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Annealed 200 Maraging Steel vs. Annealed SAE-AISI M50

Both annealed 200 maraging steel and annealed SAE-AISI M50 are iron alloys. Both are furnished in the annealed condition. They have 73% of their average alloy composition in common. There are 20 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 200 maraging steel and the bottom bar is annealed SAE-AISI M50.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
190
Poisson's Ratio 0.3
0.29
Shear Modulus, GPa 74
75
Tensile Strength: Ultimate (UTS), MPa 970
720

Thermal Properties

Latent Heat of Fusion, J/g 260
260
Melting Completion (Liquidus), °C 1460
1480
Melting Onset (Solidus), °C 1420
1440
Specific Heat Capacity, J/kg-K 460
470
Thermal Expansion, µm/m-K 12
13

Otherwise Unclassified Properties

Base Metal Price, % relative 31
9.0
Density, g/cm3 8.2
7.9
Embodied Carbon, kg CO2/kg material 4.5
5.1
Embodied Energy, MJ/kg 59
74
Embodied Water, L/kg 140
83

Common Calculations

PREN (Pitting Resistance) 11
19
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 23
25
Strength to Weight: Axial, points 33
26
Strength to Weight: Bending, points 27
23
Thermal Shock Resistance, points 29
21

Alloy Composition

Aluminum (Al), % 0.050 to 0.15
0
Boron (B), % 0 to 0.0030
0
Calcium (Ca), % 0 to 0.050
0
Carbon (C), % 0 to 0.030
0.78 to 0.88
Chromium (Cr), % 0
3.8 to 4.5
Cobalt (Co), % 8.0 to 9.0
0
Copper (Cu), % 0
0 to 0.25
Iron (Fe), % 67.8 to 71.8
87 to 90.4
Manganese (Mn), % 0 to 0.1
0.15 to 0.45
Molybdenum (Mo), % 3.0 to 3.5
3.9 to 4.8
Nickel (Ni), % 17 to 19
0 to 0.3
Phosphorus (P), % 0 to 0.010
0 to 0.030
Silicon (Si), % 0 to 0.1
0.2 to 0.6
Sulfur (S), % 0 to 0.010
0 to 0.030
Titanium (Ti), % 0.15 to 0.25
0
Vanadium (V), % 0
0.8 to 1.3
Zirconium (Zr), % 0 to 0.020
0