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| Element | Min | Max |
|---|---|---|
| C (Carbon) | 0.36% | 0.43% |
| Cr (Chromium) | 3% | 3.5% |
| Mn (Manganese) | 0.4% | 0.7% |
| Mo (Molybdenum) | 0.8% | 1.1% |
| P (Phosphorous) | 0.025% | |
| S (Sulphur) | 0.035% | |
| Si (Silicon) | 0.4% | |
| V (Vanadium) | 0.15% | 0.25% |
| Mechanical Properties | Min | Max |
|---|---|---|
| Ultimate Tensile Strength (UTS) | 950 MPa | 1150 MPa |
| 0.2% Proof Stress | 750 MPa | |
| Elongation | 11% | |
| Charpy V-Notch Impact =Room Temp. | 25 Joules |
Used commonly within the Aerospace, defence, Marine and subsea industries, for applications such as structural steels, pressure vessels, machine tools, turbine fasteners, support rods etc.
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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