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Nickel 80A vs. Nickel 689

Both nickel 80A and nickel 689 are nickel alloys. Both are furnished in the aged (precipitation hardened) condition. They have 79% of their average alloy composition in common. There are 26 material properties with values for both materials. Properties with values for just one material (6, in this case) are not shown.

For each property being compared, the top bar is nickel 80A and the bottom bar is nickel 689.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
210
Elongation at Break, % 22
23
Fatigue Strength, MPa 430
420
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 74
80
Shear Strength, MPa 660
790
Tensile Strength: Ultimate (UTS), MPa 1040
1250
Tensile Strength: Yield (Proof), MPa 710
690

Thermal Properties

Latent Heat of Fusion, J/g 320
330
Maximum Temperature: Mechanical, °C 980
990
Melting Completion (Liquidus), °C 1360
1440
Melting Onset (Solidus), °C 1310
1390
Specific Heat Capacity, J/kg-K 470
450
Thermal Expansion, µm/m-K 13
12

Otherwise Unclassified Properties

Base Metal Price, % relative 55
70
Density, g/cm3 8.3
8.5
Embodied Carbon, kg CO2/kg material 9.8
11
Embodied Energy, MJ/kg 140
150
Embodied Water, L/kg 280
330

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 210
240
Resilience: Unit (Modulus of Resilience), kJ/m3 1300
1170
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 23
23
Strength to Weight: Axial, points 35
41
Strength to Weight: Bending, points 27
30
Thermal Shock Resistance, points 31
35

Alloy Composition

Aluminum (Al), % 0.5 to 1.8
0.75 to 1.3
Boron (B), % 0
0.0030 to 0.010
Carbon (C), % 0 to 0.1
0.1 to 0.2
Chromium (Cr), % 18 to 21
18 to 20
Cobalt (Co), % 0
9.0 to 11
Iron (Fe), % 0 to 3.0
0 to 5.0
Manganese (Mn), % 0 to 1.0
0 to 0.5
Molybdenum (Mo), % 0
9.0 to 10.5
Nickel (Ni), % 69.4 to 79.7
48.3 to 60.9
Phosphorus (P), % 0
0 to 0.015
Silicon (Si), % 0 to 1.0
0 to 0.5
Sulfur (S), % 0 to 0.015
0 to 0.015
Titanium (Ti), % 1.8 to 2.7
2.3 to 2.8