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Model No: AMS 5842H MP159

AMS 5842H MP159 Round Bar

AMS 5842H MP159 round bar is a cobalt-nickel superalloy achieving ultra-high tensile strength exceeding 1830 MPa (265 ksi) through cold work and aging.
Delivery :
FOB
minimum order :
50 kilograms
Supply Ability :
5000kilograms / Month
Stock Time :
7-10Day
Country of Origin :
CHINA
Quantity :
Contact Now

AMS 5842H covers MP159 cobalt-nickel-chromium alloy in the form of bars up to 1-3/4 inch (44 mm) nominal diameter or thickness. MP159 is a multiphase nickel-cobalt based superalloy that achieves ultra-high strength through a combination of cold work and aging. With ultimate tensile strength exceeding 1830 MPa (265 ksi), it offers an exceptional balance of strength, toughness, ductility, and corrosion resistance, making it indispensable for aerospace fasteners, jet engine components, marine hardware, and petroleum industry equipment .


1. Product Specifications & Physical Data

AMS 5842H specifies MP159 round bar for high-strength, corrosion-resistant, and heat-resistant applications. The alloy is supplied in the cold worked and aged condition to achieve its optimum mechanical properties.

  • Available Forms: Round bar (up to 44 mm diameter / 1-3/4 inch) .

  • Specifications: AMS 5842H, AMS 5841, AMS 5843, UNS R30159, NACE MR0175/ISO 15156 .

Chemical Composition (Weight %)MP159 Specification
Cobalt (Co)Balance
Nickel (Ni)24.0 - 27.0
Chromium (Cr)18.0 - 20.0
Molybdenum (Mo)6.0 - 8.0
Iron (Fe)8.0 - 10.0
Titanium (Ti)2.5 - 3.25
Niobium (Nb)0.20 - 0.80
Aluminum (Al)0.10 - 0.30
Carbon (C)0.04 max.
Manganese (Mn)0.20 max.
Silicon (Si)0.20 max.
Phosphorus (P)0.020 max.
Sulfur (S)0.010 max.
 
Physical PropertiesMetricImperial
Density8.33 - 8.45 g/cm³0.301 - 0.305 lb/in³
Melting Range1340 - 1400°C2445 - 2550°F
Modulus of Elasticity210 - 220 GPa30.5 - 32.0 × 10⁶ psi
Poisson's Ratio0.310.31
 
Mechanical Properties (Cold Worked + Aged)ValueUnit
Tensile Strength (min.)1830 MPa265 ksi
Yield Strength (0.2% offset, min.)1720 MPa250 ksi
Elongation (min.)8%8%
Reduction of Area (min.)35%35%
Hardness (min.)38 HRC38 HRC

 2. Fabrication & Material Comparison

  • Cold Working: 45-50% cold reduction is essential to activate age-hardening response; material supplied in cold worked condition .

  • Aging: 650-700°C (1200-1290°F) × 4-8 hours, air cool; develops full strength after cold work .

  • Machining: Difficult due to high strength and work-hardening rate; requires rigid setups, slow speeds, positive feeds, and ample coolant .

  • Welding: Limited weldability; components typically mechanically fastened rather than welded .

  • Material Comparison:

Property ComparisonMP159MP35NInconel 71817-4 PH
Tensile Strength (min.)265 ksi260 ksi185 ksi190 ksi
Corrosion ResistanceExcellentExcellentGoodGood
Sour Service (NACE)YesYesYes (limited)Yes (H1150M)
Service Temperature590°C590°C650°C315°C
FabricabilityModerateModerateGoodGood

3. Applications

  • Aerospace: High-strength fasteners (bolts, studs), jet engine components, landing gear hardware

  • Oil & Gas: Downhole tools, wellhead components, valve stems, packers, completion equipment

  • Marine: Subsea connectors, seawater handling components, propeller shafts

  • Medical: Prosthetic devices, orthopedic implants, surgical instruments

  • Industrial: High-strength springs, torsion bars, fasteners for corrosive environments

Contact ZYTC Alloy for certified AMS 5842H MP159 round bar with full traceability, NACE MR0175 certification, material test reports, and competitive pricing. Available in standard sizes up to 44 mm diameter.

Email: daisy@zytcsteel.com

WhatsApp/WeChat: +86 17335753350