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850.0 Aluminum vs. EN 1.4962 Stainless Steel

850.0 aluminum belongs to the aluminum alloys classification, while EN 1.4962 stainless steel belongs to the iron alloys. There are 31 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 850.0 aluminum and the bottom bar is EN 1.4962 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 45
190 to 210
Elastic (Young's, Tensile) Modulus, GPa 69
200
Elongation at Break, % 7.9
22 to 34
Fatigue Strength, MPa 59
210 to 330
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
77
Shear Strength, MPa 100
420 to 440
Tensile Strength: Ultimate (UTS), MPa 140
630 to 690
Tensile Strength: Yield (Proof), MPa 76
260 to 490

Thermal Properties

Latent Heat of Fusion, J/g 380
280
Maximum Temperature: Mechanical, °C 190
910
Melting Completion (Liquidus), °C 650
1480
Melting Onset (Solidus), °C 370
1440
Specific Heat Capacity, J/kg-K 850
470
Thermal Conductivity, W/m-K 180
14
Thermal Expansion, µm/m-K 23
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 47
2.3
Electrical Conductivity: Equal Weight (Specific), % IACS 140
2.6

Otherwise Unclassified Properties

Base Metal Price, % relative 14
23
Density, g/cm3 3.1
8.1
Embodied Carbon, kg CO2/kg material 8.5
4.1
Embodied Energy, MJ/kg 160
59
Embodied Water, L/kg 1160
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 9.1
140 to 170
Resilience: Unit (Modulus of Resilience), kJ/m3 42
170 to 610
Stiffness to Weight: Axial, points 12
14
Stiffness to Weight: Bending, points 44
24
Strength to Weight: Axial, points 12
21 to 24
Strength to Weight: Bending, points 19
20 to 21
Thermal Diffusivity, mm2/s 69
3.7
Thermal Shock Resistance, points 6.1
14 to 16

Alloy Composition

Aluminum (Al), % 88.3 to 93.1
0
Boron (B), % 0
0.0015 to 0.0060
Carbon (C), % 0
0.070 to 0.15
Chromium (Cr), % 0
15.5 to 17.5
Copper (Cu), % 0.7 to 1.3
0
Iron (Fe), % 0 to 0.7
62.1 to 69
Magnesium (Mg), % 0 to 0.1
0
Manganese (Mn), % 0 to 0.1
0 to 1.5
Nickel (Ni), % 0.7 to 1.3
12.5 to 14.5
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 0 to 0.7
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Tin (Sn), % 5.5 to 7.0
0
Titanium (Ti), % 0 to 0.2
0.4 to 0.7
Tungsten (W), % 0
2.5 to 3.0
Residuals, % 0 to 0.3
0