Nickel Superalloy Waspaloy

 Technical Data Sheet

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.

Typical Mechanical Properties

Properties as per AMS 5544. Heat Treatment is as follows:
Annealing 1975°F / 30 mins and Air Cool
Solution Heat Treatment 1825°F / 2hrs and Air Cool
Stabilization Heat Treatment 1550°F /4hrs and Air Cool
Precipitation Heat Treatment 1400°F / 16 hrs and Air Cool
 
 Bar Properties
Properties as per AMS 5708 type 2 (capable of AMS 5709) Heat Treatment is as follows
Solution Treat 1900 - 1975°F / 1-4 hours and Air Cool
 Resulting hardness not higher than 302HB
Stabilization Heat Treatment Heat to 1550°F / 4 hrs and Air Cool
Precipitaion Heat Treatment Heat to 1400°F / 16 hrs and Air Cool
 Resulting hardness 32-42 HRC

Availability
 WASPALOY is available in Round Bar, Flat Bar, Forging Stock, Extruded Section, Wire, Plate, Sheet, Strip and Welding Wire. For all stock availability contact Sales.

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