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Nickel Alloy 617 (N06617, NA50)

Nickel 617 is a nickel alloy formulated for primary forming into wrought products. Cited properties are appropriate for the annealed condition. NA50 is the British Standard (BS) designation for this material. N06617 is the UNS number. And Nickel Alloy 617 is the common industry name.

The graph bars on the material properties cards below compare nickel 617 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

210 GPa 30 x 106 psi

Elongation at Break

40 %

Fatigue Strength

220 MPa 32 x 103 psi

Poisson's Ratio

0.29

Shear Modulus

80 GPa 12 x 106 psi

Shear Strength

510 MPa 73 x 103 psi

Tensile Strength: Ultimate (UTS)

740 MPa 110 x 103 psi

Tensile Strength: Yield (Proof)

280 MPa 40 x 103 psi

Thermal Properties

Latent Heat of Fusion

330 J/g

Maximum Temperature: Mechanical

1010 °C 1850 °F

Melting Completion (Liquidus)

1380 °C 2520 °F

Melting Onset (Solidus)

1330 °C 2430 °F

Specific Heat Capacity

450 J/kg-K 0.11 BTU/lb-°F

Thermal Conductivity

13 W/m-K 7.7 BTU/h-ft-°F

Thermal Expansion

12 µm/m-K

Electrical Properties

Electrical Conductivity: Equal Volume

1.4 % IACS

Electrical Conductivity: Equal Weight (Specific)

1.5 % IACS

Otherwise Unclassified Properties

Base Metal Price

75 % relative

Density

8.5 g/cm3 530 lb/ft3

Embodied Carbon

10 kg CO2/kg material

Embodied Energy

140 MJ/kg 60 x 103 BTU/lb

Embodied Water

350 L/kg 41 gal/lb

Common Calculations

Resilience: Ultimate (Unit Rupture Work)

230 MJ/m3

Resilience: Unit (Modulus of Resilience)

190 kJ/m3

Stiffness to Weight: Axial

14 points

Stiffness to Weight: Bending

23 points

Strength to Weight: Axial

24 points

Strength to Weight: Bending

21 points

Thermal Diffusivity

3.5 mm2/s

Thermal Shock Resistance

21 points

Alloy Composition

Nickel (Ni)Ni 44.5 to 62
Chromium (Cr)Cr 20 to 24
Cobalt (Co)Co 10 to 15
Molybdenum (Mo)Mo 8.0 to 10
Iron (Fe)Fe 0 to 3.0
Aluminum (Al)Al 0.8 to 1.5
Manganese (Mn)Mn 0 to 1.0
Silicon (Si)Si 0 to 1.0
Copper (Cu)Cu 0 to 0.5
Carbon (C)C 0.050 to 0.15
Sulfur (S)S 0 to 0.015
Boron (B)B 0 to 0.0060

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

Followup Questions

Similar Alloys

Further Reading

ASTM B546: Standard Specification for Electric Fusion-Welded Ni-Cr-Co-Mo Alloy (UNS N06617), Ni-Fe-Cr-Si Alloys (UNS N08330 and UNS N08332), Ni-Cr-Fe-Al Alloy (UNS N06603), Ni-Cr-Fe Alloy (UNS N06025), and Ni-Cr-Fe-Si Alloy (UNS N06045) Pipe

ASTM B166: Standard Specification for Nickel-Chromium-Iron Alloys (UNS N06600, N06601, N06603, N06690, N06693, N06025, and N06045) and Nickel-Chromium-Cobalt-Molybdenum Alloy (UNS N06617) Rod, Bar, and Wire

ASTM B167: Standard Specification for Nickel-Chromium-Iron Alloys (UNS N06600, N06601, N06603, N06690, N06693, N06025, and N06045) and Nickel-Chromium-Cobalt-Molybdenum Alloy (UNS N06617) Seamless Pipe and Tube

ASTM B168: Standard Specification Nickel-Chromium-Iron Alloys (UNS N06600, N06601, N06603, N06690, N06693, N06025, and N06045) and Nickel-Chromium-Cobalt-Molybdenum Alloy (UNS N06617) Plate, Sheet, and Strip

ASTM B564: Standard Specification for Nickel Alloy Forgings

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

Machining of Stainless Steels and Super Alloys: Traditional and Nontraditional Techniques, Helmi A. Youssef, 2016

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

Nickel Alloys, Ulrich Heubner (editor), 1998