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Nickel 689 vs. ASTM A182 Grade F5a

Nickel 689 belongs to the nickel alloys classification, while ASTM A182 grade F5a belongs to the iron alloys. There are 28 material properties with values for both materials. Properties with values for just one material (5, in this case) are not shown.

For each property being compared, the top bar is nickel 689 and the bottom bar is ASTM A182 grade F5a.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 350
310
Elastic (Young's, Tensile) Modulus, GPa 210
190
Elongation at Break, % 23
25
Fatigue Strength, MPa 420
380
Poisson's Ratio 0.29
0.29
Reduction in Area, % 21
56
Shear Modulus, GPa 80
74
Shear Strength, MPa 790
450
Tensile Strength: Ultimate (UTS), MPa 1250
710
Tensile Strength: Yield (Proof), MPa 690
520

Thermal Properties

Latent Heat of Fusion, J/g 330
260
Maximum Temperature: Mechanical, °C 990
510
Melting Completion (Liquidus), °C 1440
1460
Melting Onset (Solidus), °C 1390
1420
Specific Heat Capacity, J/kg-K 450
470
Thermal Expansion, µm/m-K 12
13

Otherwise Unclassified Properties

Base Metal Price, % relative 70
4.5
Density, g/cm3 8.5
7.8
Embodied Carbon, kg CO2/kg material 11
1.8
Embodied Energy, MJ/kg 150
24
Embodied Water, L/kg 330
69

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 240
160
Resilience: Unit (Modulus of Resilience), kJ/m3 1170
700
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 23
25
Strength to Weight: Axial, points 41
25
Strength to Weight: Bending, points 30
23
Thermal Shock Resistance, points 35
20

Alloy Composition

Aluminum (Al), % 0.75 to 1.3
0
Boron (B), % 0.0030 to 0.010
0
Carbon (C), % 0.1 to 0.2
0 to 0.25
Chromium (Cr), % 18 to 20
4.0 to 6.0
Cobalt (Co), % 9.0 to 11
0
Iron (Fe), % 0 to 5.0
91.4 to 95.6
Manganese (Mn), % 0 to 0.5
0 to 0.6
Molybdenum (Mo), % 9.0 to 10.5
0.44 to 0.65
Nickel (Ni), % 48.3 to 60.9
0 to 0.5
Phosphorus (P), % 0 to 0.015
0 to 0.040
Silicon (Si), % 0 to 0.5
0 to 0.5
Sulfur (S), % 0 to 0.015
0 to 0.030
Titanium (Ti), % 2.3 to 2.8
0