MakeItFrom.com
Menu (ESC)

Sintered 2014 Aluminum vs. EN 1.4565 Stainless Steel

Sintered 2014 aluminum belongs to the aluminum alloys classification, while EN 1.4565 stainless steel belongs to the iron alloys. There are 29 material properties with values for both materials. Properties with values for just one material (4, 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 sintered 2014 aluminum and the bottom bar is EN 1.4565 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
210
Elongation at Break, % 0.5 to 3.0
35
Fatigue Strength, MPa 52 to 100
380
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
81
Tensile Strength: Ultimate (UTS), MPa 140 to 290
880
Tensile Strength: Yield (Proof), MPa 97 to 280
480

Thermal Properties

Latent Heat of Fusion, J/g 390
310
Maximum Temperature: Mechanical, °C 170
1100
Melting Completion (Liquidus), °C 650
1420
Melting Onset (Solidus), °C 560
1380
Specific Heat Capacity, J/kg-K 880
470
Thermal Conductivity, W/m-K 130
12
Thermal Expansion, µm/m-K 23
15

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 33
1.9
Electrical Conductivity: Equal Weight (Specific), % IACS 100
2.1

Otherwise Unclassified Properties

Base Metal Price, % relative 10
28
Density, g/cm3 2.9
7.9
Embodied Carbon, kg CO2/kg material 8.0
5.4
Embodied Energy, MJ/kg 150
74
Embodied Water, L/kg 1150
210

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 1.0 to 5.7
260
Resilience: Unit (Modulus of Resilience), kJ/m3 68 to 560
550
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 47
25
Strength to Weight: Axial, points 13 to 27
31
Strength to Weight: Bending, points 20 to 33
26
Thermal Diffusivity, mm2/s 51
3.2
Thermal Shock Resistance, points 6.2 to 13
21

Alloy Composition

Aluminum (Al), % 91.5 to 96.3
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0
24 to 26
Copper (Cu), % 3.5 to 5.0
0
Iron (Fe), % 0
41.2 to 50.7
Magnesium (Mg), % 0.2 to 0.8
0
Manganese (Mn), % 0
5.0 to 7.0
Molybdenum (Mo), % 0
4.0 to 5.0
Nickel (Ni), % 0
16 to 19
Niobium (Nb), % 0
0 to 0.15
Nitrogen (N), % 0
0.3 to 0.6
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 1.2
0 to 1.0
Sulfur (S), % 0
0 to 0.015
Residuals, % 0 to 1.5
0