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

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."
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"Item was very well packed"

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.