ATI 720 (Ni-Cr-Co-Mo-W-Ti-Al precipitation-hardened superalloy) vs ATI 75 (UNS N06075)
Property comparison of ATI 720 (Ni-Cr-Co-Mo-W-Ti-Al precipitation-hardened superalloy) and ATI 75 (UNS N06075), both nickel alloy.
| Property | ATI 720 (Ni-Cr-Co-Mo-W-Ti-Al precipitation-hardened superalloy) | ATI 75 (UNS N06075) | Difference |
|---|---|---|---|
| Yield strength | 1,207 MPa | 448 MPa | -63% |
| Tensile strength | 1,586 MPa | 813 MPa | -49% |
| Elongation | 18 % | 32 % | +78% |
| Density | 8,090 kg/m³ | 8,370 kg/m³ | +3% |
Difference is ATI 75 (UNS N06075) relative to ATI 720 (Ni-Cr-Co-Mo-W-Ti-Al precipitation-hardened superalloy). Values are taken from the representative row of each material; both materials may have multiple heat treatments or conditions on their individual pages.
Identification
- grade
- Proprietary (Rolls Royce MSRR7252 / GE C50TF105)
- standard
- ATI Technical Data Sheet
- heat treatment
- Solution treat 1080-1100°C/4h OQ + age 650°C/24h AC + 760°C/16h AC
- grade
- N06075
- standard
- ATI Technical Data Sheet
- heat treatment
- Solution Annealed
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