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50Cr-50Ni Alloy vs. ASTM B817 Type II

50Cr-50Ni alloy belongs to the otherwise unclassified metals classification, while ASTM B817 type II belongs to the titanium alloys. There are 21 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 50Cr-50Ni alloy and the bottom bar is ASTM B817 type II.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 210
100
Elongation at Break, % 5.7
3.0 to 13
Poisson's Ratio 0.26
0.32
Shear Modulus, GPa 84
40
Tensile Strength: Ultimate (UTS), MPa 620
900 to 960
Tensile Strength: Yield (Proof), MPa 390
780 to 900

Thermal Properties

Latent Heat of Fusion, J/g 350
400
Specific Heat Capacity, J/kg-K 490
550
Thermal Expansion, µm/m-K 15
9.9

Otherwise Unclassified Properties

Base Metal Price, % relative 50
37
Density, g/cm3 8.0
4.6
Embodied Carbon, kg CO2/kg material 7.9
40
Embodied Energy, MJ/kg 110
650
Embodied Water, L/kg 350
220

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 31
26 to 120
Resilience: Unit (Modulus of Resilience), kJ/m3 350
2890 to 3890
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 25
34
Strength to Weight: Axial, points 21
55 to 58
Strength to Weight: Bending, points 20
45 to 47
Thermal Shock Resistance, points 14
62 to 66

Alloy Composition

Aluminum (Al), % 0 to 0.25
5.0 to 6.0
Carbon (C), % 0 to 0.1
0 to 0.1
Chlorine (Cl), % 0
0 to 0.2
Chromium (Cr), % 48 to 52
0
Copper (Cu), % 0
0.35 to 1.0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0 to 1.0
0.35 to 1.0
Manganese (Mn), % 0 to 0.3
0
Nickel (Ni), % 44.5 to 52
0
Nitrogen (N), % 0 to 0.3
0 to 0.040
Oxygen (O), % 0
0 to 0.3
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0 to 1.0
0 to 0.1
Sodium (Na), % 0
0 to 0.2
Sulfur (S), % 0 to 0.020
0
Tin (Sn), % 0
1.5 to 2.5
Titanium (Ti), % 0 to 0.5
82.1 to 87.8
Vanadium (V), % 0
5.0 to 6.0
Residuals, % 0
0 to 0.4