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Annealed 250 Maraging Steel vs. Annealed SAE-AISI M52

Both annealed 250 maraging steel and annealed SAE-AISI M52 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 250 maraging steel and the bottom bar is annealed SAE-AISI M52.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
190
Poisson's Ratio 0.3
0.29
Shear Modulus, GPa 75
75
Tensile Strength: Ultimate (UTS), MPa 970
710

Thermal Properties

Latent Heat of Fusion, J/g 270
260
Melting Completion (Liquidus), °C 1480
1510
Melting Onset (Solidus), °C 1430
1470
Specific Heat Capacity, J/kg-K 450
460
Thermal Expansion, µm/m-K 12
13

Otherwise Unclassified Properties

Base Metal Price, % relative 32
12
Density, g/cm3 8.2
7.9
Embodied Carbon, kg CO2/kg material 4.9
7.5
Embodied Energy, MJ/kg 65
110
Embodied Water, L/kg 140
89

Common Calculations

PREN (Pitting Resistance) 16
20
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 23
24
Strength to Weight: Axial, points 33
25
Strength to Weight: Bending, points 26
22
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
0.85 to 1.0
Chromium (Cr), % 0
3.5 to 4.3
Cobalt (Co), % 7.0 to 8.5
0
Copper (Cu), % 0
0 to 0.25
Iron (Fe), % 66.3 to 71.1
84.4 to 88.9
Manganese (Mn), % 0 to 0.1
0.15 to 0.45
Molybdenum (Mo), % 4.6 to 5.2
4.0 to 4.9
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), % 0.3 to 0.5
0
Tungsten (W), % 0
0.75 to 1.5
Vanadium (V), % 0
1.7 to 2.3
Zirconium (Zr), % 0 to 0.020
0