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N08020 Stainless Steel vs. Sintered 2014 Aluminum

N08020 stainless steel belongs to the iron alloys classification, while sintered 2014 aluminum belongs to the aluminum alloys. There are 29 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 N08020 stainless steel and the bottom bar is sintered 2014 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
70
Elongation at Break, % 15 to 34
0.5 to 3.0
Fatigue Strength, MPa 210 to 240
52 to 100
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
26
Tensile Strength: Ultimate (UTS), MPa 610 to 620
140 to 290
Tensile Strength: Yield (Proof), MPa 270 to 420
97 to 280

Thermal Properties

Latent Heat of Fusion, J/g 300
390
Maximum Temperature: Mechanical, °C 1100
170
Melting Completion (Liquidus), °C 1410
650
Melting Onset (Solidus), °C 1360
560
Specific Heat Capacity, J/kg-K 460
880
Thermal Conductivity, W/m-K 12
130
Thermal Expansion, µm/m-K 15
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.6
33
Electrical Conductivity: Equal Weight (Specific), % IACS 1.8
100

Otherwise Unclassified Properties

Base Metal Price, % relative 38
10
Density, g/cm3 8.2
2.9
Embodied Carbon, kg CO2/kg material 6.6
8.0
Embodied Energy, MJ/kg 92
150
Embodied Water, L/kg 220
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 83 to 170
1.0 to 5.7
Resilience: Unit (Modulus of Resilience), kJ/m3 180 to 440
68 to 560
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 24
47
Strength to Weight: Axial, points 21
13 to 27
Strength to Weight: Bending, points 20
20 to 33
Thermal Diffusivity, mm2/s 3.2
51
Thermal Shock Resistance, points 15
6.2 to 13

Alloy Composition

Aluminum (Al), % 0
91.5 to 96.3
Carbon (C), % 0 to 0.070
0
Chromium (Cr), % 19 to 21
0
Copper (Cu), % 3.0 to 4.0
3.5 to 5.0
Iron (Fe), % 29.9 to 44
0
Magnesium (Mg), % 0
0.2 to 0.8
Manganese (Mn), % 0 to 2.0
0
Molybdenum (Mo), % 2.0 to 3.0
0
Nickel (Ni), % 32 to 38
0
Niobium (Nb), % 0 to 1.0
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 1.0
0 to 1.2
Sulfur (S), % 0 to 0.035
0
Residuals, % 0
0 to 1.5