MakeItFrom.com
Menu (ESC)

Nickel 625 vs. 707.0 Aluminum

Nickel 625 belongs to the nickel alloys classification, while 707.0 aluminum belongs to the aluminum alloys. There are 29 material properties with values for both materials. Properties with values for just one material (3, 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 625 and the bottom bar is 707.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
70
Elongation at Break, % 33 to 34
1.7 to 3.4
Fatigue Strength, MPa 240 to 320
75 to 140
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 79
26
Tensile Strength: Ultimate (UTS), MPa 790 to 910
270 to 300
Tensile Strength: Yield (Proof), MPa 320 to 450
170 to 250

Thermal Properties

Latent Heat of Fusion, J/g 330
380
Maximum Temperature: Mechanical, °C 980
180
Melting Completion (Liquidus), °C 1350
630
Melting Onset (Solidus), °C 1290
600
Specific Heat Capacity, J/kg-K 440
880
Thermal Conductivity, W/m-K 11
150
Thermal Expansion, µm/m-K 13
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.3
37
Electrical Conductivity: Equal Weight (Specific), % IACS 1.4
110

Otherwise Unclassified Properties

Base Metal Price, % relative 80
9.5
Density, g/cm3 8.6
2.9
Embodied Carbon, kg CO2/kg material 14
8.3
Embodied Energy, MJ/kg 190
150
Embodied Water, L/kg 290
1140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 220 to 250
4.3 to 8.6
Resilience: Unit (Modulus of Resilience), kJ/m3 260 to 490
210 to 430
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 23
47
Strength to Weight: Axial, points 26 to 29
26 to 29
Strength to Weight: Bending, points 22 to 24
32 to 34
Thermal Diffusivity, mm2/s 2.9
58
Thermal Shock Resistance, points 22 to 25
12 to 13

Alloy Composition

Aluminum (Al), % 0 to 0.4
90.5 to 93.6
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 20 to 23
0.2 to 0.4
Cobalt (Co), % 0 to 1.0
0
Copper (Cu), % 0
0 to 0.2
Iron (Fe), % 0 to 5.0
0 to 0.8
Magnesium (Mg), % 0
1.8 to 2.4
Manganese (Mn), % 0 to 0.5
0.4 to 0.6
Molybdenum (Mo), % 8.0 to 10
0
Nickel (Ni), % 58 to 68.9
0
Niobium (Nb), % 3.2 to 4.2
0
Phosphorus (P), % 0 to 0.015
0
Silicon (Si), % 0 to 0.5
0 to 0.2
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0 to 0.4
0 to 0.25
Zinc (Zn), % 0
4.0 to 4.5
Residuals, % 0
0 to 0.15