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
  

Ensinger PEI

EOS CobaltChrome MP1 Cobalt-Chrome-Molybdenum-Based Superalloy Powder Processed by DMSL on EOSINT M 270 and EOSINT M 280
Categories: Metal; 3D Printing/Additive Manufacturing Metal; Superalloy; Cobalt Base

Material Notes: Description: Parts built from EOS CobaltChrome MP1 conform to the chemical composition UNS R31538 of high carbon CoCrMo alloy. They are nickel-free (< 0.1 % nickel content) and are characterized by a fine, uniform crystal grain structure. As built EOS CobaltChrome MP1 meets the chemical and mechanical specifications of ISO 5832-4 and ASTM F75 for cast CoCrMo implant alloys, as well as the specifications of ISO 5832-12 and ASTM F1537 for wrought CoCrMo implants alloys except remaining elongation. The remaining elongation can be increased to fulfil even these standards by high temperature stress relieving or hot isostatic pressing (HIP). Parts made from EOS CobaltChrome MP1 can be machined, spark-eroded, welded, micro shot peened, polished and coated if required. They are suitable for biomedical applications (note: subject to fulfillment of statutory validation requirements where appropriate), and for parts requiring high mechanical properties in elevated temperatures (500 - 1000 °C) and with good corrosion resistance. Due to the layerwise building method, the parts have a certain anisotropy, which can be reduced or removed by appropriate heat treatment - see Technical Data for examples.

Stress relieved: High temperature stress relieved, 6 hours at 1150 °C (2100 °F) under inert argon atmosphere

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 PropertiesMetricEnglishComments
Density 8.30 g/cc0.300 lb/in³
 
Mechanical PropertiesMetricEnglishComments
Hardness, Rockwell C 35.0 - 45.035.0 - 45.0EN ISO 6508-1
Tensile Strength 1000 - 1200 MPa145000 - 174000 psiin vertical direction (Z), Stress relieved; ISO 6892 -1:2009 (B) Annex D
 1000 - 1200 MPa145000 - 174000 psiin horizontal direction (XY), Stress relieved; ISO 6892 -1:2009 (B) Annex D
 1050 - 1350 MPa152000 - 196000 psiin vertical direction (Z), As built; ISO 6892 -1:2009 (B) Annex D
 1250 - 1450 MPa181000 - 210000 psiin horizontal direction (XY), As built; ISO 6892 -1:2009 (B) Annex D
Tensile Strength, Yield  550 - 650 MPa
@Strain 0.2 %
79800 - 94300 psi
@Strain 0.2 %
in vertical direction (Z), Stress relieved; ISO 6892 -1:2009 (B) Annex D
 550 - 650 MPa
@Strain 0.2 %
79800 - 94300 psi
@Strain 0.2 %
in horizontal direction (XY), Stress relieved; ISO 6892 -1:2009 (B) Annex D
 700 - 900 MPa
@Strain 0.2 %
102000 - 131000 psi
@Strain 0.2 %
in vertical direction (Z), As built; ISO 6892 -1:2009 (B) Annex D
 960 - 1160 MPa
@Strain 0.2 %
139000 - 168000 psi
@Strain 0.2 %
in horizontal direction (XY), As built; ISO 6892 -1:2009 (B) Annex D
Elongation at Break 8.00 - 14.0 %8.00 - 14.0 %in horizontal direction (XY), As built; ISO 6892 -1:2009 (B) Annex D
 >= 20.0 %>= 20.0 %in horizontal direction (XY), Stress relieved; ISO 6892 -1:2009 (B) Annex D
 >= 20.0 %>= 20.0 %in vertical direction (Z), Stress relieved; ISO 6892 -1:2009 (B) Annex D
 20.0 - 28.0 %20.0 - 28.0 %in vertical direction (Z), As built; ISO 6892 -1:2009 (B) Annex D
Modulus of Elasticity 170 - 210 GPa24700 - 30500 ksiin vertical direction (Z), As built; ISO 6892 -1:2009 (B) Annex D
 180 - 220 GPa26100 - 31900 ksiin vertical direction (Z), Stress relieved; ISO 6892 -1:2009 (B) Annex D
 180 - 220 GPa26100 - 31900 ksiin horizontal direction (XY), As built; ISO 6892 -1:2009 (B) Annex D
 180 - 220 GPa26100 - 31900 ksiin horizontal direction (XY), Stress relieved; ISO 6892 -1:2009 (B) Annex D
Fatigue Strength 560 MPa81200 psimax. stress to reach 10 million cycles, under 250 MPa stress amplitude and 44 Hz testing frequency; ASTM E466:1996,
 660 MPa95700 psimax. stress to reach 1 million cycles, under 250 MPa stress amplitude and 44 Hz testing frequency; ASTM E466:1996,
 
Thermal PropertiesMetricEnglishComments
CTE, linear  13.6 µm/m-°C
@Temperature 20.0 - 500 °C
7.56 µin/in-°F
@Temperature 68.0 - 932 °F
 15.1 µm/m-°C
@Temperature 500 - 1000 °C
8.39 µin/in-°F
@Temperature 932 - 1830 °F
Thermal Conductivity  13.0 W/m-K
@Temperature 20.0 °C
90.2 BTU-in/hr-ft²-°F
@Temperature 68.0 °F
 18.0 W/m-K
@Temperature 300 °C
125 BTU-in/hr-ft²-°F
@Temperature 572 °F
 22.0 W/m-K
@Temperature 500 °C
153 BTU-in/hr-ft²-°F
@Temperature 932 °F
 33.0 W/m-K
@Temperature 1000 °C
229 BTU-in/hr-ft²-°F
@Temperature 1830 °F
Melting Point 1350 - 1430 °C2460 - 2610 °F
Maximum Service Temperature, Air 1150 °C2100 °F
 
Component Elements PropertiesMetricEnglishComments
Carbon, C <= 0.160 %<= 0.160 %
Chromium, Cr 26.0 - 30.0 %26.0 - 30.0 %
Cobalt, Co 60.0 - 65.0 %60.0 - 65.0 %
Iron, Fe <= 0.750 %<= 0.750 %
Manganese, Mn <= 1.00 %<= 1.00 %
Molybdenum, Mo 5.00 - 7.00 %5.00 - 7.00 %
Nickel, Ni <= 0.100 %<= 0.100 %
Silicon, Si <= 1.00 %<= 1.00 %

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.

NPROTO802 / 322915

Proto3000 – 3D Engineering Solutions

Please read our License Agreement regarding materials data and our Privacy Policy. Questions or comments about MatWeb? Please contact us at webmaster@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.