MatWeb - Material Property Data Advertise with MatWeb!     Register Now
Data sheets for over 180,000 metals, plastics, ceramics, and composites.
MatWeb - Material Property Data HOME  •   SEARCH  •   TOOLS  •   SUPPLIERS  •   FOLDERS  •   ABOUT US  •   FAQ  •   LOG IN    
Recently Viewed Materials (most recent at top)  

Login to see your most recently viewed materials here.

Or if you don't have an account with us yet, then click here to register.

  Searches:   Advanced  | Category  | Property  | Metals  | Trade Name  | Manufacturer  | Recently Viewed Materials
  

Specialty Compounds RTP Company

EOS NickelAlloy IN625 DMSL Powder
Categories: Metal; 3D Printing/Additive Manufacturing Metal; Nonferrous Metal; Nickel Alloy

Material Notes: Parts built from EOS NickelAlloy IN625 have chemical composition corresponding to UNS N06625, AMS 5666F, AMS 5599G, W.Nr 2.4856, DIN NiCr22Mo9Nb. This type of alloy is characterized by having high tensile, creep and rupture strength. Conventionally cast or wrought components in this type of nickel alloy have typically excellent fatigue and thermal fatigue properties combined with good oxidation resistance. EOS NickelAlloy IN625 is expected to have good corrosion resistance in various corrosive environments. Especially sea water applications require high pitting and crevice corrosion resistance, stress-corrosion resistance against chloride ions, high tensile and corrosion-fatigue strength. However, corrosion resistance has not been verified yet and therefore it is recommended to conduct relevant corrosion tests and studies prior to use in specific corrosive environment. Parts built from EOS NickelAlloy IN625 can be heat treated and material properties can be varied within specified range. Parts can be machined, spark-eroded, welded, micro shot-peened, polished and coated in both as-built and in heat-treated conditions. Due to the layerwise building method, the parts have certain anisotropy.

Information provided by EOS GmbH (Electro Optical Systems).

Key Words: UNS N06625
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 8.40 g/cc0.303 lb/in³Part; ISO 3369
Particle Size 29 - 41 µm29 - 41 µmd50; ISO 13320
 
Mechanical PropertiesMetricEnglishComments
Hardness, Rockwell C 2727EN ISO 6508-1:2005
Tensile Strength, Ultimate 860 - 880 MPa125000 - 128000 psiin vertical direction (Z), As built; ISO 6892-1 B10
 975 - 985 MPa141000 - 143000 psiin horizontal direction (XY), As built; ISO 6892-1 B10
 880 - 900 MPa
@Treatment Temp. 870 °C,
Time 3600 sec
128000 - 131000 psi
@Treatment Temp. 1600 °F,
Time 1.00 hour
in vertical direction (Z), Heat treated; ISO 6892-1 B10
 990 - 1010 MPa
@Treatment Temp. 870 °C,
Time 3600 sec
144000 - 146000 psi
@Treatment Temp. 1600 °F,
Time 1.00 hour
in horizontal direction (XY), Heat treated; ISO 6892-1 B10
Tensile Strength, Yield 625 - 635 MPa90600 - 92100 psiin vertical direction (Z), As built; ISO 6892-1 B10
 715 - 725 MPa104000 - 105000 psiin horizontal direction (XY), As built; ISO 6892-1 B10
 635 - 645 MPa
@Treatment Temp. 870 °C,
Time 3600 sec
92100 - 93500 psi
@Treatment Temp. 1600 °F,
Time 1.00 hour
in vertical direction (Z), Heat treated; ISO 6892-1 B10
 675 - 685 MPa
@Treatment Temp. 870 °C,
Time 3600 sec
97900 - 99400 psi
@Treatment Temp. 1600 °F,
Time 1.00 hour
in horizontal direction (XY), Heat treated; ISO 6892-1 B10
Elongation at Break 31 - 35 %31 - 35 %in horizontal direction (XY), As built; ISO 6892-1 B10
 46 - 50 %46 - 50 %in vertical direction (Z), As built; ISO 6892-1 B10
 32 - 36 %
@Treatment Temp. 870 °C,
Time 3600 sec
32 - 36 %
@Treatment Temp. 1600 °F,
Time 1.00 hour
in horizontal direction (XY), Heat treated; ISO 6892-1 B10
 47 - 51 %
@Treatment Temp. 870 °C,
Time 3600 sec
47 - 51 %
@Treatment Temp. 1600 °F,
Time 1.00 hour
in vertical direction (Z), Heat treated; ISO 6892-1 B10
 
Component Elements PropertiesMetricEnglishComments
Aluminum, Al <= 0.40 %<= 0.40 %
Carbon, C <= 0.10 %<= 0.10 %
Chromium, Cr 20 - 23 %20 - 23 %
Cobalt, Co <= 1.0 %<= 1.0 %
Iron, Fe <= 5.0 %<= 5.0 %
Manganese, Mn <= 0.50 %<= 0.50 %
Molybdenum, Mo 8.0 - 10 %8.0 - 10 %
Nickel, Ni 58 - 68.85 %58 - 68.85 %Balance
Niobium, Nb (Columbium, Cb) 3.15 - 4.15 %3.15 - 4.15 %
Phosphorus, P <= 0.015 %<= 0.015 %
Silicon, Si <= 0.50 %<= 0.50 %
Sulfur, S <= 0.015 %<= 0.015 %
Tantalum, Ta <= 0.050 %<= 0.050 %
Titanium, Ti <= 0.40 %<= 0.40 %
 
Descriptive Properties
Surface roughness1-5 µmRa, after shot peening
 3-10 µmRz, after shot peening
Volume rate4.2 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.

NEOS930 / 280590

Please read our License Agreement regarding materials data and our Privacy Policy. Questions or comments about MatWeb? Please contact us at info@matweb.com. We appreciate your input.

The contents of this web site, the MatWeb logo, and "MatWeb" are Copyright 1996-2024 by MatWeb, LLC. MatWeb is intended for personal, non-commercial use. The contents, results, and technical data from this site may not be reproduced either electronically, photographically or substantively without permission from MatWeb, LLC.