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Annealed SAE-AISI H22 vs. Annealed Titanium 6-6-2

Annealed SAE-AISI H22 belongs to the iron alloys classification, while annealed titanium 6-6-2 belongs to the titanium alloys. There are 21 material properties with values for both materials. Properties with values for just one material (12, in this case) are not shown.

For each property being compared, the top bar is annealed SAE-AISI H22 and the bottom bar is annealed titanium 6-6-2.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
120
Poisson's Ratio 0.29
0.32
Shear Modulus, GPa 77
44
Tensile Strength: Ultimate (UTS), MPa 700
1140

Thermal Properties

Latent Heat of Fusion, J/g 250
400
Melting Completion (Liquidus), °C 1670
1610
Melting Onset (Solidus), °C 1620
1560
Specific Heat Capacity, J/kg-K 440
540
Thermal Conductivity, W/m-K 31
5.5
Thermal Expansion, µm/m-K 12
9.4

Otherwise Unclassified Properties

Base Metal Price, % relative 28
40
Density, g/cm3 8.7
4.8
Embodied Carbon, kg CO2/kg material 4.9
29
Embodied Energy, MJ/kg 73
470
Embodied Water, L/kg 72
200

Common Calculations

Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 22
34
Strength to Weight: Axial, points 22
66
Strength to Weight: Bending, points 20
50
Thermal Diffusivity, mm2/s 8.2
2.1
Thermal Shock Resistance, points 22
75

Alloy Composition

Aluminum (Al), % 0
5.0 to 6.0
Carbon (C), % 0.3 to 0.4
0 to 0.050
Chromium (Cr), % 1.8 to 3.8
0
Copper (Cu), % 0 to 0.25
0.35 to 1.0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 82.2 to 87.4
0.35 to 1.0
Manganese (Mn), % 0.15 to 0.4
0
Molybdenum (Mo), % 0
5.0 to 6.0
Nickel (Ni), % 0 to 0.3
0
Nitrogen (N), % 0
0 to 0.040
Oxygen (O), % 0
0 to 0.2
Phosphorus (P), % 0 to 0.030
0
Silicon (Si), % 0.15 to 0.4
0
Sulfur (S), % 0 to 0.030
0
Tin (Sn), % 0
1.5 to 2.5
Titanium (Ti), % 0
82.8 to 87.8
Tungsten (W), % 10 to 11.8
0
Vanadium (V), % 0.25 to 0.5
0
Residuals, % 0
0 to 0.4