MakeItFrom.com
Menu (ESC)

EN 2.4856 Nickel vs. 1235 Aluminum

EN 2.4856 nickel belongs to the nickel alloys classification, while 1235 aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (1, 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 2.4856 nickel and the bottom bar is 1235 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
69
Elongation at Break, % 28
28 to 34
Fatigue Strength, MPa 280
23 to 58
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 79
26
Shear Strength, MPa 570
52 to 56
Tensile Strength: Ultimate (UTS), MPa 880
80 to 84
Tensile Strength: Yield (Proof), MPa 430
23 to 57

Thermal Properties

Latent Heat of Fusion, J/g 330
400
Maximum Temperature: Mechanical, °C 1000
170
Melting Completion (Liquidus), °C 1480
640
Melting Onset (Solidus), °C 1430
640
Specific Heat Capacity, J/kg-K 440
900
Thermal Conductivity, W/m-K 10
230
Thermal Expansion, µm/m-K 11
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.3
60
Electrical Conductivity: Equal Weight (Specific), % IACS 1.4
200

Otherwise Unclassified Properties

Base Metal Price, % relative 80
9.5
Density, g/cm3 8.6
2.7
Embodied Carbon, kg CO2/kg material 14
8.3
Embodied Energy, MJ/kg 190
160
Embodied Water, L/kg 290
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 200
17 to 25
Resilience: Unit (Modulus of Resilience), kJ/m3 440
3.8 to 24
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 23
50
Strength to Weight: Axial, points 28
8.2 to 8.6
Strength to Weight: Bending, points 24
15 to 16
Thermal Diffusivity, mm2/s 2.7
93
Thermal Shock Resistance, points 29
3.6 to 3.7

Alloy Composition

Aluminum (Al), % 0 to 0.4
99.35 to 100
Carbon (C), % 0.030 to 0.1
0
Chromium (Cr), % 20 to 23
0
Cobalt (Co), % 0 to 1.0
0
Copper (Cu), % 0 to 0.5
0 to 0.050
Iron (Fe), % 0 to 5.0
0 to 0.65
Magnesium (Mg), % 0
0 to 0.050
Manganese (Mn), % 0 to 0.5
0 to 0.050
Molybdenum (Mo), % 8.0 to 10
0
Nickel (Ni), % 58 to 68.8
0
Niobium (Nb), % 3.2 to 4.2
0
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0 to 0.5
0 to 0.65
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0 to 0.4
0 to 0.060
Vanadium (V), % 0
0 to 0.050
Zinc (Zn), % 0
0 to 0.1