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SAE-AISI 4340 Steel vs. R58150 Titanium

SAE-AISI 4340 steel belongs to the iron alloys classification, while R58150 titanium belongs to the titanium alloys. There are 26 material properties with values for both materials. Properties with values for just one material (6, in this case) are not shown.

For each property being compared, the top bar is SAE-AISI 4340 steel and the bottom bar is R58150 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
140
Elongation at Break, % 12 to 22
13
Fatigue Strength, MPa 330 to 740
330
Poisson's Ratio 0.29
0.32
Shear Modulus, GPa 73
52
Shear Strength, MPa 430 to 770
470
Tensile Strength: Ultimate (UTS), MPa 690 to 1280
770
Tensile Strength: Yield (Proof), MPa 470 to 1150
550

Thermal Properties

Latent Heat of Fusion, J/g 250
410
Maximum Temperature: Mechanical, °C 430
320
Melting Completion (Liquidus), °C 1460
1760
Melting Onset (Solidus), °C 1420
1700
Specific Heat Capacity, J/kg-K 470
500
Thermal Expansion, µm/m-K 13
8.4

Otherwise Unclassified Properties

Base Metal Price, % relative 3.5
48
Density, g/cm3 7.8
5.4
Embodied Carbon, kg CO2/kg material 1.7
31
Embodied Energy, MJ/kg 22
480
Embodied Water, L/kg 53
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 79 to 170
94
Resilience: Unit (Modulus of Resilience), kJ/m3 590 to 3490
1110
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 24
32
Strength to Weight: Axial, points 24 to 45
40
Strength to Weight: Bending, points 22 to 33
35
Thermal Shock Resistance, points 20 to 38
48

Alloy Composition

Carbon (C), % 0.38 to 0.43
0 to 0.1
Chromium (Cr), % 0.7 to 0.9
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 95.1 to 96.3
0 to 0.1
Manganese (Mn), % 0.6 to 0.8
0
Molybdenum (Mo), % 0.2 to 0.3
14 to 16
Nickel (Ni), % 1.7 to 2.0
0
Nitrogen (N), % 0
0 to 0.050
Oxygen (O), % 0
0 to 0.2
Phosphorus (P), % 0 to 0.035
0
Silicon (Si), % 0.15 to 0.35
0
Sulfur (S), % 0 to 0.040
0
Titanium (Ti), % 0
83.5 to 86