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Nickel 690 vs. 6262A Aluminum

Nickel 690 belongs to the nickel alloys classification, while 6262A 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 nickel 690 and the bottom bar is 6262A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
68
Elongation at Break, % 3.4 to 34
4.5 to 11
Fatigue Strength, MPa 180 to 300
94 to 110
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 79
26
Shear Strength, MPa 420 to 570
190 to 240
Tensile Strength: Ultimate (UTS), MPa 640 to 990
310 to 410
Tensile Strength: Yield (Proof), MPa 250 to 760
270 to 370

Thermal Properties

Latent Heat of Fusion, J/g 320
400
Maximum Temperature: Mechanical, °C 1010
160
Melting Completion (Liquidus), °C 1380
640
Melting Onset (Solidus), °C 1340
580
Specific Heat Capacity, J/kg-K 470
890
Thermal Conductivity, W/m-K 14
170
Thermal Expansion, µm/m-K 14
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.5
45
Electrical Conductivity: Equal Weight (Specific), % IACS 1.6
140

Otherwise Unclassified Properties

Base Metal Price, % relative 50
11
Density, g/cm3 8.3
2.8
Embodied Carbon, kg CO2/kg material 8.2
8.4
Embodied Energy, MJ/kg 120
150
Embodied Water, L/kg 290
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 31 to 170
17 to 34
Resilience: Unit (Modulus of Resilience), kJ/m3 160 to 1440
540 to 1000
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 24
49
Strength to Weight: Axial, points 21 to 33
31 to 41
Strength to Weight: Bending, points 20 to 27
36 to 44
Thermal Diffusivity, mm2/s 3.5
67
Thermal Shock Resistance, points 16 to 25
14 to 18

Alloy Composition

Aluminum (Al), % 0
94.2 to 97.8
Bismuth (Bi), % 0
0.4 to 0.9
Carbon (C), % 0 to 0.050
0
Chromium (Cr), % 27 to 31
0.040 to 0.14
Copper (Cu), % 0 to 0.5
0.15 to 0.4
Iron (Fe), % 7.0 to 11
0 to 0.7
Magnesium (Mg), % 0
0.8 to 1.2
Manganese (Mn), % 0 to 0.5
0 to 0.15
Nickel (Ni), % 58 to 66
0
Silicon (Si), % 0 to 0.5
0.4 to 0.8
Sulfur (S), % 0 to 0.015
0
Tin (Sn), % 0
0.4 to 1.0
Titanium (Ti), % 0
0 to 0.1
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15