Non-Corrosion Resisting Steel S150
Technical Data Sheet
| Chemical Composition Limits | |||||||||
| Weight% | C | Si | Mn | P+S max | Cr | Mo | Ni | Nb | Other |
| S150 | 0.08-0.16 | 0.15-0.60 | 0.30-1.20 | P 0.030 S 0.025 |
9.80-11.20 | 0.40-0.80 | 0.60-1.20 | 0.15-0.45 | V0.10-0.25 |
Typical Mechanical Properties
| Grade | Treatment | Tensile Strength Rm , N/mm² | Proof Stress Rp 0.2, N/mm² | Elongation in 5.65 √Cross Sectional Area% | Hardness HB |
| S150 | Solution Annealed | - | - | - | 277 max |
| S150 | Hardened and Tempered | 930-1080 | 780 | 10 | 285-331 |
Availability
Alloy S150 is available in Bar, for all stock availability contact Sales.
Customer Reviews - What Customers Say About Us!
"I would like to extend my gratitude to the entire staff at Aircraft Materials. It is a true pleasure to work with professionals in the aerospace industry. Keep up the great work!"
"Thank you very much, everything seems perfect. The quality of your cutting is superb."
"Could not fault your service."
"The service was perfect you had stock and same day collection"
"Item was very well packed"
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Disclaimer
Every effort is made to ensure that technical specifications are accurate. However, technical specifications included herein should be used as a guideline only. All specifications are subject to change without notice.
