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242.0 Aluminum vs. EN 2.4951 Nickel

242.0 aluminum belongs to the aluminum alloys classification, while EN 2.4951 nickel belongs to the nickel alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, 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 242.0 aluminum and the bottom bar is EN 2.4951 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 70 to 110
200
Elastic (Young's, Tensile) Modulus, GPa 73
190
Elongation at Break, % 0.5 to 1.5
34
Fatigue Strength, MPa 55 to 110
200
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 27
76
Shear Strength, MPa 150 to 240
500
Tensile Strength: Ultimate (UTS), MPa 180 to 290
750
Tensile Strength: Yield (Proof), MPa 120 to 220
270

Thermal Properties

Latent Heat of Fusion, J/g 390
320
Maximum Temperature: Mechanical, °C 210
1150
Melting Completion (Liquidus), °C 640
1360
Melting Onset (Solidus), °C 530
1310
Specific Heat Capacity, J/kg-K 870
460
Thermal Conductivity, W/m-K 130 to 170
12
Thermal Expansion, µm/m-K 22
12

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 33 to 44
1.6
Electrical Conductivity: Equal Weight (Specific), % IACS 96 to 130
1.7

Otherwise Unclassified Properties

Base Metal Price, % relative 12
60
Density, g/cm3 3.1
8.5
Embodied Carbon, kg CO2/kg material 8.3
9.3
Embodied Energy, MJ/kg 150
130
Embodied Water, L/kg 1130
280

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 1.3 to 3.4
200
Resilience: Unit (Modulus of Resilience), kJ/m3 110 to 340
190
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 45
23
Strength to Weight: Axial, points 16 to 26
25
Strength to Weight: Bending, points 23 to 32
22
Thermal Diffusivity, mm2/s 50 to 62
3.1
Thermal Shock Resistance, points 8.0 to 13
23

Alloy Composition

Aluminum (Al), % 88.4 to 93.6
0 to 0.3
Carbon (C), % 0
0.080 to 0.15
Chromium (Cr), % 0 to 0.25
18 to 21
Cobalt (Co), % 0
0 to 5.0
Copper (Cu), % 3.5 to 4.5
0 to 0.5
Iron (Fe), % 0 to 1.0
0 to 5.0
Magnesium (Mg), % 1.2 to 1.8
0
Manganese (Mn), % 0 to 0.35
0 to 1.0
Nickel (Ni), % 1.7 to 2.3
65.4 to 81.7
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0 to 0.7
0 to 1.0
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.25
0.2 to 0.6
Zinc (Zn), % 0 to 0.35
0
Residuals, % 0 to 0.15
0