Nickel 625 vs. Nickel 600
Both nickel 625 and nickel 600 are nickel alloys. They have 82% of their average alloy composition in common. There are 31 material properties with values for both materials. Properties with values for just one material (1, in this case) are not shown.
For each property being compared, the top bar is nickel 625 and the bottom bar is nickel 600.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 200 | |
190 |
Elongation at Break, % | 33 to 34 | |
3.4 to 35 |
Fatigue Strength, MPa | 240 to 320 | |
220 to 300 |
Poisson's Ratio | 0.29 | |
0.29 |
Shear Modulus, GPa | 79 | |
75 |
Shear Strength, MPa | 530 to 600 | |
430 to 570 |
Tensile Strength: Ultimate (UTS), MPa | 790 to 910 | |
650 to 990 |
Tensile Strength: Yield (Proof), MPa | 320 to 450 | |
270 to 760 |
Thermal Properties
Curie Temperature, °C | -200 | |
-120 |
Latent Heat of Fusion, J/g | 330 | |
310 |
Maximum Temperature: Mechanical, °C | 980 | |
1100 |
Melting Completion (Liquidus), °C | 1350 | |
1410 |
Melting Onset (Solidus), °C | 1290 | |
1350 |
Specific Heat Capacity, J/kg-K | 440 | |
460 |
Thermal Conductivity, W/m-K | 11 | |
14 |
Thermal Expansion, µm/m-K | 13 | |
13 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 1.3 | |
1.7 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 1.4 | |
1.8 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 80 | |
55 |
Density, g/cm3 | 8.6 | |
8.5 |
Embodied Carbon, kg CO2/kg material | 14 | |
9.0 |
Embodied Energy, MJ/kg | 190 | |
130 |
Embodied Water, L/kg | 290 | |
250 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 220 to 250 | |
31 to 180 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 260 to 490 | |
190 to 1490 |
Stiffness to Weight: Axial, points | 13 | |
13 |
Stiffness to Weight: Bending, points | 23 | |
23 |
Strength to Weight: Axial, points | 26 to 29 | |
21 to 32 |
Strength to Weight: Bending, points | 22 to 24 | |
20 to 26 |
Thermal Diffusivity, mm2/s | 2.9 | |
3.6 |
Thermal Shock Resistance, points | 22 to 25 | |
19 to 29 |
Alloy Composition
Aluminum (Al), % | 0 to 0.4 | |
0 |
Carbon (C), % | 0 to 0.1 | |
0 to 0.15 |
Chromium (Cr), % | 20 to 23 | |
14 to 17 |
Cobalt (Co), % | 0 to 1.0 | |
0 |
Copper (Cu), % | 0 | |
0 to 0.5 |
Iron (Fe), % | 0 to 5.0 | |
6.0 to 10 |
Manganese (Mn), % | 0 to 0.5 | |
0 to 1.0 |
Molybdenum (Mo), % | 8.0 to 10 | |
0 |
Nickel (Ni), % | 58 to 68.9 | |
72 to 80 |
Niobium (Nb), % | 3.2 to 4.2 | |
0 |
Phosphorus (P), % | 0 to 0.015 | |
0 |
Silicon (Si), % | 0 to 0.5 | |
0 to 0.5 |
Sulfur (S), % | 0 to 0.015 | |
0 to 0.015 |
Titanium (Ti), % | 0 to 0.4 | |
0 |