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Hardened SAE-AISI M10 vs. Hardened SAE-AISI T6

Both hardened SAE-AISI M10 and hardened SAE-AISI T6 are iron alloys. Both are furnished in the hardened (H) condition. They have 68% of their average alloy composition in common.

For each property being compared, the top bar is hardened SAE-AISI M10 and the bottom bar is hardened SAE-AISI T6.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
210
Poisson's Ratio 0.29
0.29
Rockwell C Hardness 67
67
Shear Modulus, GPa 76
81
Tensile Strength: Ultimate (UTS), MPa 2170
2150

Thermal Properties

Latent Heat of Fusion, J/g 270
250
Melting Completion (Liquidus), °C 1520
1830
Melting Onset (Solidus), °C 1470
1770
Specific Heat Capacity, J/kg-K 460
400
Thermal Conductivity, W/m-K 31
18
Thermal Expansion, µm/m-K 12
12

Otherwise Unclassified Properties

Base Metal Price, % relative 14
70
Density, g/cm3 7.9
9.5
Embodied Carbon, kg CO2/kg material 8.3
11
Embodied Energy, MJ/kg 120
170
Embodied Water, L/kg 100
160

Common Calculations

PREN (Pitting Resistance) 31
39
Stiffness to Weight: Axial, points 14
12
Stiffness to Weight: Bending, points 24
21
Strength to Weight: Axial, points 76
63
Strength to Weight: Bending, points 47
39
Thermal Diffusivity, mm2/s 8.5
4.7
Thermal Shock Resistance, points 68
64

Alloy Composition

Carbon (C), % 0.84 to 1.1
0.75 to 0.85
Chromium (Cr), % 3.8 to 4.5
4.0 to 4.8
Cobalt (Co), % 0
11 to 13
Copper (Cu), % 0 to 0.25
0 to 0.25
Iron (Fe), % 82.3 to 85.6
55.9 to 63.5
Manganese (Mn), % 0.1 to 0.4
0.2 to 0.4
Molybdenum (Mo), % 7.8 to 8.5
0.4 to 1.0
Nickel (Ni), % 0 to 0.3
0 to 0.3
Phosphorus (P), % 0 to 0.030
0 to 0.030
Silicon (Si), % 0.2 to 0.45
0.2 to 0.4
Sulfur (S), % 0 to 0.030
0 to 0.030
Tungsten (W), % 0
18.5 to 21
Vanadium (V), % 1.8 to 2.2
1.5 to 2.1