Rene 41® Nickel Superalloy, Heat Treatment: 1079°C (1975°F) + Age
Subcategory: Metal; Nickel Base; Superalloy
Key Words: Allvac, an Allegheny Teledyne Company, UNS N07041; AMS 5712, 5713; René 41 Nickel
| Component | Wt. % |  | | | Al | 1.6 | | | B | 0.007 | | | C | 0.06 | |
| | Component | Wt. % | | | | Co | 11 | | | Cr | 19 | | | Fe | 3 | |
| | Component | Wt. % | | | | Mo | 9.75 | | | Ni | 52 | | | Ti | 3.15 | |
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Material Notes:
Nickel content calculated as remainder. Data provided by Allvac. Applications: Jet and rocket engines, torque rings, afterburners, and hardware; space shuttle turbo pumps seals.
| Physical Properties | Metric | English | Comments |
|
| Density | 8.24 g/cc | 0.298 lb/in³ | |
Mechanical Properties |
|
| Hardness, Brinell | 334 | 334 | Estimated from Rockwell C value for Brinell test with 3000 kg load/10 mm diameter ball |
| Hardness, Knoop | 363 | 363 | Estimated from Rockwell C value. |
| Hardness, Rockwell C | 36 | 36 | |
| Hardness, Vickers | 349 | 349 | Estimated from Rockwell C value. |
| Tensile Strength, Ultimate | 1241 MPa | 180000 psi | |
| Tensile Strength, Yield | 793 MPa | 115000 psi | 0.2% Offset |
| Elongation at Break | 20 % | 20 % | |
| Reduction of Area | 25 % | 25 % | |
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