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Metal Alloy Properties: nickel alloy
ATI 690 Bar to ATI C-263 Aged
Metal and alloy mechanical properties — tensile/yield strength, elastic modulus, density, hardness for steels, aluminum alloys, copper alloys, titanium, nickel alloys, cast iron, and more
| category | material id | cte per K (1/K) | density kg m3 (kg/m3) | elastic modulus MPa (MPa) | elongation percent (%) | grade | heat treatment | melting point C (°C) | name | property basis | reduction percent (%) | specific heat J kgK (J/(kg·K)) | standard | tensile strength MPa (MPa) | thermal conductivity W mK (W/(m·K)) | yield strength MPa (MPa) |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| nickel alloy | ATI 690 Bar | — | 8,190 | — | 45 | Ni-Cr-Fe (N06690) | Annealed (bar) | — | ATI 690 | Minimum | — | — | ASME SB-166; ASTM B-166 | 585 | — | 241 |
| nickel alloy | ATI 718-DA Aged | — | 8,190 | 200,000 | — | UNS N07718 | Direct age 718°C/8h FC to 621°C/8h AC (no solution treat) | 1,302 | ATI 718-DA (Inconel 718 Direct Age, thermo-mechanically processed) | Typical | — | — | ATI Technical Data Sheet | 1,531 | — | — |
| nickel alloy | ATI 718-HS Aged | — | 8,190 | 200,000 | — | UNS N07718 | Solution treat 941-1024°C + age 718°C/8h FC to 621°C | 1,302 | ATI 718-HS (Inconel 718 High Strength, thermo-mechanically processed) | Typical | — | — | ATI Technical Data Sheet | 1,365 | — | — |
| nickel alloy | ATI 718-OP STA | — | 8,190 | 200,000 | 25 | UNS N07718 | Solution treat 1021-1038°C/1-2h + age 774-802°C/6-8h AC | 1,301.5 | ATI 718-OP (Inconel 718 Oil Patch, solution treated and aged) | Typical | 35 | 444 | ATI Technical Data Sheet | 1,172 | — | 827 |
| nickel alloy | ATI 718Plus SolutionTreated | — | 8,250 | — | — | N07818 | Solution Treated 954-982C | 1,302 | ATI 718Plus (UNS N07818) Solution Treated | Typical | — | — | ATI Technical Data Sheet | — | — | — |
| nickel alloy | ATI 718Plus SolutionTreatedAndAged | — | 8,250 | 200,000 | 28 | N07818 | Solution Treated and Aged 788C/704C | 1,302 | ATI 718Plus (UNS N07818) Solution Treated and Aged | Typical | — | — | ATI Technical Data Sheet | 1,476 | — | 1,145 |
| nickel alloy | ATI 720 Aged | — | 8,090 | 220,000 | 18 | Proprietary (Rolls Royce MSRR7252 / GE C50TF105) | Solution treat 1080-1100°C/4h OQ + age 650°C/24h AC + 760°C/16h AC | — | ATI 720 (Ni-Cr-Co-Mo-W-Ti-Al precipitation-hardened superalloy) | Typical | — | — | ATI Technical Data Sheet | 1,586 | — | 1,207 |
| nickel alloy | ATI 75 Annealed | 0.000011 | 8,370 | — | 32 | N06075 | Solution Annealed | 1,360 | ATI 75 (UNS N06075) | Typical | — | 461 | ATI Technical Data Sheet | 813 | 12.1 | 448 |
| nickel alloy | ATI 901 Bar | — | 8,220 | — | 25 | Ni-Fe-Cr-Mo-Ti (N09901) | Aged (bar) | — | ATI 901 | Minimum | — | — | UNS N09901 | 1,276 | — | 1,172 |
| nickel alloy | ATI C-263 Aged | — | 8,360 | 220,000 | 35 | UNS N07263 | Solution anneal 1038-1177°C + age 802°C/8h AC (AMS 5872E) | — | ATI C-263 (Ni-Co-Cr-Mo precipitation-hardened superalloy, age hardened) | Typical | — | — | ATI Technical Data Sheet | 1,034 | — | 621 |
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