinc (Zn), % 0
0 to 0.050
Residuals, % 0
0 to 0.1