René 41 STA
VerifiedmetalRené 41 STA is a nickel-base superalloy (Ni-Co-Cr-Mo-W-Al-Ti) in solution heat-treated and aged condition, designed for high-temperature structural applications in jet engines and gas turbines operating up to 1100°F (593°C). The STA condition provides optimized strength and creep resistance through controlled grain structure and precipitation hardening, with excellent bearing strength and fatigue performance in bar, forging, plate, and sheet forms.
aerospacestructural
Compliance & Regulations
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Specification
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Ultimate Bearing Strength(Fbru) | — | ksi | 7 entriesClick to expand | ||
Bearing Yield Strength(Fbry) | — | ksi | 7 entriesClick to expand | ||
Compressive Modulus(Ec) | — | ksi | 22°C · Sheet | — | |
Compressive Yield Strength(Fcy) | — | ksi | 6 entriesClick to expand | ||
Elongation at Break(εf)4 entries | — | - | 22°C · Bar/Forging · Solution treated and aged (1400°F) · AMS 5712 OR AMS 5713 · L · t=≤1.000 in | — | |
| ↳ | — | - | 22°C · Sheet · Solution treated and aged (1400°F) · AMS 5545 · LT · t=≤0.020 in | — | |
| ↳ | — | - | 22°C · Sheet · Solution treated and aged (1400°F) · AMS 5545 · LT · t=0.021-0.187 in | — | |
| ↳ | — | - | 22°C · Plate · Solution treated and aged (1400°F) · AMS 5545 · LT · t=0.188-0.375 in | — | |
Poisson's Ratio(ν) | — | - | 22°C | — | |
Reduction of Area(RA) | — | - | 22°C · Bar/Forging · Solution treated and aged (1400°F) · AMS 5712 OR AMS 5713 · L · t=≤1.000 in | — | |
Shear Modulus(G) | — | ksi | 22°C · Sheet | — | |
Ultimate Shear Strength(Fsu) | — | ksi | 5 entriesClick to expand | ||
Ultimate Tensile Strength(σUTS) | — | ksi | 8 entriesClick to expand | ||
Yield Strength (0.2% offset)(σy) | — | ksi | 8 entriesClick to expand | ||
Young's Modulus(E) | Curve (10 pts) | ksi | L | — | |
N entriesMultiple entries per property — large groups are collapsed; click a summary row to expand. Use filters above to narrow by form / heat treatment / basis.
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
CTE vs Temperature(α(T)) | Curve (6 pts) | µin/in·°F | — | — | |
Specific Heat vs Temperature(Cp(T)) | Curve (17 pts) | BTU/(lb·°F) | — | — | |
Thermal Conductivity vs Temperature(k(T)) | Curve (17 pts) | BTU/(hr·ft·°F) | — | — |
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | — | lb/in³ | 22°C | — |
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
Regulatory Screening
Environmental
Export Control
RoHS, REACH, and Prop 65 statuses are validated against official substance lists (ECHA SVHC Candidate List, OEHHA Prop 65, RoHS Annex II). Other regulations are estimated from composition and material classification. All screening is a starting point for due diligence — always verify with your supplier before making compliance decisions.