Alloy 625

Alloy 625UNS N06625

Availability

  • Welded Pipe 1/2″ – 8″
  • Butt-Weld Fittings 1/2″ – 8″
  • Flanges 1/2″ – 8″
  • Bar 1″ – 4-1/2″

Specifications

  • ASTM B443, B705, B366, B446, B564
  • ASME SB443, SB705, SB366, SB446, SB564

Chemical Composition

C Cr Fe Ni Al Ti Co + TA
Max - Max Min Max Max -
0.10 20.0 – 23.0 5.0 58.0 0.40 0.40 3.15 – 4.15
Alloy 625 is a Nickel-Chromium alloy used for its high strength, excellent fabricability and outstanding corrosion resistance. Service temperatures range from cryogenic to 1800 ̊ F. Alloy 625 strength is derived from the stiffening effect of molybdenium and columbium on its Nickel-Chromium matrix; thus precipitation-hardening treatments are not required. This combination of elements also is responsible for superior resistance to a wide range of corrosive environments of unusual severity as well as to high-temperature effects such as oxidation and carburization.
  • Outstanding resistance to pitting, crevice corrosion, impingement corrosion and intergranular attack.
  • Almost complete freedom from Chloride- induced stress corrosion cracking.
  • Good resistance to mineral acids, such as nitric, phosphoric, sulphuric and hydrochloric acids.
  • Good resistance to alkalis and organic acids.
  • Good mechanical properties.
  • Used for structures in contact with seawater and subject to high mechanical stresses
  • Flue gas scrubbers components
  • Chimney linings
  • Superphosphoric acid production equipment
  • Sour gas production tubes
  • Offshore industry, marine equipment
  • High tensile, creep, rupture strength, outstanding fatigue and thermal-fatigue strength; oxidation resistance; and excellent weldability and brazeability make it a good choice in the aerospace industry
Tensile Strength
(KSI)
120
Yield Strength
(KSI)
60

KSI can be converted to MPA (Megapascals) by multiplying by 6.895.

 
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