MP35N is a cobalt-nickel-chromium-molybdenum superalloy designed for high-strength, corrosion-resistant applications requiring excellent fatigue resistance and performance in cryogenic to moderate elevated temperatures. Primarily used in aerospace fasteners, springs, and medical implants, MP35N offers yield strengths exceeding 1,000 MPa with superior resistance to stress-corrosion cracking and seawater corrosion compared to conventional stainless steels.
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8 interactive curves for this material
Stress-strain, S-N fatigue and environmental knockdown curves are free with an account.
Create free account| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Elongation at Break(εf) | Curve (8 pts) | - | L | ||
Shear Modulus(G)2 entries | 80.67 | GPa | 22°C · Bar | ||
| ↳ | Curve (25 pts) | Pa | — | ||
Stress–Strain Curve (buckling region, ≤ 2% strain)(σ–ε (low-strain))3 entries | Curve (10 pts) | Pa | 21°C · L | ||
| ↳ | Curve (12 pts) | Pa | 204°C · L | ||
| ↳ | Curve (11 pts) | Pa | 371°C · L | ||
Ultimate Tensile Strength(σUTS) | Curve (8 pts) | Pa | L | ||
Yield Strength (0.2% offset)(σy) | Curve (8 pts) | Pa | L | ||
Young's Modulus(E)2 entries | 234.4 | GPa | 22°C · Bar | ||
| ↳ | Curve (5 pts) | Pa | L |
2 interactive curves for this material
Stress-strain, S-N fatigue and environmental knockdown curves are free with an account.
Create free account| 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) | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 8.415 | kg/m³ | 22°C |