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MP35N Rod Ultra High Strength Nickel Cobalt Alloy For Aerospace Medical

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MP35N Rod Ultra High Strength Nickel Cobalt Alloy For Aerospace Medical

Name: MP35N Rod Ultra High Strength Nickel Cobalt Alloy For Aerospace Medical
Brand: NikTech
Price: 1 USD

Brand Name : NikTech

Model Number : UMCO50

Certification : ISO 9001:2008

Place of Origin : China

MOQ : 150kgs

Price : Negotiatable

Payment Terms : ,L/C,T/T,Western Union,MoneyGram

Supply Ability : 300 Ton per Month

Delivery Time : 2-30days

Packaging Details : Wood box for Rod

Wear Resistance : High

Material Type : Alloy

Density : 8.43 g/cm3

Magnetic Properties : Non-magnetic

Elongation : 10-52%

Corrosion Resistance : Excellent

Melting Point : 1440℃

Tensile Strength : 1100MPa

Hardness : HRC 32-50

Composition : Cobalt, Chromium, Chromium，Moly

Applications : Aerospace, Gas Turbines, Chemical Processing, Medical Devices

Common Trade Names 1 : W.Nr. 2.4999

Common Trade Names 2 : UNS R30035

Common Trade Names 3 : AWS 110

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MP35N Rod: Ultra-High Strength Nickel-Cobalt Alloy for Aerospace and Medical Applications

Product Overview

MP35N (UNS R30035) is a non-magnetic, age-hardenable nickel-cobalt-chromium-molybdenum alloy renowned for its exceptional combination of ultra-high strength, toughness, ductility, and outstanding corrosion resistance. This multiphase alloy is engineered to perform in the most demanding environments, making it ideal for applications in aerospace, medical devices, oil and gas, marine, and chemical processing industries.

Chemical Composition

Element	Ni (%)	Co (%)	Cr (%)	Mo (%)	Fe (%)	Mn (%)	Si (%)	P (%)	S (%)	C (%)
Min	33.0	Balance	19.0	9.0	–	–	–	–	–	–
Max	37.0	–	21.0	10.5	1.0	0.15	0.15	0.015	0.01	0.025

Mechanical Properties

Condition	Tensile Strength (ksi)	Yield Strength (ksi)	Elongation (%)	Hardness (HRC)
AMS 5844	255	225	12	45
AMS 5845	260	230	8	≥38
NACE MR0175	220	210	10	≤51

Physical Properties

Property	Value
Density	8.43 g/cm³
Melting Point	1440°C
Modulus of Elasticity	234 GPa
Thermal Conductivity	11.2 W/m·K
Coefficient of Expansion	12.8 µm/m·°C
Electrical Resistivity	1.67% IACS

Standards and Specifications

Standard	Description
AMS 5844	Solution Heat Treated and Work Strengthened
AMS 5845	Solution Heat Treated, Work Strengthened, and Aged
ASTM F562	Wrought 35% Cobalt-35% Nickel-20% Chromium-10% Molybdenum Alloy for Surgical Implant Applications
NACE MR0175	Materials for Use in H2S-Containing Environments in Oil and Gas Production

Applications

MP35N rods are utilized in various industries due to their superior properties:

Aerospace: Components such as fasteners and structural parts requiring high strength and resistance to fatigue.
Medical Devices: Implants, surgical instruments, and orthodontic devices benefiting from biocompatibility and corrosion resistance.
Oil and Gas: Downhole tools, valve stems, and springs exposed to harsh environments.
Marine: Subsea components and fasteners resistant to seawater corrosion.
Chemical Processing: Equipment parts exposed to aggressive chemicals and high temperatures.

FAQs

Q1: What is the maximum operating temperature for MP35N rods?

A1: MP35N rods can operate effectively up to temperatures of 800°F (427°C) in moderately elevated environments.

Q2: Can MP35N rods be welded?

A2: Yes, MP35N rods can be welded using standard welding techniques. However, post-weld heat treatment may be required to restore mechanical properties.

Q3: How does MP35N compare to other high-strength alloys?

A3: MP35N offers superior corrosion resistance and higher tensile strength compared to many other high-strength alloys, ensuring better performance in extreme conditions.

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