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Data Sheet:

Alloy X

Chemical Composition Limits
Weight % C Cr Co Fe Mn Mo Ni Si W P S
Alloy X 0.05 - 0.15 20.5- 23.0 0.5- 2.5 17.0- 20.0 1 max 8-10 Bal 1 max 0.2- 1.0 0.04 max 0.03 max

  

Alloy X is a nickel-chromium-iron-molybdenum alloy with exceptional resistance to oxidation and outstanding strength, this alloy is used in nuclear engineering and heat treating furnaces. Alloy X is also know as Alloy HX®, Hastelloy X® and Inconel HX®

  

Availability

Alloy X is available in Bar (Round), Rod, Strip, Plate, Sheet, Wire, Pipe, Tube, Forging Stock, Extruded Section and Welding Wire.  For all stock availability contact Sales.

  

Specifications

Sheet AMS 5536, ASTM B435, ASME SB 435, HR204, ISO 6208, DIN 17750, AECMA PrEN2185, AIR 9165-43, LW2.4665 Part 1
Strip AMS 5536, ASTM B435, ASME SB 435, HR204, ISO 6208, DIN 17750, AECMA PrEN2185, LW2.4665 Part 1
Plate AMS 5536, ASTM B435, ASME SB 435, HR204, ISO 6208, DIN 17750, AECMA PrEN2185
Bar AMS 5754, HR6, ISO 9723, DIN 17752, AECMA PrEN2182, AIR 9165-43, LW2.4665 Part 2
Tube

ASTM B775, ASTM B829, ASME SB 751, ASME SB 829, ISO 6207, DIN 17751

Welded AMS 5588, ASTM B751, ASME SB 626

Seamless AMS 5587, ASTM B622, ASME SB 622
Pipe

ASTM B775, ASTM B 829, ASME SB 775, ASME SB 829, DIN 17751

Welded ASTM B619, ASME SB 619

Seamless ASTM B622, ASME SB 622
Fittings ASTM B366, ASME SB 366
Rod ASME SB 572, DIN 17752
Forgings AMS 5754, HR6, ISO 9725, DIN 17754, AECMA PrEN2182, AECMA PrEN2183, AIR 9165-43,  LW2.4665 Part 2
Rings AMS 5754
Wire AMS 5798, ISO 9724, DIN 17753
Billet HR6
Other UNS N06002

  

Typical Mechanical Properties

Rupture Strength (1000 h)
Temperature psi MPa
760°C / 1400°F 16,000 110
815°C / 1500°F 10,500 72
870°C / 1600°F 6500 45
925°C / 1700°F 3800 26
980°C / 1800°F 2200 15

(This material was Annealed)

Availability

 

Disclaimer

Every effort is made to ensure that technical specifications are accurate. However, technical specifications included herein should be used as a guideline only. All specifications are subject to change without notice.

 

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