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EN 1.4945 Stainless Steel vs. EN AC-44000 Aluminum

EN 1.4945 stainless steel belongs to the iron alloys classification, while EN AC-44000 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 1.4945 stainless steel and the bottom bar is EN AC-44000 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 200 to 220
51
Elastic (Young's, Tensile) Modulus, GPa 200
71
Elongation at Break, % 19 to 34
7.3
Fatigue Strength, MPa 230 to 350
64
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
27
Tensile Strength: Ultimate (UTS), MPa 640 to 740
180
Tensile Strength: Yield (Proof), MPa 290 to 550
86

Thermal Properties

Latent Heat of Fusion, J/g 290
560
Maximum Temperature: Mechanical, °C 920
170
Melting Completion (Liquidus), °C 1490
590
Melting Onset (Solidus), °C 1440
590
Specific Heat Capacity, J/kg-K 470
910
Thermal Conductivity, W/m-K 14
140
Thermal Expansion, µm/m-K 17
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.9
36
Electrical Conductivity: Equal Weight (Specific), % IACS 3.2
130

Otherwise Unclassified Properties

Base Metal Price, % relative 30
9.5
Density, g/cm3 8.1
2.5
Embodied Carbon, kg CO2/kg material 5.0
7.8
Embodied Energy, MJ/kg 73
150
Embodied Water, L/kg 150
1070

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 130 to 180
11
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 760
51
Stiffness to Weight: Axial, points 14
16
Stiffness to Weight: Bending, points 24
55
Strength to Weight: Axial, points 22 to 25
20
Strength to Weight: Bending, points 20 to 22
28
Thermal Diffusivity, mm2/s 3.7
61
Thermal Shock Resistance, points 14 to 16
8.4

Alloy Composition


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Aluminum (Al), % 0
87.1 to 90
Carbon (C), % 0.040 to 0.1
0
Chromium (Cr), % 15.5 to 17.5
0
Copper (Cu), % 0
0 to 0.050
Iron (Fe), % 57.9 to 65.7
0 to 0.19
Magnesium (Mg), % 0
0 to 0.45
Manganese (Mn), % 0 to 1.5
0 to 0.1
Nickel (Ni), % 15.5 to 17.5
0
Niobium (Nb), % 0.4 to 1.2
0
Nitrogen (N), % 0.060 to 0.14
0
Phosphorus (P), % 0 to 0.035
0
Silicon (Si), % 0.3 to 0.6
10 to 11.8
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
0 to 0.15
Tungsten (W), % 2.5 to 3.5
0
Zinc (Zn), % 0
0 to 0.070
Residuals, % 0
0 to 0.1