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Ensinger PEI

MAR-M246 Cast Nickel Superalloy
Categories: Metal; Superalloy; Nickel Base

Material Notes: Typical Applications: Jet engine blades; better ductility than MAR-M200

Mechanical property data for 'as-cast' samples.

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Physical PropertiesMetricEnglishComments
Density 8.44 g/cc0.305 lb/in³
 
Mechanical PropertiesMetricEnglishComments
Rupture Strength  41.4 MPa
@Temperature 1090 °C,
Time 3.60e+6 sec
6000 psi
@Temperature 2000 °F,
Time 1000 hour
 68.9 MPa
@Temperature 1090 °C,
Time 360000 sec
10000 psi
@Temperature 2000 °F,
Time 100 hour
 124 MPa
@Temperature 982 °C,
Time 3.60e+6 sec
18000 psi
@Temperature 1800 °F,
Time 1000 hour
 186 MPa
@Temperature 982 °C,
Time 360000 sec
27000 psi
@Temperature 1800 °F,
Time 100 hour
 448 MPa
@Temperature 816 °C,
Time 3.60e+6 sec
65000 psi
@Temperature 1500 °F,
Time 1000 hour
 565 MPa
@Temperature 816 °C,
Time 360000 sec
82000 psi
@Temperature 1500 °F,
Time 100 hour
 
Component Elements PropertiesMetricEnglishComments
Aluminum, Al 5.5 %5.5 %
Boron, B 0.015 %0.015 %
Carbon, C 0.15 %0.15 %
Chromium, Cr 9.0 %9.0 %
Cobalt, Co 10 %10 %
Copper, Cu 0.10 %0.10 %
Iron, Fe 0.15 %0.15 %
Manganese, Mn 0.10 %0.10 %
Nickel, Ni 61.885 %61.885 %As Balance
Silicon, Si 0.050 %0.050 %
Tantalum, Ta 1.5 %1.5 %
Titanium, Ti 1.5 %1.5 %
Tungsten, W 10 %10 %
Zirconium, Zr 0.050 %0.050 %

References for this datasheet.

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.

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