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Specialty Compounds RTP Company

EOS NickelAlloy HX DMSL on EOS M 400-4
Categories: Metal; 3D Printing/Additive Manufacturing Metal; Nonferrous Metal; Nickel Alloy

Material Notes: EOS NickelAlloy HX is a nickel-chromium-iron-molybdenum alloy in fine powder form. Its composition corresponds to UNS N06002. While the wrought and cast versions of the alloy generally are solution annealed, the laser sintered version has a high strength and good elongation already in the as-built condition. Solution annealing of the laser sintered material will homogenize the microstructure, relax internal stresses and increase the elongation, while slightly decreasing the strength. This type of alloy is characterized by having high strength and oxidation resistance also at elevated temperatures, and is often used up to 1200°C. Therefore its applications can be found in aerospace technology, gas turbine parts, etc. Parts built from EOS NickelAlloy HX can be heat treated and material properties can be varied within specified range. In both as-built and solution heat treated states the parts can be machined, spark-eroded, welded, micro shot-peened, polished, and coated if required. Unexposed powder can be reused.

Heat treatment procedure: According to AMS2773 and AMS5390: Solution anneal at 1177ºC for 1 hour, followed by rapid air cooling to below 60ºC.

Information provided by EOS GmbH (Electro Optical Systems).

Key Words: N06002
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 PropertiesMetricEnglishComments
Density 8.20 g/cc0.296 lb/in³ISO 3369
Particle Size <= 63 µm<= 63 µm<0.5 wt% above 63µm; ASTM B214
 
Mechanical PropertiesMetricEnglishComments
Tensile Strength, Ultimate 710 MPa103000 psiHeat treated; ISO 6892-1 B10
 770 MPa112000 psiAs built; ISO 6892-1 B10
Tensile Strength, Yield 345 MPa50000 psiHeat treated; ISO 6892-1 B10
 610 MPa88500 psiAs built; ISO 6892-1 B10
Elongation at Break 31 %31 %As built; ISO 6892-1 B10
 45 %45 %Heat treated; ISO 6892-1 B10
 
Component Elements PropertiesMetricEnglishComments
Aluminum, Al <= 0.50 %<= 0.50 %
Boron, B <= 0.010 %<= 0.010 %
Carbon, C <= 0.10 %<= 0.10 %
Chromium, Cr 20.5 - 23 %20.5 - 23 %
Cobalt, Co 0.50 - 2.5 %0.50 - 2.5 %
Copper, Cu <= 0.50 %<= 0.50 %
Iron, Fe 17 - 20 %17 - 20 %
Manganese, Mn <= 1.0 %<= 1.0 %
Molybdenum, Mo 8.0 - 10 %8.0 - 10 %
Nickel, Ni 40.165 - 53.8 %40.165 - 53.8 %Balance
Phosphorus, P <= 0.040 %<= 0.040 %
Selenium, Se <= 0.0050 %<= 0.0050 %
Silicon, Si <= 1.0 %<= 1.0 %
Sulfur, S <= 0.030 %<= 0.030 %
Titanium, Ti <= 0.15 %<= 0.15 %
Tungsten, W 0.20 - 1.0 %0.20 - 1.0 %
 
Descriptive Properties
Surface roughness20-50 µmRz, after shot peening
 4-6.5 µmRa, after shot peening
Volume rate16.8 mm³/s

Some of the values displayed above may have been converted from their original units and/or rounded in order to display the information in a consistent format. Users requiring more precise data for scientific or engineering calculations can click on the property value to see the original value as well as raw conversions to equivalent units. We advise that you only use the original value or one of its raw conversions in your calculations to minimize rounding error. We also ask that you refer to MatWeb's terms of use regarding this information. Click here to view all the property values for this datasheet as they were originally entered into MatWeb.

NEOS937 / 280597

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