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Alloy MP159 (AMS 5841)

Technical Data Sheet

MP159 is a Nickel-Cobalt based multiphase alloy. This combination of properties enables ultra high strength, toughness, good ductility and excellent corrosion resistance. Through work strengthening and aging MP159 alloy exhibits ultimate tensile strength levels in excess of 1830 MPa. MP159 is used in many different industries from use in prosthetic devices, jet engine components, fasteners, marine applications to petroleum industry applications.

Chemical Composition Limits
Weight %NiCoCrFeMoTiCbAl
MP15925.535.719.09.07.03.00.60.2

Typical Mechanical Properties

MaterialCondtionTensile Strength ksiYield Strength ksiElongation %Reduction of Area %Hardness HRC
MP159Annealed
123586069
MP159AMS 5841160 max70 max506520 HRC max
MP159Annealed, Cold Worked 48%2302051246
MP159AMS 5842----

≥38HRC

MP159Annealed, Cold Worked + Aged275265835
MP159AMS 5843260 min250 min6 min20 min≥44HRC

Availability

Alloy MP159 is available in Bar (Round). For all stock availability contact Sales.

Specifications

UNS R30159

AMS 5841 Bar (Solution Heat Treated)

Solution Heat Treat: 1900°F - 1925°F / 4-8 hours + Water Quench

AMS 5842 Bar (Solution Heat Treated and Work Strengthened)

Solution Heat Treat: 1900°F - 1925°F / 4-8 hours + Water Quench

Followed by work strengthened / strain hardening

AMS 5843 Bar (Solution Heat Treated, Work Strengthened and Aged)

Solution Heat Treat: 1900°F - 1925°F / 4-8 hours + Water Quench

Followed by work strengthened / strain hardening

Ffollowed by ageing: 1200-1250°F 4-4.5 hours + Air Cool.

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