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Full-Hard Nickel Alloy 600

Full-hard nickel 600 is nickel 600 in the full-hard temper. It has the highest strength and lowest ductility compared to the other variants of nickel 600. The graph bars on the material properties cards below compare full-hard nickel 600 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

190 GPa 28 x 106 psi

Elongation at Break

3.4 %

Fatigue Strength

300 MPa 44 x 103 psi

Poisson's Ratio

0.29

Shear Modulus

75 GPa 11 x 106 psi

Shear Strength

570 MPa 83 x 103 psi

Tensile Strength: Ultimate (UTS)

990 MPa 140 x 103 psi

Tensile Strength: Yield (Proof)

760 MPa 110 x 103 psi

Thermal Properties

Curie Temperature

-120 °C -190 °F

Latent Heat of Fusion

310 J/g

Maximum Temperature: Mechanical

1100 °C 2010 °F

Melting Completion (Liquidus)

1410 °C 2580 °F

Melting Onset (Solidus)

1350 °C 2470 °F

Specific Heat Capacity

460 J/kg-K 0.11 BTU/lb-°F

Thermal Conductivity

14 W/m-K 8.2 BTU/h-ft-°F

Thermal Expansion

13 µm/m-K

Electrical Properties

Electrical Conductivity: Equal Volume

1.7 % IACS

Electrical Conductivity: Equal Weight (Specific)

1.8 % IACS

Otherwise Unclassified Properties

Base Metal Price

55 % relative

Calomel Potential

-170 mV

Density

8.5 g/cm3 530 lb/ft3

Embodied Carbon

9.0 kg CO2/kg material

Embodied Energy

130 MJ/kg 54 x 103 BTU/lb

Embodied Water

250 L/kg 30 gal/lb

Common Calculations

Resilience: Ultimate (Unit Rupture Work)

31 MJ/m3

Resilience: Unit (Modulus of Resilience)

1490 kJ/m3

Stiffness to Weight: Axial

13 points

Stiffness to Weight: Bending

23 points

Strength to Weight: Axial

32 points

Strength to Weight: Bending

26 points

Thermal Diffusivity

3.6 mm2/s

Thermal Shock Resistance

29 points

Alloy Composition

Nickel (Ni)Ni 72 to 80
Chromium (Cr)Cr 14 to 17
Iron (Fe)Fe 6.0 to 10
Manganese (Mn)Mn 0 to 1.0
Silicon (Si)Si 0 to 0.5
Copper (Cu)Cu 0 to 0.5
Carbon (C)C 0 to 0.15
Sulfur (S)S 0 to 0.015

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

Followup Questions

Further Reading

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

Microstructure of Superalloys, Madeleine Durand-Charre, 1998

ASM Specialty Handbook: Nickel, Cobalt, and Their Alloys, Joseph R. Davis (editor), 2000

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

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

Nickel Alloys, Ulrich Heubner (editor), 1998