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Carpenter Custom Age 625 PLUS® Nickel-Base Alloy, Aged 732°C (1350°F)/4hr/AC
Categories: Metal; Nonferrous Metal; Nickel Alloy; Superalloy

Material Notes: Data provided by Carpenter Technology Corporation.

Custom Age 625 PLUS® alloy is a precipitation hardenable, nickel-base alloy which, in many environments, displays corrosion resistance similar to that of Alloy 625 and superior to that of Alloy 718. A yield strength (0.2% offset) above 120 ksi (827 MPa) can be obtained by aging without prior warm or cold working. The precipitation hardening capability is particularly important in applications where large-section size or intricate shape precludes warm working. In the age hardened (high strength) condition, Custom Age 625 PLUS alloy offers exceptional resistance to stress corrosion cracking as well as general, pitting and crevice corrosion.

Custom Age 625 PLUS alloy could be considered for applications where severely corrosive environments are a concern, such as those encountered in deep sour gas wells as well as in a variety of refinery and chemical process industry applications. In addition, Custom Age 625 PLUS alloy could be considered a candidate for use in marine environments, where Alloy 625 has been used successfully. The higher strength capability of Custom Age 625 PLUS alloy may be particularly useful for fasteners and shafts.

Custom Age 625 PLUS® is a registered trademark of Carpenter Technology Corporation.

Key Words: UNS N07716; NACE MR0175; ASTM B805; AMS 5854
Vendors: Visit metalmen for your metals needs. Products include special chemistry, tight tolerances, custom tempers, odd dimensions/forms, and small quantities. Phone 1-800-767-9494.

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Physical PropertiesOriginal ValueComments
Density 8.40 g/cc
 
Mechanical PropertiesOriginal ValueComments
Hardness, Brinell 290Estimated from Rockwell C for 3000 kg load, 10 mm ball Brinell measurement.
Hardness, Knoop 315Estimated from Rockwell C
Hardness, Rockwell C 30
Hardness, Vickers 304Estimated from Rockwell C
Tensile Strength, Ultimate 1117 MPa
Tensile Strength, Yield 710 MPa
@Strain 0.2 %
Elongation at Break 48 %In 4D
Reduction of Area 65 %
Modulus of Elasticity 207 GPa
@Temperature 23.0 °C
Fatigue Strength 690 MPa
@# of Cycles 5.00e+6
smooth, axial
 
Electrical PropertiesOriginal ValueComments
Electrical Resistivity 0.0001299 ohm-cm
 
Thermal PropertiesOriginal ValueComments
CTE, linear 12.6 µm/m-°C
@Temperature 25.0 - 100 °C
 13.4 µm/m-°C
@Temperature 25.0 - 300 °C
 14.0 µm/m-°C
@Temperature 25.0 - 500 °C
Specific Heat Capacity 0.418 J/g-°C
Melting Point 1257 - 1356 °C
Solidus 1257 °C
Liquidus 1356 °C
 
Component Elements PropertiesOriginal ValueComments
Aluminum, Al <= 0.35 %
Carbon, C <= 0.030 %
Chromium, Cr 19 - 22 %
Iron, Fe 5.0 %as remainder
Manganese, Mn <= 0.20 %
Molybdenum, Mo 7.0 - 9.5 %
Nickel, Ni 59 - 63 %
Niobium, Nb (Columbium, Cb) 2.75 - 4.0 %
Phosphorus, P <= 0.015 %
Silicon, Si <= 0.20 %
Sulfur, S <= 0.010 %
Titanium, Ti 1.0 - 1.6 %

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 go back to viewing the property data in MatWeb's normal format.

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