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ASTM F562 AMS 5844 5845 MP35n R30035 High Strength Cobalt Alloy Bar1
Non-ferrous Metal ProductsMP35n BarAMS 5844 Bar
Tianjin ZYTC Alloy Technology Co., Ltd
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Product Description ASTM F562 AMS 5844 MP35N R30035 High Strength Cobalt Alloy BarShapeRound,Forging,Ring,Coil,Flange,Disc,Foil,Spherical,Ribbon,Square,Bar,Pipe,SheetGradeDuplex: 2205(UNS S31803/S32205),2507(UNS S32750),UNS S32760(Zeron 100),2304,904L Others:253Ma,254SMo,654SMo,F50(UNSS32100)F60,F61,F65,1J22,N4,N6 etc Alloy : Alloy 20/28/31 Hastelloy:HastelloyB/ -2/B-3/C22/C-4/S/ C276/C-2000/G-35/G-30/X/N/g Hastelloy B / UNS N10001,Hastelloy B-2 / UNS N10665 / DIN W. Nr. 2.4617,Hastelloy C,Hastelloy C-4 / UNS N06455 / DIN W. Nr. 2.4610,Hastelloy C-22 / UNS N06022 / DIN W. Nr. 2.4602,Hastelloy C-276 / UNS N10276 / DIN W. Nr. 2.4819,Hastelloy X / UNS N06002 / DIN W. Nr. 2.4665 Haynes: Haynes 230/556/188/263 Inconel 600/601/602CA/617/625/713/718/738/X-750,Carpenter 20 Inconel 718 / UNS N07718 / DIN W. Nr. 2.4668,Inconel 601 / UNS N06601 / DIN W. Nr. 2.4851,Inconel 625 / UNS N06625 / DIN W. Nr. 2.4856,Inconel 725 / UNS N07725,Inconel X-750 / UNS N07750 / DIN W. Nr. 2.4669,Inconel 600 / UNS N06600 / DIN W. Nr. 2.4816 Incoloy: Incoloy 800/800H/800HT/825/925/926; GH: GH2132,GH3030,GH3039,GH3128,GH4180,GH3044 Monel: Monel 400/K500/R405 Nitronic: Nitronic 40/50/60; Nimonic: Nimonic 75/80A/90/A263 ; SpecificationWire: 0.01-10mmStrip: 0.05*5.0-5.0*250mm Bar: φ4-50mm;Length 2000-5000mmPipe: φ6-273mm;δ1-30mm;Length 1000-8000mmSheet: δ 0.8-36mm;Width 650-2000mm;Length 800-4500mmIntroductionMP35N is a vacuum induction, vacuum arc re-melted quaternary alloy based on nickel and cobalt with substantial additions of chromium and molybdenum. The alloy possesses an attractive combination of ultra-high-strength, toughness and outstanding corrosion resistance. MP35N alloy may be employed in the annealed condition but can easily be work strengthened to tensile strength levels in excess of 260 ksi (1,793 MPa) with the retention of good ductility. Ageing of worked material causes precipitation hardening and can raise the tensile strength by an additional 40 ksi (276 MPa). The density of MP35N alloy is 8.43 g/cc.Technical Data SheetMP35N? is a multi-phase alloy containing Nickel, Cobalt, Chromium and Molybdenum with a unique range of properties - ultra high strength, toughness, biocompatibility and corrosion resistance. It is produced by vacuum induction melting and vacuum arc re-melting (VIM-VAR) and is then strengthened by work hardening and aging, giving hardnesses of up to 55-60 Rockwell C and strength levels as high as 260-300KSI.Due, to this unique combination of properties, MP35N? has many applications in such industries as oil and gas, aerospace and medical. MP35N can be effectively used at cryogenic temperatures without embrittlement and maintain its properties at temperatures up to 600°F, and is also suitable for medical implants and orthodontic/prosthetic devices.MP35N? is able to resist corrosion to most mineral acid, hydrogen sulfide and seawater environments whilst exhibiting excellent resistance to stress corrosion cracking and hydrogen embrittlement, even at high strength levels. NACE MR0175 allows a hardness of up to 51 HRC for material that has been work strengthened and aged by one of the processes listed in the table below.Aircraft Materials supplies MP35N? in round bar certified to either AMS 5844 (0.270" - 1.520" diameter) or NACE MR0175 (0.5" - 2.5" diameter), as well as sheet, strip and plate products suitable for medical applications.Chemical Composition LimitsWeight %NiCoCrMoTiFeSiMnPBSCMP35N?33-37Bal19-219-10.51 max1 max0.15 max0.15 max0.015 max0.010 max0.010 max0.03 maxMP35N? is a registered trademark of SPS Technologies Inc. Typical Mechanical PropertiesMaterialCondtionUltimate Tensile Strength ksi0.2 % Yield Strength ksiElongation %Reduction of Area %Hardness HRCMP35N ?AMS 5844Solution Heat Treated and Work Strengthened255225125045MP35N?AMS 5845Solution Heat Treated and Work Strengthened and Aged26023083538 minAMS 5844 is Solution Treated and Cold Worked. The AMS specification only requires that the hardness shall not be lower than 38 HRC or equivalent. However other typical mechanical properties of AMS 5844 are detailed above.MaterialCondtionTensile Strength ksiYield Strength ksiElongation %Reduction of Area %Hardness HRCMP35N?NACE MR0175Age @ 1300°F/ 4 hrs220210104051 maxMP35N?NACE MR0175Age @ 1350°F / 4hrs210200104051 maxMP35N?NACE MR0175Age @ 1425°F / 6hrs190180104051 maxMP35N? Properties as per NACE MR0175 - Cold Drawn - Reduced Strength (min properties, round bar under 2" dia)AvailabilityAlloy MP35N? is available in Round Bar, Tube, Wire, Sheet and Plate. For all stock availability contact Sales.SpecificationsUNS R30035AMS 5758 - MP35N? VIM-VAR BarSolution heat treated @1900-1925°F for 4 to 8 hoursAMS 5844 - MP35N? VIM-VAR BarSolution heat treated @1900-1925°F for 4 to 8 hours and Work StrengthenedAMS 5845 - MP35N? VIM-VAR BarSolution heat treated @ 1900-1925°F for 4 to 8 hours, Work Strengthened & Aged @ 1000-1200°F for 4 hoursNACE MR0175ASTM F-562 - Surgical Implant ApplicationsBS 7252-6 Surgical Implant ApplicationsISO 5832-6 Surgical Implant ApplicationsQ1: Do you accept the trial order ?A1: Yes,if we have the exactly size in stock.we can delivery even 1 piece/meter .Q2: Can I have free sample before making orders?A2: Yes,we can supply free sample as requirement,but buyer needs to pay the freight charges ,the freight fee will return to buyer after making order.Q3: How do you control the quality ?A3: MTC and PMI will be sent before shipment,any 3rd party inspection if need .Q4: How about your delivery time ?A4: Generally delivery time is 15 working days .Q5: How can I quickly get the price list ?A5: Directly click "chat now" or send us email with detail specifications,you will get the official price list in 1 hour .
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