Maraging Steel 350/ C350
Technical Data Sheet
Chemical Composition Limits | ||||||||||||
Weight% | Ni | Co | Mn | Si | C | B | P | S | Al | Mo | Ti | Zr |
C350 | 18.50 | 12.0 | 0.10 max | 0.10 max | 0.03 max | 0.003 | 0.01 max | 0.01 max | 0.10 | 4.8 | 1.40 | 0.01 |
Alloy C350 is a nickel maraging steel which contains Cobalt as the primary strengthening agent. C350 has excellent mechanical properties, workability and heat treatment characteristics. Alloy C350 is used for missile and rocket motor cases, landing and takeoff gear components, high performance shafting, gears and fasteners.
Typical Mechanical Properties
Material | 0.2 % Yield Strength ksi | Ultimate Tensile Strength ksi | Elongation in 4D(%) |
Alloy C350 | 330 | 350 | 8 |
Availability
C 350 is available in Bar, Plate, Sheet, Rod, Billet, Forgings, Seamless Pipe, Welded Pipe, Seamless Tube, Welded Tube. For all stock availability contact Sales.
Specifications
MIL-S-46850
Trade name's: Maraging 350, Vascomax C350™
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.
Sell your Stock Online at 4metal.co.uk