MatWeb - Material Property Data Advertise with MatWeb!     Register Now
Data sheets for over 180,000 metals, plastics, ceramics, and composites.
MatWeb - Material Property Data HOME  •   SEARCH  •   TOOLS  •   SUPPLIERS  •   FOLDERS  •   ABOUT US  •   FAQ  •   LOG IN    
Recently Viewed Materials (most recent at top)  

Login to see your most recently viewed materials here.

Or if you don't have an account with us yet, then click here to register.

  Searches:   Advanced  | Category  | Property  | Metals  | Trade Name  | Manufacturer  | Recently Viewed Materials
  

Extreme Materials from MCAM
Visit Mitsubishi Chemical Advanced Materials for Extreme Materials - high performance plastic machining stock engineered to replace metals such as nickel alloys or stainless steel.

(Viewing data as-entered. Click here to return)
Elmet-Starck MP35N® Nickel/Cobalt/Chromium/Molybdenum Alloy
Categories: Metal; Nonferrous Metal; Cobalt Alloy; Nickel Alloy; Superalloy

Material Notes: MP35N is a nickel-cobalt based alloy of the Multiphase® alloy system that has ultra high strength, toughness, ductility, biocompatibility, and outstanding corrosion resistance. H.C. Starck offers MP35N alloy in flat rolled plate, sheet, and foil products. MP35N is produced by vacuum induction melting and consumable vacuum arc re-melting. Strengthened by work hardening and aging to levels of 260 to 300 ksi (1790 to 2070 MPa), MP35N has good ductility with greater than 40% reduction in area, and good toughness. MP35N can be effectively utilized at cryogenic temperatures without embrittlement and up to 600°F without loss in performance. The high strength and corrosion resistance, high modulus, ease of fabrication, and other mechanical properties make MP35N an ideal candidate for high performance products, where emphasis is placed upon dependability for demanding applications.

MP35N products are used in diverse applications:

  • Biomedical uses: Orthodontics and Prosthetics
  • Oil Industry, Chemical and Marine equipment – Valve components, springs, high pressure door dogs
  • Aircraft and Aerospace components – Springs, leading edge strips
  • High Pulse Magnet Research

Information provided by H.C. Starck.

Vendors: Elmet Technologies is a 100% US owned and operated, fully integrated manufacturer of Molybdenum, Tungsten and related alloys such as TZM, WHA & MoLa. At our 220,000 sqr/ft plant in Lewiston, Maine, Elmet manufactures W & Mo pure powders plus rod, wire, plate, sheet & foil in additional to offering fabrication and machining services. ITAR, ISO and AS9100 registered. www.elmettechnologies.com

Click here to view all available suppliers for this material.

Please click here if you are a supplier and would like information on how to add your listing to this material.

 
Physical PropertiesOriginal ValueComments
Density 8.43 g/cc
 
Mechanical PropertiesOriginal ValueComments
Hardness, Rockwell C 7.0Annealed
 4450% Cold Rolled
 4750% Cold Rolled (4 hrs at 1025°F/550°C)
Hardness, Vickers 220Annealed
 42050% Cold Rolled
 48050% Cold Rolled (4 hrs at 1025°F/550°C)
Tensile Strength, Ultimate 110 ksiAnnealed
 220 ksi50% Cold Rolled
 265 ksi50% Cold Rolled (4 hrs at 1025°F/550°C)
Tensile Strength, Yield 50.0 ksiAnnealed
 200 ksi50% Cold Rolled
 225 ksi50% Cold Rolled (4 hrs at 1025°F/550°C)
Elongation at Break 3.0 %50% Cold Rolled (4 hrs at 1025°F/550°C)
 10 %50% Cold Rolled
 60 %Annealed
Modulus of Elasticity 201 GPa
@Temperature 482 °C
Annealed
 201 GPa
@Temperature 482 °C
Cold Worked
 216 GPa
@Temperature 232 °C
Annealed
 219 GPa
@Temperature 232 °C
Cold Worked
 233 GPa
@Temperature 25.6 °C
Annealed
 235 GPa
@Temperature 25.6 °C
Cold Worked
Poissons Ratio 0.38
@Temperature 232 °C
Calculated; Annealed
 0.40
@Temperature 25.6 °C
Calculated; Annealed
 0.42
@Temperature 482 °C
Calculated; Annealed
 0.45
@Temperature 25.6 °C
Calculated; Cold Worked
 0.46
@Temperature 232 °C
Calculated; Cold Worked
 0.47
@Temperature 482 °C
Calculated; Cold Worked
Shear Modulus 68.0 GPa
@Temperature 482 °C
Cold Worked
 71.0 GPa
@Temperature 482 °C
Annealed
 75.0 GPa
@Temperature 232 °C
Cold Worked
 78.0 GPa
@Temperature 232 °C
Annealed
 81.0 GPa
@Temperature 25.6 °C
Cold Worked
 83.0 GPa
@Temperature 25.6 °C
Annealed
 
Electrical PropertiesOriginal ValueComments
Electrical Resistivity 0.0000990 ohm-cm
@Temperature -184 °C
 0.000101 ohm-cm
@Temperature -73.0 °C
 0.000103 ohm-cm
@Temperature 21.0 °C
 0.000105 ohm-cm
@Temperature 93.0 °C
 0.000108 ohm-cm
@Temperature 204 °C
 0.000110 ohm-cm
@Temperature 316 °C
 0.000113 ohm-cm
@Temperature 427 °C
 0.000115 ohm-cm
@Temperature 538 °C
 0.000118 ohm-cm
@Temperature 649 °C
Magnetic Permeability 1.00085
@Temperature 119 °C
 1.00092
@Temperature 25.0 °C
 1.00096
@Temperature -27.0 °C
 1.00104
@Temperature -73.0 °C
 1.00117
@Temperature -140 °C
 1.00142
@Temperature -195 °C
Magnetic Susceptibility 8.03
@Temperature 119 °C
µ emu/g
 8.7
@Temperature 25.0 °C
µ emu/g
 9.22
@Temperature -27.0 °C
µ emu/g
 9.81
@Temperature -73.0 °C
µ emu/g
 11.07
@Temperature -140 °C
µ emu/g
 13.47
@Temperature -195 °C
µ emu/g
 
Thermal PropertiesOriginal ValueComments
CTE, linear 7.10 µin/in-°F
@Temperature 21.0 - 93.0 °C
 7.60 µin/in-°F
@Temperature 21.0 - 204 °C
 8.20 µin/in-°F
@Temperature 21.0 - 316 °C
 8.30 µin/in-°F
@Temperature 21.0 - 427 °C
 8.70 µin/in-°F
@Temperature 21.0 - 538 °C
Thermal Conductivity 45.0 BTU-in/hr-ft²-°F
@Temperature -184 °C
 63.0 BTU-in/hr-ft²-°F
@Temperature -73.0 °C
 78.0 BTU-in/hr-ft²-°F
@Temperature 21.0 °C
 88.0 BTU-in/hr-ft²-°F
@Temperature 93.0 °C
 104 BTU-in/hr-ft²-°F
@Temperature 204 °C
 118 BTU-in/hr-ft²-°F
@Temperature 316 °C
 133 BTU-in/hr-ft²-°F
@Temperature 427 °C
 148 BTU-in/hr-ft²-°F
@Temperature 538 °C
 162 BTU-in/hr-ft²-°F
@Temperature 649 °C
Melting Point 1315 - 1440 °C
Solidus 1315 °C
Liquidus 1440 °C
 
Component Elements PropertiesOriginal ValueComments
Chromium, Cr 20 %
Cobalt, Co 35 %
Molybdenum, Mo 10 %
Nickel, Ni 35 %

Some of the values displayed above may have been converted from their original units and/or rounded in order to display the information in a consistent format. Users requiring more precise data for scientific or engineering calculations can click on the property value to see the original value as well as raw conversions to equivalent units. We advise that you only use the original value or one of its raw conversions in your calculations to minimize rounding error. We also ask that you refer to MatWeb's terms of use regarding this information. Click here to go back to viewing the property data in MatWeb's normal format.

Users viewing this material also viewed the following:
Titanium Ti-6Al-4V (Grade 5), Annealed
Special Metals INCONEL® Alloy 718
Special Metals INCONEL® 706 Precipitation Hardening Alloy, Hot Finished Rod, 3 Part Heat Treatment, 8.0 inch (203 mm) Diameter
Latrobe MP35N® Alloy
Carpenter MP35N* Ni-Co-Cr-Mo Alloy, Cold Drawn 53%, Aged 565°C/4hr/AC

NHCST972 / 146233

Rulon Bearings

Please read our License Agreement regarding materials data and our Privacy Policy. Questions or comments about MatWeb? Please contact us at webmaster@matweb.com. We appreciate your input.

The contents of this web site, the MatWeb logo, and "MatWeb" are Copyright 1996-2024 by MatWeb, LLC. MatWeb is intended for personal, non-commercial use. The contents, results, and technical data from this site may not be reproduced either electronically, photographically or substantively without permission from MatWeb, LLC.