Waspaloy® Nickel Superalloy, Heat Treatment: 1010°C (1850°F) + Age
Subcategory: Metal; Nickel Base; Superalloy
Key Words: Allvac, an Allegheny Teledyne Company, UNS N07001; AMS 5704, 5706, 5707, 5708. ASTM B 637
| Component | Wt. % |  | | | Al | 1.4 | | | B | 0.01 | | | C | 0.05 | | | Co | 13 | |
| | Component | Wt. % | | | | Cr | 19.5 | | | Fe | 1 | | | Mo | 4.3 | |
| | Component | Wt. % | | | | Ni | 57 | | | Ti | 3 | | | Zr | 0.7 | |
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Material Notes:
Nickel content calculated as remainder. Data provided by Allvac. Applications: Turbine compressor blades and discs, shafts, spacers, fasteners, miscellaneous jet engine hardware; space shuttle turbo pump seals. Waspaloy is a registered trademark of Pratt & Whitney Aircraft.
| Physical Properties | Metric | English | Comments |
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| Density | 8.19 g/cc | 0.296 lb/in³ | |
Mechanical Properties |
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| Hardness, Brinell | 351 | 351 | Estimated from Rockwell C value for Brinell test with 3000 kg load/10 mm diameter ball |
| Hardness, Knoop | 382 | 382 | Estimated from Rockwell C value. |
| Hardness, Rockwell C | 38 | 38 | |
| Hardness, Vickers | 367 | 367 | Estimated from Rockwell C value. |
| Tensile Strength, Ultimate | 1276 MPa | 185000 psi | |
| Tensile Strength, Yield | 897 MPa | 130000 psi | 0.2% Offset |
| Elongation at Break | 23 % | 23 % | |
| Reduction of Area | 25 % | 25 % | |
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