Waspaloy/UNS N07001
Grade: Waspaloy/UNS N07001/W.Nr 2.4654/Nickel Alloy Waspaloy
Sheet/Plate: 0.3mm-150mm
Strip/Foil: 0.02mm-16mm
Pipe: 6mm*0.5mm-1200mm*100mm
Bar: Ф6mm – Ф600mm
Wire: Ф0.01mm – Ф6mm
Others: Forged Rings, Flanges, Elbows, Tees, Reducers etc.
Standard: ASTM/ASME/AMS
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WASPALOY is a nickel based age hardenable alloy that possesses high temperature strength while still having a good corrosion resistance, especially to oxidation. WASPALOY can be used at temperatures up to 650°C (1200°F) which is critical rotating applications. WASPALOY is used in gas turbine engine components, missile systems, shafts, spacers, seals, rings, casings, fasteners and many other uses in engine hardware, airframe assemblies.
| Chemical Composition Limits | |||||||||||||||
| Weight % | Cr | B | Zr | Al | Ti | Mo | Co | Cu | Fe | S | Si | Mn | C | P | Ni |
| Waspaloy | 18-21 | 0.003-00.1 | 0.02-0.12 | 1.2-1.6 | 2.75-3.25 | 3.5-5.0 | 12-15 | 0.50 max | 2 max | 0.030 max | 0.75 max | 1 max | 0.02-0.10 max | 0.030 max | Bal |
Typical Mechanical Properties
| Material | Condtion | Thickness | Temp | Tensile Strength ksi | Yield Strength ksi | Elongation in 4D | Hardness HRC |
| Sheet | Sol Treated, Stabilization + Precipitation HT | 0-0.020″ | Room | 170 | 110 | 15 | 34-44 |
| Sheet | Sol Treated, Stabilization + Precipitation HT | 0-0.020″ | 1000°F | 145 | 100 | 13 | |
| Sheet | Sol Treated, Stabilization + Precipitation HT | over 0.020″ | Room | 175 | 115 | 20 | 34-44 |
| Sheet | Sol Treated, Stabilization + Precipitation HT | over 0.020″ | 1000°F | 150 | 105 | 15 |
Specifications
Rod, Bar, Wire and Forging Stock
ASTM B 637, ISO 9723, ISO 9724, ISO 9725, AMS 5704, AMS 5706, AMS 5707, AMS 5708, AMS 5709, AMS 5828, MAM 5706, AECMA PrEN 2193, AECMA PrEN 2194, AECMA PrEN 2406, AECMA PrEN 2958, AECMA PrEN 2959, AECMA PrEN 2960, AECMA PrEN 3220.
Plate, Sheet and Strip
AMS 5544, AECMA PrEN 2195
Other
UNS N07001, W. Nr 2.4654, MSRR 7192


WASPALOY is a nickel based age hardenable alloy that possesses high temperature strength while still having a good corrosion resistance, especially to oxidation. WASPALOY can be used at temperatures up to 650°C (1200°F) which is critical rotating applications. WASPALOY is used in gas turbine engine components, missile systems, shafts, spacers, seals, rings, casings, fasteners and many other uses in engine hardware, airframe assemblies.
| Chemical Composition Limits | |||||||||||||||
| Weight % | Cr | B | Zr | Al | Ti | Mo | Co | Cu | Fe | S | Si | Mn | C | P | Ni |
| Waspaloy | 18-21 | 0.003-00.1 | 0.02-0.12 | 1.2-1.6 | 2.75-3.25 | 3.5-5.0 | 12-15 | 0.50 max | 2 max | 0.030 max | 0.75 max | 1 max | 0.02-0.10 max | 0.030 max | Bal |
Typical Mechanical Properties
| Material | Condtion | Thickness | Temp | Tensile Strength ksi | Yield Strength ksi | Elongation in 4D | Hardness HRC |
| Sheet | Sol Treated, Stabilization + Precipitation HT | 0-0.020″ | Room | 170 | 110 | 15 | 34-44 |
| Sheet | Sol Treated, Stabilization + Precipitation HT | 0-0.020″ | 1000°F | 145 | 100 | 13 | |
| Sheet | Sol Treated, Stabilization + Precipitation HT | over 0.020″ | Room | 175 | 115 | 20 | 34-44 |
| Sheet | Sol Treated, Stabilization + Precipitation HT | over 0.020″ | 1000°F | 150 | 105 | 15 |
Specifications
Rod, Bar, Wire and Forging Stock
ASTM B 637, ISO 9723, ISO 9724, ISO 9725, AMS 5704, AMS 5706, AMS 5707, AMS 5708, AMS 5709, AMS 5828, MAM 5706, AECMA PrEN 2193, AECMA PrEN 2194, AECMA PrEN 2406, AECMA PrEN 2958, AECMA PrEN 2959, AECMA PrEN 2960, AECMA PrEN 3220.
Plate, Sheet and Strip
AMS 5544, AECMA PrEN 2195
Other
UNS N07001, W. Nr 2.4654, MSRR 7192
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