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

ASTM B817 type I belongs to the titanium alloys classification, while 50Cr-50Ni alloy belongs to the otherwise unclassified metals. There are 21 material properties with values for both materials. Properties with values for just one material (9, in this case) are not shown.

For each property being compared, the top bar is ASTM B817 type I and the bottom bar is 50Cr-50Ni alloy.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 100
210
Elongation at Break, % 4.0 to 13
5.7
Poisson's Ratio 0.32
0.26
Shear Modulus, GPa 40
84
Tensile Strength: Ultimate (UTS), MPa 770 to 960
620
Tensile Strength: Yield (Proof), MPa 700 to 860
390

Thermal Properties

Latent Heat of Fusion, J/g 410
350
Specific Heat Capacity, J/kg-K 560
490
Thermal Expansion, µm/m-K 9.6
15

Otherwise Unclassified Properties

Base Metal Price, % relative 36
50
Density, g/cm3 4.4
8.0
Embodied Carbon, kg CO2/kg material 38
7.9
Embodied Energy, MJ/kg 610
110
Embodied Water, L/kg 200
350

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 30 to 120
31
Resilience: Unit (Modulus of Resilience), kJ/m3 2310 to 3540
350
Stiffness to Weight: Axial, points 13
15
Stiffness to Weight: Bending, points 35
25
Strength to Weight: Axial, points 48 to 60
21
Strength to Weight: Bending, points 42 to 49
20
Thermal Shock Resistance, points 54 to 68
14

Alloy Composition

Aluminum (Al), % 5.5 to 6.8
0 to 0.25
Carbon (C), % 0 to 0.1
0 to 0.1
Chlorine (Cl), % 0 to 0.2
0
Chromium (Cr), % 0
48 to 52
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.4
0 to 1.0
Manganese (Mn), % 0
0 to 0.3
Nickel (Ni), % 0
44.5 to 52
Nitrogen (N), % 0 to 0.040
0 to 0.3
Oxygen (O), % 0 to 0.3
0
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0 to 0.1
0 to 1.0
Sodium (Na), % 0 to 0.2
0
Sulfur (S), % 0
0 to 0.020
Titanium (Ti), % 87 to 91
0 to 0.5
Vanadium (V), % 3.5 to 4.5
0
Residuals, % 0 to 0.4
0