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4130 vs SAE 4150 Carbon Steel (Normalized at 870 °C (1600 °F))

Property comparison of 4130 and SAE 4150 Carbon Steel (Normalized at 870 °C (1600 °F)), both carbon steel.

Carbon Steel13 compared properties
Property4130SAE 4150 Carbon Steel (Normalized at 870 °C (1600 °F))Difference
Yield strength460 MPa731 MPa+59%
Tensile strength560 MPa116 MPa-79%
Elongation21.5 %11.7 %-46%
Elastic modulus200,000 MPa200,000 MPa0%
Shear modulus76,923 MPa76,923 MPa0%
Poisson ratio0.30.30%
Density7,850 kg/m³7,850 kg/m³0%
Brinell hardness217 HB321 HB+48%
Thermal conductivity51.9 W/m·K51.9 W/m·K0%
Specific heat460 J/kg·K465 J/kg·K+1%
Coefficient of thermal expansion0.000012 1/K0.000012 1/K0%
Melting point1,480 °C1,480 °C0%
Reduction in area59.6 %30.8 %-48%

Difference is SAE 4150 Carbon Steel (Normalized at 870 °C (1600 °F)) relative to 4130. Values are taken from the representative row of each material; both materials may have multiple heat treatments or conditions on their individual pages.

Identification

4130
grade
4130
standard
SAE
heat treatment
Annealed at 865 °C (1585 T)
SAE 4150 Carbon Steel (Normalized at 870 °C (1600 °F))
grade
4150
standard
SAE
heat treatment
Normalized at 870 °C (1600 °F)

About AISI/SAE 41xx chromium-molybdenum steels

41xx grades are low-alloy steels with chromium and molybdenum. They harden deeper and tougher than plain carbon grades and weld reasonably well. 4130 is the standard for aircraft tubing and pressure vessels; 4140 covers shafts, gears, and high-strength fasteners.

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