Material
Alloy X
International Codes
UNS N06002
24,665
Main Features
Corrosion Resistant
Density
8,22Kg/dm3
Chemical Composition
Cr
20,5-23%
Ni
Bal%
Mo
8-10%
Co
0,5-2,5%
NbTa
Al
Max 0,5%
Ti
Max 0,15%
C
0,05-0,15%
Fe
17-20%
Mn
max 1%
Si
Max 1%
P
Max 0,030%
S
Max 0,030%
CbTa
Max 0,5%
Cu
Altro
0,2-1%
Standards
ASTM
B435, B572
AMS
5536, 5754, 5798
General Proprieties
Alloy X (UNS N06002) is a nickel-based superalloy ideal for gas turbine engine, aircraft, industrial furnace, and chemical processing applications. Gas turbine engines use Alloy X flame holders, spray bars, transition ducts, combustor cans and other combustion-related parts. Alloy X also performs well in aircraft parts, including jet engine tailafterburner components, and cabin heaters. This alloy is also know as Hastelloy® X. Alloy X is available at CHUN & VOLLERIN in these formats: Bars, Plates, Pipes.
All data are to be considered typical for the product selected.
Refer to the production certificate for the specific characteristics of the product.
All the material has a UNI EN 10240 3.1 certificate with EU, USA and JP origin. All registered trademarks are the property of their respective owners.