MP35N Solution Treated

Verifiedmetal

MP35N 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

MP35N/MP35N Solution Treated

Units:

si imperial

Property OverviewNormalized to typical max values

1 interactive curve for this material

Stress-strain, S-N fatigue and environmental knockdown curves are free with an account.

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Thickness

Property	Value	Unit	Conditions
Elongation at Break(εf)2 entries	8.000	-	22°C · Bar · Solution treated and cold drawn · AMS 5844 · L · t=≤1.000 in
↳	8.000	-	22°C · Bar · Solution treated and cold drawn · AMS 5844 · L · t=1.001-1.750 in
Reduction of Area(RA)2 entries	35.00	-	22°C · Bar · Solution treated and cold drawn · AMS 5844 · L · t=≤1.000 in
↳	35.00	-	22°C · Bar · Solution treated and cold drawn · AMS 5844 · L · t=1.001-1.750 in
Shear Modulus(G)	80.67	GPa	22°C · Bar
Ultimate Shear Strength(Fsu)	999.7	MPa	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)	Pa	21°C · L
Ultimate Tensile Strength(σUTS)2 entries	1.793	GPa	22°C · Bar · Solution treated and cold drawn · AMS 5844 · L · t=≤1.000 in
↳	1.793	GPa	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	1.586	GPa	22°C · Bar · Solution treated and cold drawn · AMS 5844 · L · t=≤1.000 in
↳	1.586	GPa	22°C · Bar · Solution treated and cold drawn · AMS 5844 · L · t=1.001-1.750 in
Young's Modulus(E)	234.4	GPa	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, or test environment.

Rows with are inherited from the base material

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2 interactive curves for this material

Stress-strain, S-N fatigue and environmental knockdown curves are free with an account.

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Property	Value	Unit	Conditions	Source
CTE vs Temperature(α(T))	Curve (17 pts)	1/K	—
Thermal Conductivity vs Temperature(k(T))	Curve (17 pts)	W/(m·K)	—

Rows with are inherited from the base material

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Property	Value	Unit	Conditions	Source
Density(ρ)	8.415	kg/m³	22°C

Rows with are inherited from the base material

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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.

MP35N Solution Treated

Mechanical Properties

Thermal Properties

Physical Properties

Regulatory Screening

Environmental

Export Control