Nickel 80A vs. Grade 364 Molybdenum

Nickel 80A belongs to the nickel alloys classification, while grade 364 molybdenum belongs to the otherwise unclassified metals. There are 20 material properties with values for both materials. Properties with values for just one material (10, in this case) are not shown.

For each property being compared, the top bar is nickel 80A and the bottom bar is grade 364 molybdenum.

Nickel Alloy 80A (2.4631, N07080, NA20)Grade 364 Molybdenum

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa		190
Elastic (Young's, Tensile) Modulus, GPa		310

Elongation at Break, %		22
Elongation at Break, %		6.2 to 11

Poisson's Ratio		0.29
Poisson's Ratio		0.31

Shear Modulus, GPa		74
Shear Modulus, GPa		120

Tensile Strength: Ultimate (UTS), MPa		1040
Tensile Strength: Ultimate (UTS), MPa		580 to 720

Tensile Strength: Yield (Proof), MPa		710
Tensile Strength: Yield (Proof), MPa		350 to 620

Thermal Properties

Latent Heat of Fusion, J/g		320
Latent Heat of Fusion, J/g		370

Specific Heat Capacity, J/kg-K		470
Specific Heat Capacity, J/kg-K		250

Thermal Expansion, µm/m-K		13
Thermal Expansion, µm/m-K		7.0

Otherwise Unclassified Properties

Density, g/cm³		8.3
Density, g/cm³		10

Embodied Carbon, kg CO₂/kg material		9.8
Embodied Carbon, kg CO₂/kg material		28

Embodied Energy, MJ/kg		140
Embodied Energy, MJ/kg		330

Embodied Water, L/kg		280
Embodied Water, L/kg		360

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m³		210
Resilience: Ultimate (Unit Rupture Work), MJ/m³		43 to 57

Resilience: Unit (Modulus of Resilience), kJ/m³		1300
Resilience: Unit (Modulus of Resilience), kJ/m³		200 to 630

Stiffness to Weight: Axial, points		13
Stiffness to Weight: Axial, points		17

Stiffness to Weight: Bending, points		23
Stiffness to Weight: Bending, points		22

Strength to Weight: Axial, points		35
Strength to Weight: Axial, points		16 to 20

Strength to Weight: Bending, points		27
Strength to Weight: Bending, points		15 to 17

Thermal Shock Resistance, points		31
Thermal Shock Resistance, points		19 to 24

Alloy Composition

Aluminum (Al), %		0.5 to 1.8
Aluminum (Al), %		0

Carbon (C), %		0 to 0.1
Carbon (C), %		0.010 to 0.040

Chromium (Cr), %		18 to 21
Chromium (Cr), %		0

Iron (Fe), %		0 to 3.0
Iron (Fe), %		0 to 0.010

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

Molybdenum (Mo), %		0
Molybdenum (Mo), %		99.2 to 99.5

Nickel (Ni), %		69.4 to 79.7
Nickel (Ni), %		0 to 0.0050

Nitrogen (N), %		0
Nitrogen (N), %		0 to 0.0020

Oxygen (O), %		0
Oxygen (O), %		0 to 0.030

Silicon (Si), %		0 to 1.0
Silicon (Si), %		0 to 0.0050

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

Titanium (Ti), %		1.8 to 2.7
Titanium (Ti), %		0.4 to 0.55

Zirconium (Zr), %		0
Zirconium (Zr), %		0.060 to 0.12