Metals & alloys · Nickel & cobalt alloys

René 41-type nickel superalloy

A high-strength γ′-hardened nickel superalloy used in turbine and rocket components requiring high-temperature strength and oxidation resistance.

Family
Wrought Nickel Superalloy
Record
Standard
Conditions
1
Sources
4
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01

Overview

Material class
Metals & alloys
Category
Nickel & cobalt alloys
Family
Wrought Nickel Superalloy
Product forms
Sheet/plate, Bar/rod

Composition

ConstituentMinMaxTypicalNote
Ni5054
Cr182019
Co101211
Mo910.59.8
Ti33.33.1
Al1.41.81.6

02

Properties and conditions

Engineering properties

PropertyValueUnitCondition
Density8.25g/cm³Representative; verify product form and condition
Elastic modulus~220GPaRepresentative; verify product form and condition
Yield strength~900–1200MPaaged
Tensile strength~1200–1500MPaRepresentative; verify product form and condition
Service temperatureup to ~870°Cshort/medium duration
Fabricabilitydemandingprocess controlled

Conditions

reference

Representative supplied condition

Condition not fully specified in the source record.

03

Processing and use

Processing

  • Product form, thermal history and manufacturing route materially affect performance.

Applications

  • Rocket engine components
  • Turbine rings
  • Afterburner hardware

Selection considerations

  • Use the current governing standard and supplier certification for design or procurement.

04

Standards and related materials

Standards and designations

SystemDesignationNote
UNSN07041
AMS5545 / 5712product dependent

05

Sources and context

Sources

Confirm the applicable specification, product form and condition before using values for design or procurement.

Supply and sustainability

Availability and lead time depend on grade, product form, certification and regional supply chain.

Segregated recovery and closed-loop recycling improve material efficiency where practical.