MP35N Solution Treated
VerifiedmetalMP35N is a cobalt-nickel-chromium-molybdenum superalloy solution treated to a fully annealed condition, providing excellent corrosion and fatigue resistance for aerospace applications requiring high strength retention at elevated temperatures. Solution-treated MP35N offers optimal ductility and toughness with moderate strength levels, making it suitable for critical rotating components and fasteners in jet engines and gas turbines operating up to approximately 650°C.
aerospacestructural
Compliance & Regulations
?EAR?Conflict Free?RoHS?REACH?TSCA?Prop 65
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Thickness
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Elongation at Break(εf)2 entries | — | - | 22°C · Bar · Solution treated and cold drawn · AMS 5844 · L · t=≤1.000 in | — | |
| ↳ | — | - | 22°C · Bar · Solution treated and cold drawn · AMS 5844 · L · t=1.001-1.750 in | — | |
Reduction of Area(RA)2 entries | — | - | 22°C · Bar · Solution treated and cold drawn · AMS 5844 · L · t=≤1.000 in | — | |
| ↳ | — | - | 22°C · Bar · Solution treated and cold drawn · AMS 5844 · L · t=1.001-1.750 in | — | |
Shear Modulus(G) | — | ksi | 22°C · Bar | — | |
Ultimate Shear Strength(Fsu) | — | ksi | 22°C · Bar · Solution treated and cold drawn · AMS 5844 · t=≤1.000 in | — | |
Stress–Strain Curve (buckling region, ≤ 2% strain)(σ–ε (low-strain)) | Curve (10 pts) | ksi | 21°C · L | — | |
Ultimate Tensile Strength(σUTS)2 entries | — | ksi | 22°C · Bar · Solution treated and cold drawn · AMS 5844 · L · t=≤1.000 in | — | |
| ↳ | — | ksi | 22°C · Bar · Solution treated and cold drawn · AMS 5844 · L · t=1.001-1.750 in | — | |
Yield Strength (0.2% offset)(σy)2 entries | — | ksi | 22°C · Bar · Solution treated and cold drawn · AMS 5844 · L · t=≤1.000 in | — | |
| ↳ | — | ksi | 22°C · Bar · Solution treated and cold drawn · AMS 5844 · L · t=1.001-1.750 in | — | |
Young's Modulus(E) | — | ksi | 22°C · Bar | — |
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 (17 pts) | µin/in·°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.