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Nickel-Iron-Chromium AlloysUNS N09901View material details

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Compare Materials: Nimonic 901
MaterialNimonic 901N09901

Summary

Material familyNickel-Iron-Chromium Alloys
Grade / UNSN09901
SummaryAn age-hardenable nickel-iron-chromium alloy used for gas-turbine discs, shafts and rings.

Performance overview

Material focusAge-hardenable Ni-Fe-Cr
Physical reference
Density
8.14 g/cm³
Dynamic Young’s modulus
201 GPa
Specific heat
431 J/(kg·K)
Special Metals · Alloy 901 · SMC-076 · Tables 1, 2, 4; forged-bar curve in Figure 1 ↗
Chemical composition
Chemical composition

Selected nominal composition · wt.%

Ni
42.5
Cr
12.5
Mo
5.75
Ti
2.9
Al
≤0.35
Fe
Balance
Special Metals · Alloy 901 · SMC-076 · Tables 1, 2, 4; forged-bar curve in Figure 1 ↗

Mechanical properties

Reference conditions vary or are incomplete. Read the basis, condition and source for each column; these values do not establish a performance ranking or finished-fastener acceptance values.

Tensile strengthNot documented in this reference
0.2% yield strengthNot documented in this reference
ElongationNot documented in this reference
Reference conditions
Data basis
Published physical reference
Condition
Fully heat treated (modulus sample)
Sample form
Not documented in this reference
Sample size
Not documented in this reference
Test temperature
20°C for modulus and specific heat
Test method
Not documented in this reference
Test direction
Not documented in this reference
Elongation gauge length
Not documented in this reference

Temperature & corrosion

Evaluate the medium, concentration, impurities, temperature and loading together. A melting point or oxidation reference is not a safe working-temperature limit.

Service conditions to reviewState product form, heat treatment and the required strength.
Temperature-dependent data
  • Strength and ductility vs temperatureVacuum-refined, extruded and forged bar
View material details

Heat treatment

Delivery condition and heat-treatment requirements are agreed for the requested product form and order.

ConditionFully heat treated (modulus sample)
Reference treatmentForged-bar recommendation in source: 1090°C / 3 h, water quench; 775°C / 4 h, air cool; 705–720°C / 24 h, air cool. This is not a BYBOLT process instruction.Special Metals · Alloy 901 · SMC-076 · Tables 1, 2, 4; forged-bar curve in Figure 1 ↗

Reference applications

Application examples provide context for review; suitability depends on the actual service conditions.

Reference applicationsGas-turbine shafts, discs & rings

Standards & documentation

Confirm the edition, product form and condition. Material specifications do not establish finished-fastener compliance.

Material specifications by form
Sources
Sources

Documents for your enquiry

Every BYBOLT delivery includes an MTC / EN 10204 3.1 certificate, heat-number traceability and mechanical testing. Threaded products include sampled GO / NO-GO gauging. Test methods and acceptance criteria follow the agreed specification; PMI, third-party inspection and additional records are agreed separately at quotation.

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