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UNS N10629 Nickel-Molybdenum Alloy

N10629 nickel is a nickel alloy formulated for primary forming into wrought products. Cited properties are appropriate for the annealed condition.

This material is well established: the Further Reading section below cites a number of published standards, and that list is not necessarily exhaustive.

It has a moderately low heat capacity among wrought nickels. In addition, it has a moderately high melting temperature and a moderately high embodied energy.

The graph bars on the material properties cards below compare N10629 nickel to: wrought nickels (top), all nickel 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

Elastic (Young's, Tensile) Modulus

220 GPa 32 x 106 psi

Elongation at Break

45 %

Fatigue Strength

340 MPa 49 x 103 psi

Poisson's Ratio

0.31

Rockwell B Hardness

88

Shear Modulus

83 GPa 12 x 106 psi

Shear Strength

600 MPa 87 x 103 psi

Tensile Strength: Ultimate (UTS)

860 MPa 120 x 103 psi

Tensile Strength: Yield (Proof)

400 MPa 57 x 103 psi

Thermal Properties

Latent Heat of Fusion

310 J/g

Maximum Temperature: Mechanical

910 °C 1660 °F

Melting Completion (Liquidus)

1610 °C 2930 °F

Melting Onset (Solidus)

1560 °C 2830 °F

Specific Heat Capacity

390 J/kg-K 0.094 BTU/lb-°F

Thermal Expansion

10 µm/m-K

Otherwise Unclassified Properties

Base Metal Price

75 % relative

Density

9.2 g/cm3 570 lb/ft3

Embodied Carbon

15 kg CO2/kg material

Embodied Energy

190 MJ/kg 82 x 103 BTU/lb

Embodied Water

270 L/kg 32 gal/lb

Common Calculations

Resilience: Ultimate (Unit Rupture Work)

320 MJ/m3

Resilience: Unit (Modulus of Resilience)

360 kJ/m3

Stiffness to Weight: Axial

13 points

Stiffness to Weight: Bending

22 points

Strength to Weight: Axial

26 points

Strength to Weight: Bending

22 points

Thermal Shock Resistance

27 points

Alloy Composition

Nickel (Ni)Ni 65 to 72.4
Molybdenum (Mo)Mo 26 to 30
Iron (Fe)Fe 1.0 to 6.0
Cobalt (Co)Co 0 to 2.5
Chromium (Cr)Cr 0.5 to 1.5
Manganese (Mn)Mn 0 to 1.5
Aluminum (Al)Al 0.1 to 0.5
Copper (Cu)Cu 0 to 0.5
Silicon (Si)Si 0 to 0.050
Phosphorus (P)P 0 to 0.040
Carbon (C)C 0 to 0.010
Sulfur (S)S 0 to 0.010

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

Followup Questions

Similar Alloys

Further Reading

ASTM B333: Standard Specification for Nickel-Molybdenum Alloy Plate, Sheet, and Strip

ASTM B335: Standard Specification for Nickel-Molybdenum Alloy Rod

ASTM B462: Standard Specification for Forged or Rolled UNS N06030, UNS N06022, UNS N06035, UNS N06200, UNS N06059, UNS N06686, UNS N08020, UNS N08024, UNS N08026, UNS N08367, UNS N10276, UNS N10665, UNS N10675, UNS N10629, UNS N08031, UNS N06045, UNS N06025, and UNS R20033 Alloy Pipe Flanges, Forged Fittings, and Valves and Parts for Corrosive High-Temperature Service

ASTM B619: Standard Specification for Welded Nickel and Nickel-Cobalt Alloy Pipe

ASTM B626: Standard Specification for Welded Nickel and Nickel-Cobalt Alloy Tube

ASTM B622: Standard Specification for Seamless Nickel and Nickel-Cobalt Alloy Pipe and Tube

ASTM B564: Standard Specification for Nickel Alloy Forgings

Aerospace Materials, Brian Cantor et al. (editors), 2001

Engineering Properties of Nickel and Nickel Alloys, John L. Everhart, 1971