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EN 1.4832 Stainless Steel vs. 1070A Aluminum

EN 1.4832 stainless steel belongs to the iron alloys classification, while 1070A 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 1.4832 stainless steel and the bottom bar is 1070A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 150
18 to 40
Elastic (Young's, Tensile) Modulus, GPa 200
68
Elongation at Break, % 11
2.3 to 33
Fatigue Strength, MPa 140
17 to 51
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
26
Tensile Strength: Ultimate (UTS), MPa 510
68 to 140
Tensile Strength: Yield (Proof), MPa 260
17 to 120

Thermal Properties

Latent Heat of Fusion, J/g 310
400
Maximum Temperature: Mechanical, °C 950
170
Melting Completion (Liquidus), °C 1400
640
Melting Onset (Solidus), °C 1360
640
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 14
230
Thermal Expansion, µm/m-K 16
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.1
60
Electrical Conductivity: Equal Weight (Specific), % IACS 2.5
200

Otherwise Unclassified Properties

Base Metal Price, % relative 19
9.0
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 3.6
8.2
Embodied Energy, MJ/kg 51
150
Embodied Water, L/kg 160
1200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 48
3.0 to 18
Resilience: Unit (Modulus of Resilience), kJ/m3 170
2.1 to 100
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 18
7.0 to 14
Strength to Weight: Bending, points 18
14 to 22
Thermal Diffusivity, mm2/s 3.7
94
Thermal Shock Resistance, points 12
3.1 to 6.3

Alloy Composition

Aluminum (Al), % 0
99.7 to 100
Carbon (C), % 0.15 to 0.35
0
Chromium (Cr), % 19 to 21
0
Copper (Cu), % 0
0 to 0.030
Iron (Fe), % 58.6 to 67.4
0 to 0.25
Magnesium (Mg), % 0
0 to 0.030
Manganese (Mn), % 0 to 2.0
0 to 0.030
Molybdenum (Mo), % 0 to 0.5
0
Nickel (Ni), % 13 to 15
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0.5 to 2.5
0 to 0.2
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0 to 0.030
Zinc (Zn), % 0
0 to 0.070