UNS Number N06002, DIN 2.4665
Hastelloy X / N6002 / GH32 / 2.4665
Hastelloy X is a nickel-chromium-iron-molybdenum alloy containing approximately 22% chromium for outstanding resistance to oxidation at high temperatures up to 1200°C.
Hastelloy X has good high temperature and stress rupture properties above 790°C (1450°F) and can be used for applications up to 1200°C (2200°F). With the high levels of chromium, nickel and molybdenum in the material, Hastelloy X exhibits levels of corrosion resistance similar to high nickel alloys more customarily used in corrosion applications.
Hastelloy X can be used in many industrial furnace applications because of its resistance to oxidizing, neutral and carburizing atmospheres; widely used for aircraft parts, such as jet engine tailpipes, afterburners, turbine blades, and vanes.
Forms of Hastelloy X Available at Zhonghai Alloy
• Sheet
• Plate
• Bar
Hastelloy X Chemical Composition:
| Grade | Ni% | Cr% | Fe% | Mo% | C% | Mn% | Si% | Co% | Al% | W% | B% | S% | P% |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Hastelloy X | Bal. | 20.5-23.5 | 17.0-20.0 | 8.0-10.0 | 0.05-0.15 | Max 1.0 | Max 1.0 | 0.5-2.5 | Max 0.1 | 0.2-1.0 | Max 0.005 | Max 0.01 | Max 0.015 |
Hastelloy X Physical Properties:
| Grade | Density | Melting Point |
| Hastelloy X | 8.3g/cm3 | 1260°C-1355°C |
ASTM Specifications
| Sheet/Plate | Bar |
|---|---|
| B435 | B572 |
