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SAE-AISI 1086 Steel vs. Nickel 59

SAE-AISI 1086 steel belongs to the iron alloys classification, while nickel 59 belongs to the nickel alloys. There are 28 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown.

For each property being compared, the top bar is SAE-AISI 1086 steel and the bottom bar is nickel 59.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
220
Elongation at Break, % 11
50
Fatigue Strength, MPa 300 to 360
320
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 72
84
Shear Strength, MPa 450 to 520
560
Tensile Strength: Ultimate (UTS), MPa 760 to 870
780
Tensile Strength: Yield (Proof), MPa 480 to 580
350

Thermal Properties

Latent Heat of Fusion, J/g 240
330
Maximum Temperature: Mechanical, °C 400
990
Melting Completion (Liquidus), °C 1460
1500
Melting Onset (Solidus), °C 1410
1450
Specific Heat Capacity, J/kg-K 470
430
Thermal Conductivity, W/m-K 50
10
Thermal Expansion, µm/m-K 11
17

Otherwise Unclassified Properties

Base Metal Price, % relative 1.8
65
Density, g/cm3 7.8
8.7
Embodied Carbon, kg CO2/kg material 1.4
12
Embodied Energy, MJ/kg 19
160
Embodied Water, L/kg 45
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 79 to 84
320
Resilience: Unit (Modulus of Resilience), kJ/m3 610 to 890
280
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 24
23
Strength to Weight: Axial, points 27 to 31
25
Strength to Weight: Bending, points 24 to 26
22
Thermal Diffusivity, mm2/s 14
2.7
Thermal Shock Resistance, points 26 to 30
15

Alloy Composition

Aluminum (Al), % 0
0.1 to 0.4
Carbon (C), % 0.8 to 0.93
0 to 0.010
Chromium (Cr), % 0
22 to 24
Cobalt (Co), % 0
0 to 0.3
Copper (Cu), % 0
0 to 0.5
Iron (Fe), % 98.5 to 98.9
0 to 1.5
Manganese (Mn), % 0.3 to 0.5
0 to 0.5
Molybdenum (Mo), % 0
15 to 16.5
Nickel (Ni), % 0
56.2 to 62.9
Phosphorus (P), % 0 to 0.040
0 to 0.015
Silicon (Si), % 0
0 to 0.1
Sulfur (S), % 0 to 0.050
0 to 0.010