This is a low-alloy, high-strength steel with high nickel and cobalt additions to promote toughness. The alloy has good hardenability and weldability and excellent fracture toughness. It is typically used in the 220/240 ksi (1520/1655Mpa) tensile strength range. For optimum cleanliness, the alloy is produced by the consumable electrode vacuum arc remelting process.
Aircraft structural components, rocket motor cases, armor plate, pressure vessels, gears
For ingot breakdown heat to 2200ºF (1205ºC) and to 1900ºF (1040ºC) for finish forging. Do not forge below 1700ºF (925ºC). Parts may be transferred to an annealing furnace after forging – see heat treatment.
1250ºF (675ºC) for 4 hours, air cool to room temp, plus 1150ºF (620ºC) for 4-8 hours and air cool. Alternative is a sub-critical anneal at 1150ºF (620ºC) for 12-24 hours and air cool.
would normally be carried out prior to hardening and tempering, at 1600-1700ºF (870-925ºC) for 1 hour followed by air cooling.
Austenitize at 1525-1575ºF (830-850ºC) for 1 hour and oil quench
At 400-1100ºF (205-595ºC) depending upon desired properties. Double tempering is recommended.
Refrigeration : this treatment would be carried out to remove any retained austenite, and might be performed at –100ºF (-73ºC) for 2 hours followed by air warm back to room temperature.
Those practices used for machining 4340 steel at similar hardness levels are recommended for HP 9-4-30 grade.
Helium-shielded TIG welding is the preferred method, using HP 9-4-30 filler wire.