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EOS Maraging Steel M S1 Powder Processed by DMSL on EOSINT M 270 and EOSINT M 280
Categories: Metal; 3D Printing/Additive Manufacturing Metal; Ferrous Metal; Alloy Steel

Material Notes: Description: Parts built in EOS Maraging Steel MS 1have a chemical composition corresponding to US classification 18% Ni Maraging 300, European 1.2709 and German X3NiCoMoT 1i 8-9-5 .This kind of steel is characterized by having very good mechanical properties, and being easily heat treatable using a simple thermal age-hardening process to obtain excellent hardness and strength. Parts built from EOS Maraging Steel MS1 are easily machinable after the building process and can be easily post-hardened to more then 50 HRC by age-hardening at 490 °C (914 °F) for 6 hours. In both as-built and age-hardened states the parts can be machined, spark-eroded, welded, micro shot-peened, polished and coated if required. Due to the layer wise building method, the parts have a certain anisotropy, which can be reduced or removed by appropriate heat treatment - see Technical Data for examples.

Ageing temperature 490 °C (914 °F), 6 hours, air cooling

Information provided by Proto3000

Key Words: Direct Metal Laser Sintering
Vendors: No vendors are listed for this material. Please click here if you are a supplier and would like information on how to add your listing to this material.
 
Physical PropertiesOriginal ValueComments
Density 8.00 - 8.10 g/cc
 
Mechanical PropertiesOriginal ValueComments
Hardness, Rockwell C 33.0 - 37.0As built; EN/ISO 6508-1
 50.0 - 56.0Heat treated; EN/ISO 6508-1
Tensile Strength 900 - 1100 MPain vertical direction (Z), As built; ISO 689-21:2009 (B) Annex D
 1000 - 1200 MPain horizontal direction (XY), As built; ISO 689-21:2009 (B) Annex D
 1930 MPain horizontal direction (XY), Heat treated; ISO 689-21:2009 (B) Annex D
 1950 - 2150 MPain vertical direction (Z), Heat treated; ISO 689-21:2009 (B) Annex D
Tensile Strength, Yield 900 - 1100 MPa
@Strain 0.2 %
in vertical direction (Z), As built; ISO 689-21:2009 (B) Annex D
 950 - 1150 MPa
@Strain 0.2 %
in horizontal direction (XY), As built; ISO 689-21:2009 (B) Annex D
 1862 MPa
@Strain 0.2 %
in horizontal direction (XY), Heat treated; ISO 689-21:2009 (B) Annex D
 1890 - 2090 MPa
@Strain 0.2 %
in vertical direction (Z), Heat treated; ISO 689-21:2009 (B) Annex D
Elongation at Break >= 2.00 %in horizontal direction (XY), Heat treated; ISO 689-21:2009 (B) Annex D
 2.00 - 6.00 %in vertical direction (Z), Heat treated; ISO 689-21:2009 (B) Annex D
 6.00 - 14.0 %in vertical direction (Z), As built; ISO 689-21:2009 (B) Annex D
 6.00 - 14.0 %in horizontal direction (XY), As built; ISO 689-21:2009 (B) Annex D
Modulus of Elasticity 130 - 170 GPain vertical direction (Z), As built; ISO 689-21:2009 (B) Annex D
 135 - 185 GPain horizontal direction (XY), As built; ISO 689-21:2009 (B) Annex D
 160 - 200 GPain horizontal direction (XY), Heat treated; ISO 689-21:2009 (B) Annex D
 160 - 200 GPain vertical direction (Z), Heat treated; ISO 689-21:2009 (B) Annex D
Charpy Impact 7.00 - 15.0 JNotched, Heat treated
 35.0 - 55.0 JNotched, As built
 
Thermal PropertiesOriginal ValueComments
Specific Heat Capacity 0.430 - 0.470 J/g-°CAs built
 0.430 - 0.470 J/g-°CHeat treated
Thermal Conductivity 14.2 - 15.8 W/m-KAs built
 19.0 - 21.0 W/m-KHeat treated
Maximum Service Temperature, Air 400 °C
 
Component Elements PropertiesOriginal ValueComments
Aluminum, Al 0.0500 - 0.150 %
Carbon, C <= 0.0300 %
Chromium, Cr <= 0.500 %
Cobalt, Co 8.50 - 9.50 %
Copper, Cu <= 0.500 %
Iron, Fe 64.6 - 69.35 %Balance
Manganese, Mn <= 0.100 %
Molybdenum, Mo 4.50 - 5.20 %
Nickel, Ni 17.0 - 19.0 %
Phosphorus, P <= 0.100 %
Silicon, Si <= 0.100 %
Sulfur, S <= 0.0100 %
Titanium, Ti 0.600 - 0.800 %

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NPROTO801 / 322914

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