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X3CrNiMoAl13.8.2 is a precipitation age hardened steel, that offers a high toughness and strength as well as a good resistance to stress corrosion cracking!
| Element | Min | Max |
|---|---|---|
| Al (Aluminium) | 1.1% | |
| C (Carbon) | 0.03% | |
| Cr (Chromium) | 12.7 | |
| Mn (Manganese) | 0.06% | |
| Mo (Molybdenum) | 2.2% | |
| Ni (Nickel) | 8.2% | |
| Si (Silicon) | 0.04% |
| Mechanical Properties | Min | Max |
|---|---|---|
| Ultimate Tensile Strength (UTS) | 1210 MPa | |
| 0.2% Proof Stress | 1140 MPa | |
| Elongation | 12% | |
| Gauge Length | A5D | |
| Hardness (Rockwell C) | 40 HRC | 45 HRC |
| Charpy V-Notch Impact = Room Temp. | 54 Joules |
Used within the Aerospace, petrochemical and nuclear industries for applications such as aircraft components, shafts, valves etc.
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Information is given for illustrative purposes only. Tachart accepts no responsibility for the accuracy of the data contained within or the use of the data by any other party.
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