Waspaloy Solution, stabilization, and precipitation heat treated
VerifiedmetalWaspaloy is a nickel-based superalloy containing cobalt, chromium, molybdenum, and tungsten alloying elements, designed for high-temperature structural applications in gas turbine engines and other demanding aerospace environments. The solution, stabilization, and precipitation heat-treated condition provides optimized strength and creep resistance through controlled gamma-prime precipitation, with tensile properties (yield strength, ultimate tensile strength, elongation, and reduction of area) suitable for elevated-temperature service up to approximately 1200°F (650°C).
turbine discgas turbineaerospaceforged superalloy
Compliance & Regulations
?ITAR?EAR?Conflict Free?RoHS?REACH?TSCA?Prop 65
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| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Elongation at Break(εf)4 entries | — | - | 22°C · Forging · Solution, stabilization, and precipitation heat treated · AMS 5704 · L · t=≤3.500 in | — | |
| ↳ | — | - | 22°C · Bar/Forging · Solution, stabilization, and precipitation heat treated · AMS 5706 OR AMS 5707 · L · t=≤3.500 in | — | |
| ↳ | — | - | 22°C · Sheet/Strip/Plate · Solution, stabilization, and precipitation heat treated · AMS 5544 · LT · t=≤0.020 in | — | |
| ↳ | — | - | 22°C · Sheet/Strip/Plate · Solution, stabilization, and precipitation heat treated · AMS 5544 · LT · t=>0.020 in | — | |
Ramberg–Osgood Exponent vs Temperature(n(T)) | Curve (10 pts) | - | — | — | |
Reduction of Area(RA)2 entries | — | - | 22°C · Forging · Solution, stabilization, and precipitation heat treated · AMS 5704 · L · t=≤3.500 in | — | |
| ↳ | — | - | 22°C · Bar/Forging · Solution, stabilization, and precipitation heat treated · AMS 5706 OR AMS 5707 · L · t=≤3.500 in | — | |
Reduction of Area vs Temperature(RA(T)) | Curve (10 pts) | - | L | — | |
Stress–Strain Curve(σ–ε) | Curve (12 pts) | ksi | 538°C · L | — | |
Ultimate Tensile Strength(σUTS) | — | ksi | 5 entriesClick to expand | ||
Yield Strength (0.2% offset)(σy) | — | ksi | 5 entriesClick to expand | ||
Young's Modulus(E) | Curve (6 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 (8 pts) | µin/in·°F | — | — | |
Specific Heat vs Temperature(Cp(T)) | Curve (10 pts) | BTU/(lb·°F) | — | — | |
Thermal Conductivity vs Temperature(k(T)) | Curve (7 pts) | BTU/(hr·ft·°F) | — | — |
Verified Unverified Low confidence (<80%) Link to source
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | — | lb/in³ | — | — |
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
Regulatory Screening
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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.