MakeItFrom.com
Menu (ESC)

Annealed 9310 Ni-Cr-Mo Steel

Annealed SAE-AISI 9310 is SAE-AISI 9310 steel in the annealed condition. The graph bars on the material properties cards below compare annealed SAE-AISI 9310 to: SAE-AISI wrought steels (top), all iron alloys (middle), and the entire database (bottom). A full bar means this is the highest value in the relevant set. A half-full bar means it's 50% of the highest, and so on.

Mechanical Properties

Brinell Hardness

540

Elastic (Young's, Tensile) Modulus

190 GPa 27 x 106 psi

Elongation at Break

17 %

Fatigue Strength

300 MPa 43 x 103 psi

Poisson's Ratio

0.29

Rockwell B Hardness

240

Shear Modulus

73 GPa 11 x 106 psi

Shear Strength

510 MPa 73 x 103 psi

Tensile Strength: Ultimate (UTS)

820 MPa 120 x 103 psi

Tensile Strength: Yield (Proof)

450 MPa 65 x 103 psi

Thermal Properties

Latent Heat of Fusion

250 J/g

Maximum Temperature: Mechanical

440 °C 820 °F

Melting Completion (Liquidus)

1460 °C 2660 °F

Melting Onset (Solidus)

1420 °C 2580 °F

Specific Heat Capacity

470 J/kg-K 0.11 BTU/lb-°F

Thermal Conductivity

48 W/m-K 28 BTU/h-ft-°F

Thermal Expansion

13 µm/m-K

Electrical Properties

Electrical Conductivity: Equal Volume

7.7 % IACS

Electrical Conductivity: Equal Weight (Specific)

8.9 % IACS

Otherwise Unclassified Properties

Base Metal Price

4.4 % relative

Density

7.9 g/cm3 490 lb/ft3

Embodied Carbon

1.8 kg CO2/kg material

Embodied Energy

24 MJ/kg 10 x 103 BTU/lb

Embodied Water

57 L/kg 6.8 gal/lb

Common Calculations

Resilience: Ultimate (Unit Rupture Work)

120 MJ/m3

Resilience: Unit (Modulus of Resilience)

540 kJ/m3

Stiffness to Weight: Axial

13 points

Stiffness to Weight: Bending

24 points

Strength to Weight: Axial

29 points

Strength to Weight: Bending

25 points

Thermal Diffusivity

13 mm2/s

Thermal Shock Resistance

24 points

Alloy Composition

Iron (Fe)Fe 93.8 to 95.2
Nickel (Ni)Ni 3.0 to 3.5
Chromium (Cr)Cr 1.0 to 1.4
Manganese (Mn)Mn 0.45 to 0.65
Silicon (Si)Si 0.2 to 0.35
Molybdenum (Mo)Mo 0.080 to 0.15
Carbon (C)C 0.080 to 0.13
Phosphorus (P)P 0 to 0.015
Sulfur (S)S 0 to 0.012

All values are % weight. Ranges represent what is permitted under applicable standards.

Followup Questions

Further Reading

ASTM A646: Standard Specification for Premium Quality Alloy Steel Blooms and Billets for Aircraft and Aerospace Forgings

Properties and Selection: Irons, Steels and High Performance Alloys, ASM Handbook vol. 1, ASM International, 1993

ASM Specialty Handbook: Carbon and Alloy Steels, J. R. Davis (editor), 1996

Manufacture and Uses of Alloy Steels, Henry D. Hibbard, 2005

Steels: Processing, Structure, and Performance, 2nd ed., George Krauss, 2015