Alloy Steel 9310

Material Data Sheet

9310 is low alloy steel containing nickel, chromium and molybdenum. It has high core hardness and high fatigue strength. This alloy is best machined in the normalized and tempered state. All of this makes 9310 excellent for aircraft parts.

Chemical Composition
Chemistry Content(%)
Iron, Fe 94.0
Nickel, Ni 3.0 – 3.5
Chromium, Cr 1.0 – 1.4
Manganese, Mn 0.45 – 0.65
Silicon, Si 0.15 – 0.30
Phosphorus, P 0.025
Sulfur, S ≤ 0.025
Molybdenum, Mo 0.08 – 0.15
Carbon, C 0.08 – 0.13
Physical Properties
Properties Metric Imperial
Density 7.7 – 8.03 g/cm3 0.278-0.290 lb/in3
Melting Point 1427 °C 2600 °F
Mechanical Properties
Properties Metric Imperial
Hardness, Brinell 363 363
Hardness, Knoop 392 392
Hardness, Rockwell B 100 100
Hardness, Rockwell C 40 40
Hardness, Vickers 384 384
Tensile Strength, Ultimate 1234 MPa 179000 psi
Tensile Strength, Yield 986 MPa 143000 psi
Elongation at Break 15.7% 15.7%
Modulus of Elasticity 200 GPa 2900 ksi
Bulk Modulus 140 GPa 20300 ksi
Poisson’s Ratio 0.29 0.29
Machinability 50% 50%
Shear Modulus 80 GPa 11600 ksi
Applications

Alloy Steel 9310 is used in the following application areas:

  • Heavy-Duty Gears
  • Clutch Parts
  • Machined Components
  • Aircraft Parts

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