Data Sheet

X

UNS N06002
Bars
Sheets/Plates
Tubes/Pipes
Material

Alloy X

International Codes

UNS N06002

2,4665

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 tailpipes, afterburner 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.

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