Nickel 625 vs. Nickel 200
Both nickel 625 and nickel 200 are nickel alloys. They have 64% 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 200.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 200 | |
180 |
Elongation at Break, % | 33 to 34 | |
23 to 44 |
Fatigue Strength, MPa | 240 to 320 | |
120 to 350 |
Poisson's Ratio | 0.29 | |
0.31 |
Shear Modulus, GPa | 79 | |
70 |
Shear Strength, MPa | 530 to 600 | |
300 to 340 |
Tensile Strength: Ultimate (UTS), MPa | 790 to 910 | |
420 to 540 |
Tensile Strength: Yield (Proof), MPa | 320 to 450 | |
120 to 370 |
Thermal Properties
Curie Temperature, °C | -200 | |
360 |
Latent Heat of Fusion, J/g | 330 | |
290 |
Maximum Temperature: Mechanical, °C | 980 | |
900 |
Melting Completion (Liquidus), °C | 1350 | |
1460 |
Melting Onset (Solidus), °C | 1290 | |
1440 |
Specific Heat Capacity, J/kg-K | 440 | |
450 |
Thermal Conductivity, W/m-K | 11 | |
69 |
Thermal Expansion, µm/m-K | 13 | |
13 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 1.3 | |
18 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 1.4 | |
18 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 80 | |
65 |
Density, g/cm3 | 8.6 | |
8.9 |
Embodied Carbon, kg CO2/kg material | 14 | |
11 |
Embodied Energy, MJ/kg | 190 | |
150 |
Embodied Water, L/kg | 290 | |
230 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 220 to 250 | |
110 to 150 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 260 to 490 | |
42 to 370 |
Stiffness to Weight: Axial, points | 13 | |
11 |
Stiffness to Weight: Bending, points | 23 | |
21 |
Strength to Weight: Axial, points | 26 to 29 | |
13 to 17 |
Strength to Weight: Bending, points | 22 to 24 | |
14 to 17 |
Thermal Diffusivity, mm2/s | 2.9 | |
17 |
Thermal Shock Resistance, points | 22 to 25 | |
13 to 16 |
Alloy Composition
Aluminum (Al), % | 0 to 0.4 | |
0 |
Carbon (C), % | 0 to 0.1 | |
0 to 0.15 |
Chromium (Cr), % | 20 to 23 | |
0 |
Cobalt (Co), % | 0 to 1.0 | |
0 |
Copper (Cu), % | 0 | |
0 to 0.25 |
Iron (Fe), % | 0 to 5.0 | |
0 to 0.4 |
Manganese (Mn), % | 0 to 0.5 | |
0 to 0.35 |
Molybdenum (Mo), % | 8.0 to 10 | |
0 |
Nickel (Ni), % | 58 to 68.9 | |
99 to 100 |
Niobium (Nb), % | 3.2 to 4.2 | |
0 |
Phosphorus (P), % | 0 to 0.015 | |
0 |
Silicon (Si), % | 0 to 0.5 | |
0 to 0.35 |
Sulfur (S), % | 0 to 0.015 | |
0 to 0.010 |
Titanium (Ti), % | 0 to 0.4 | |
0 |