Alloy 625 is a Nickel-Chromium based Superalloy with Min 58% Nickel.
Note that the Chemical Composition requirements vary according to which variant is ordered. For full details consult the published specification.
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ASTM B446-03 (2014) Alloy 625 |
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|---|---|
| Chemical Element | % Present |
| Phosphorous (P) | 0.02 max |
| Sulphur (S) | 0.02 max |
| Carbon (C) | 0.03 max |
| Manganese (Mn) | 0.05 max |
| Aluminium (Al) | 0.4 max |
| Titanium (Ti) | 0.4 max |
| Copper (Cu) | 0.5 max |
| Silicon (Si) | 0.5 max |
| Cobalt (Co) | 1 max |
| Niobium (Columbium) (Nb) | 3.15 - 4.15 |
| Columbium + Tantalum (Cb+Ta) | 3.15 - 4.15 |
| Iron (Fe) | 2 - 5 |
| Molybdenum (Mo) | 7 - 12.5 |
| Chromium (Cr) | 18 - 23 |
| Nickel (Ni) | 58 min |
This details the main elements only
N06625, N06219, N06650, Alloy 625, ASTM B446-03 (2014)
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ASTM B446-03 (2014) Bar - |
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|---|---|
| Mechanical Property | Value |
| Proof Stress | 270-420 Min MPa |
| Tensile Strength | 660-820 Min MPa |
| Elongation A50 mm | 25-50 Min % |
A wide range of Mechanical requirements applies according to size and the degree of cold or hot work that has been applied. For full details consult the published specification.