AWS ER80S-B2 vs. N06110 Nickel

AWS ER80S-B2 belongs to the iron alloys classification, while N06110 nickel belongs to the nickel alloys. There are 23 material properties with values for both materials. Properties with values for just one material (8, in this case) are not shown.

For each property being compared, the top bar is AWS ER80S-B2 and the bottom bar is N06110 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa		190
Elastic (Young's, Tensile) Modulus, GPa		210

Elongation at Break, %		21
Elongation at Break, %		53

Poisson's Ratio		0.29
Poisson's Ratio		0.28

Shear Modulus, GPa		73
Shear Modulus, GPa		84

Tensile Strength: Ultimate (UTS), MPa		620
Tensile Strength: Ultimate (UTS), MPa		730

Tensile Strength: Yield (Proof), MPa		540
Tensile Strength: Yield (Proof), MPa		330

Thermal Properties

Latent Heat of Fusion, J/g		260
Latent Heat of Fusion, J/g		340

Melting Completion (Liquidus), °C		1460
Melting Completion (Liquidus), °C		1490

Melting Onset (Solidus), °C		1420
Melting Onset (Solidus), °C		1440

Specific Heat Capacity, J/kg-K		470
Specific Heat Capacity, J/kg-K		440

Thermal Expansion, µm/m-K		13
Thermal Expansion, µm/m-K		12

Otherwise Unclassified Properties

Base Metal Price, % relative		3.0
Base Metal Price, % relative		65

Density, g/cm³		7.8
Density, g/cm³		8.6

Embodied Carbon, kg CO₂/kg material		1.6
Embodied Carbon, kg CO₂/kg material		11

Embodied Energy, MJ/kg		21
Embodied Energy, MJ/kg		160

Embodied Water, L/kg		54
Embodied Water, L/kg		320

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m³		130
Resilience: Ultimate (Unit Rupture Work), MJ/m³		320

Resilience: Unit (Modulus of Resilience), kJ/m³		760
Resilience: Unit (Modulus of Resilience), kJ/m³		260

Stiffness to Weight: Axial, points		13
Stiffness to Weight: Axial, points		14

Stiffness to Weight: Bending, points		24
Stiffness to Weight: Bending, points		23

Strength to Weight: Axial, points		22
Strength to Weight: Axial, points		23

Strength to Weight: Bending, points		21
Strength to Weight: Bending, points		21

Thermal Shock Resistance, points		18
Thermal Shock Resistance, points		20

Alloy Composition

Aluminum (Al), %		0
Aluminum (Al), %		0 to 1.0

Carbon (C), %		0.070 to 0.12
Carbon (C), %		0 to 0.15

Chromium (Cr), %		1.2 to 1.5
Chromium (Cr), %		28 to 33

Copper (Cu), %		0 to 0.35
Copper (Cu), %		0 to 0.5

Iron (Fe), %		95.2 to 97.5
Iron (Fe), %		0 to 1.0

Manganese (Mn), %		0.4 to 0.7
Manganese (Mn), %		0 to 1.0

Molybdenum (Mo), %		0.4 to 0.65
Molybdenum (Mo), %		9.0 to 12

Nickel (Ni), %		0 to 0.2
Nickel (Ni), %		51 to 62

Niobium (Nb), %		0
Niobium (Nb), %		0 to 1.0

Phosphorus (P), %		0 to 0.025
Phosphorus (P), %		0 to 0.5

Silicon (Si), %		0.4 to 0.7
Silicon (Si), %		0 to 1.0

Sulfur (S), %		0 to 0.025
Sulfur (S), %		0 to 0.015

Titanium (Ti), %		0
Titanium (Ti), %		0 to 1.0

Tungsten (W), %		0
Tungsten (W), %		1.0 to 4.0

Residuals, %		0 to 0.5
Residuals, %		0