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Nickel 689 vs. Nickel 80A

Both nickel 689 and nickel 80A 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 689 and the bottom bar is nickel 80A.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition

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