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7129 Aluminum vs. Nickel 601

7129 Aluminum belongs to the aluminum alloys classification, while nickel 601 belongs to the nickel 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 7129 Aluminum and the bottom bar is nickel 601.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
200
Elongation at Break, % 9.0 to 9.1
10 to 38
Fatigue Strength, MPa 150 to 190
220 to 380
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
76
Shear Strength, MPa 250 to 260
440 to 530
Tensile Strength: Ultimate (UTS), MPa 430
660 to 890
Tensile Strength: Yield (Proof), MPa 380 to 390
290 to 800

Thermal Properties

Latent Heat of Fusion, J/g 380
320
Maximum Temperature: Mechanical, °C 180
1100
Melting Completion (Liquidus), °C 630
1410
Melting Onset (Solidus), °C 510
1360
Specific Heat Capacity, J/kg-K 880
470
Thermal Conductivity, W/m-K 150
11
Thermal Expansion, µm/m-K 24
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 40
1.5
Electrical Conductivity: Equal Weight (Specific), % IACS 120
1.6

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
49
Density, g/cm3 2.9
8.3
Embodied Carbon, kg CO2/kg material 8.3
8.0
Embodied Energy, MJ/kg 150
110
Embodied Water, L/kg 1150
280

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 37 to 38
86 to 200
Resilience: Unit (Modulus of Resilience), kJ/m3 1050 to 1090
210 to 1630
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 47
23
Strength to Weight: Axial, points 41
22 to 30
Strength to Weight: Bending, points 43 to 44
20 to 25
Thermal Diffusivity, mm2/s 58
2.8
Thermal Shock Resistance, points 19
17 to 23

Alloy Composition

Aluminum (Al), % 91 to 94
1.0 to 1.7
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0 to 0.1
21 to 25
Copper (Cu), % 0.5 to 0.9
0 to 1.0
Gallium (Ga), % 0 to 0.030
0
Iron (Fe), % 0 to 0.3
7.7 to 20
Magnesium (Mg), % 1.3 to 2.0
0
Manganese (Mn), % 0 to 0.1
0 to 1.0
Nickel (Ni), % 0
58 to 63
Silicon (Si), % 0 to 0.15
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.050
0
Vanadium (V), % 0 to 0.050
0
Zinc (Zn), % 4.2 to 5.2
0
Residuals, % 0 to 0.15
0