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A350 LF2
Alloy Steel
| Element | Min | Max |
|---|---|---|
| C (Carbon) | 0.3% | |
| Cr (Chromium) | 0.3% | |
| Cu (Copper) | 0.4% | |
| Mn (Manganese) | 0.6 | 1.35% |
| Mo (Molybdenum) | 0.12% | |
| Nb (Niobium) | 0.02% | |
| Ni (Nickel) | 0.4% | |
| P (Phosphorus) | 0.035% | |
| S (Sulphur) | 0.04% | |
| Si (Silicon) | 0.15% | 0.3% |
| V (Vanadium) | 0.08% |
| Mechanical Property | Min | Max |
|---|---|---|
| Ultimate Tensile Strength (UTS) | 485 MPa | 655 MPa |
| Yield Strength | 250 MPa | |
| Elongation | 22% |
Disclaimer:
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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