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Hastelloy X

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Product Description

Description:

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 China Special Bolts
• 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

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