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Carpenter Custom Age 625 PLUS® Nickel-Base Alloy, Double Aged 732°C/8hr/FC to 621°C/8hr/AC

Category Metal , Nonferrous Metal , Nickel Alloy , Superalloy
Manufacturer Carpenter Technology Corporation (Cartech)
Trade Name
Port Ningbo port,China
Trade Terms FOB, CFR, CIF
Payment Terms L/C, T/T, Western Union
Download PDF Carpenter Custom Age 625 PLUS® Nickel-Base Alloy, Double Aged 732°C/8hr/FC to 621°C/8hr/AC.pdf
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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. 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.
Physical Properties Metric English Comments
Density 8.40 g/cc
0.303 lb/in³
Mechanical Properties Metric English Comments
Tensile Strength, Ultimate 1262 MPa
183000 psi
1055 MPa

@Temperature 538 °C
 153000 psi

@Temperature 1000 °F
1069 MPa

@Temperature 649 °C
 155000 psi

@Temperature 1200 °F
1069 MPa

@Temperature 427 °C
 155000 psi

@Temperature 801 °F
1104 MPa

@Temperature 316 °C
 160100 psi

@Temperature 601 °F
1152 MPa

@Temperature 232 °C
 167100 psi

@Temperature 450 °F
1186 MPa

@Temperature 177 °C
 172000 psi

@Temperature 351 °F
Tensile Strength, Yield 883 MPa

@Strain 0.200 %
 128000 psi

@Strain 0.200 %
773 MPa

@Strain 0.200 %,
Temperature 649 °C
 112000 psi

@Strain 0.200 %,
Temperature 1200 °F
787 MPa

@Strain 0.200 %,
Temperature 316 °C
 114000 psi

@Strain 0.200 %,
Temperature 601 °F
787 MPa

@Strain 0.200 %,
Temperature 538 °C
 114000 psi

@Strain 0.200 %,
Temperature 1000 °F
787 MPa

@Strain 0.200 %,
Temperature 427 °C
 114000 psi

@Strain 0.200 %,
Temperature 801 °F
800 MPa

@Strain 0.200 %,
Temperature 232 °C
 116000 psi

@Strain 0.200 %,
Temperature 450 °F
821 MPa

@Strain 0.200 %,
Temperature 177 °C
 119000 psi

@Strain 0.200 %,
Temperature 351 °F
Elongation at Break 33 %
33 %
In 4D
25 %

@Temperature 649 °C
 25 %

@Temperature 1200 °F
 In 4D
31 %

@Temperature 538 °C
 31 %

@Temperature 1000 °F
 In 4D
32 %

@Temperature 316 °C
 32 %

@Temperature 601 °F
 In 4D
32 %

@Temperature 427 °C
 32 %

@Temperature 801 °F
 In 4D
34 %

@Temperature 232 °C
 34 %

@Temperature 450 °F
 In 4D
34 %

@Temperature 177 °C
 34 %

@Temperature 351 °F
 In 4D
Reduction of Area 56 %
56 %
31 %

@Temperature 649 °C
 31 %

@Temperature 1200 °F
52 %

@Temperature 538 °C
 52 %

@Temperature 1000 °F
54 %

@Temperature 427 °C
 54 %

@Temperature 801 °F
59 %

@Temperature 316 °C
 59 %

@Temperature 601 °F
59 %

@Temperature 177 °C
 59 %

@Temperature 351 °F
60 %

@Temperature 232 °C
 60 %

@Temperature 450 °F
Modulus of Elasticity 207 GPa

@Temperature 23.0 °C
 30000 ksi

@Temperature 73.4 °F
Thermal Properties Metric English Comments
CTE, linear 12.6 µm/m-°C

@Temperature 25.0 - 100 °C
 7.00 µin/in-°F

@Temperature 77.0 - 212 °F
13.4 µm/m-°C

@Temperature 25.0 - 300 °C
 7.44 µin/in-°F

@Temperature 77.0 - 572 °F
14.0 µm/m-°C

@Temperature 25.0 - 500 °C
 7.78 µin/in-°F

@Temperature 77.0 - 932 °F
Specific Heat Capacity 0.418 J/g-°C
0.0999 BTU/lb-°F
Melting Point 1257 - 1356 °C
2295 - 2473 °F
Solidus 1257 °C
2295 °F
Liquidus 1356 °C
2473 °F
Component Elements Properties Metric English Comments
Aluminum, Al <= 0.35 %
<= 0.35 %
Carbon, C <= 0.030 %
<= 0.030 %
Chromium, Cr 19 - 22 %
19 - 22 %
Iron, Fe 5.0 %
5.0 %
as remainder
Manganese, Mn <= 0.20 %
<= 0.20 %
Molybdenum, Mo 7.0 - 9.5 %
7.0 - 9.5 %
Nickel, Ni 59 - 63 %
59 - 63 %
Niobium, Nb (Columbium, Cb) 2.75 - 4.0 %
2.75 - 4.0 %
Phosphorous, P <= 0.015 %
<= 0.015 %
Silicon, Si <= 0.20 %
<= 0.20 %
Sulfur, S <= 0.010 %
<= 0.010 %
Titanium, Ti 1.0 - 1.6 %
1.0 - 1.6 %
Electrical Properties Metric English Comments
Electrical Resistivity 0.0001299 ohm-cm
0.0001299 ohm-cm
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