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AISI Grade 18Ni (250) Maraging Steel, 3.18 mm thick sheet, solution annealed at 815°C (1500°F) for 30 minutes, air cooled, aged at 480°C (900°F) for 1 hour
Categories: Metal; Ferrous Metal; Alloy Steel; Low Alloy Steel; Carbon Steel; Low Carbon Steel; Maraging Steel

Material Notes: Applications: Bearings, Belleville springs, bolts, cannon recoil springs, rocket motor and missiles cases, couplings, load cells, flexures for guidance mechanisms of missiles, helicopter drive shafts, transmission shafts, fan shafts in commercial jet engines, aircraft wing components and forgings, aluminum die casting dies, cold forming dies, plastic molding dies, cores, pins, punches, and trim knees.

Key Words: maraging steels, UNS K92890, ASTM A538 (B), ASTM A579 grade 72
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Physical PropertiesOriginal ValueComments
Density 8.00 g/cc
 
Mechanical PropertiesOriginal ValueComments
Tensile Strength, Ultimate 1824 MPa
Tensile Strength, Yield 1769 MPa
@Strain 0.2 %
Elongation at Break 4.8 %In 50 mm.
 9.4 %in 25 mm
Reduction of Area 48.7 %
Modulus of Elasticity 190 GPa
Bulk Modulus 160 GPaTypical for steel.
Poissons Ratio 0.30Calculated
Shear Modulus 73.0 GPaEstimated from elastic modulus
 
Electrical PropertiesOriginal ValueComments
Electrical Resistivity 0.0000174 ohm-cmTypical steel
 
Thermal PropertiesOriginal ValueComments
CTE, linear 10.1 µm/m-°C
@Temperature 21.0 - 480 °C
Thermal Conductivity 25.3 W/m-K
@Temperature 20.0 °C
 25.8 W/m-K
@Temperature 50.0 °C
 27.0 W/m-K
@Temperature 100 °C
 
Component Elements PropertiesOriginal ValueComments
Aluminum, Al 0.10 %
Boron, B 0.0030 %
Carbon, C <= 0.030 %
Cobalt, Co 7.5 %
Iron, Fe 68 %As remainder
Manganese, Mn <= 0.10 %
Molybdenum, Mo 4.8 %
Nickel, Ni 18.5 %
Phosphorus, P <= 0.010 %
Silicon, Si <= 0.10 %
Sulfur, S <= 0.010 %
Titanium, Ti 0.40 %
Zirconium, Zr 0.010 %

References for this datasheet.

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AISI Grade 18Ni (250) Maraging Steel, 3.18 mm thick sheet, solution annealed at 815°C (1500°F) for 30 minutes, air cooled, aged at 455°C (850°F) for 3 hours

M1825I / 7384

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