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Nickel Alloy 725 / Inconel 725®

Technical Data Sheet

Alloy 725 (UNS N07725) is a nickel-chromium-molybdenum-niobium alloy that is highly resistant to corrosion and has been age hardened for extremely high strength twice that of annealed alloy 625. Alloy 725 strength is developed by heat treatment rather than by cold work this also enables strength to be imparted to large non-uniform sections that cannot be strengthened by cold works. Alloy 725 is used for hangers, landing nipples and high strength fasteners in marine applications.

Chemical Composition Limits
Weight%NiCrMoNbTiAlCMnSiPSFe
Alloy 72555.0-59.019.0 -22.57.0-9.52.75-4.01.0-1.70.35 max0.03 max0.35 max0.20 max0.015 max0.010 maxRem

Typical Mechanical Properties

MaterialForm and ConditionYield Strength (0.2% Offset)Tensile StrengthElongation %Hardness, Rc
ksiMPaksiMPa
Alloy 725 roundAnnealed
62.0427124.0855575
Alloy 725 roundAge Hardened133.0917180.012413036
Transverse Specimens from hot-finished rounds of 4.0 to 7.5 in (102 to 190mm) diameter

Availability

Alloy 725 is available in Bar, Round Bar, Flat Bar, Forging Stock. Contact Sales for further availability.

Specifications

Bar and Wire ASTM B 805, ASME Code Case 2217

Bar and Forging Stock SMC Specification HA91, ASME Code Case 2217

UNS N07725

FMC Spec M40504

NACE MR-0175/ ISO 15156

Inconel 725 (trademark)

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