
15-5PH Stainless Steel Sheet
High-strength precipitation-hardening stainless steel sheet for aerospace and industrial applications
15-5PH stainless steel sheet delivers excellent strength-to-weight ratio with superior corrosion resistance and formability. Ideal for aircraft structures, engine components, and applications requiring both mechanical performance and environmental durability.
Quick Specifications
- UNS Designation
- S15500
- Werkstoff Number
- 1.4545
- Yield Strength (H1025)
- 1,310 MPa (190 ksi) minimum
- Tensile Strength (H1025)
- 1,450 MPa (210 ksi) minimum
- Elongation (H1025)
- 10% minimum
- Density
- 7.81 g/cm³
Standards & Certifications
Product Description
15-5PH is a martensitic precipitation-hardening stainless steel engineered for applications demanding high strength combined with good corrosion resistance and reasonable formability. The 15% chromium and 5% nickel composition provides an excellent balance of mechanical properties and environmental resistance. This grade is specifically developed to offer better formability than PH13-8Mo while maintaining comparable strength levels after heat treatment.
The material's metallurgical design allows for cold forming in the annealed condition before final hardening, providing significant manufacturing flexibility for complex shapes. The precipitation mechanism involves fine dispersal of intermetallic compounds that develop during the 480°C aging treatment, creating a uniform strengthening effect throughout the microstructure. This controlled precipitation hardening results in superior fatigue strength and fatigue crack propagation resistance compared to martensitic stainless steels hardened by carbon content alone.
15-5PH sheet exhibits excellent corrosion resistance in atmospheric, neutral, and mildly corrosive industrial environments. The material resists pitting corrosion in chloride solutions better than conventional stainless steels and demonstrates exceptional resistance to stress corrosion cracking. Its low carbon content minimizes carbide formation and intergranular corrosion susceptibility, particularly important in applications involving welding or thermal cycling.
Manufacturing of 15-5PH sheet employs vacuum induction melting followed by controlled rolling and annealing to develop a fine, uniform grain structure. This approach ensures consistent mechanical properties across the thickness and excellent ductility in the as-annealed condition. The material responds predictably to standard forming operations, making it suitable for sheet metalworking applications including stamping, deep drawing, and press forming.
Specifications
| UNS Designation | S15500 |
| Werkstoff Number | 1.4545 |
| Yield Strength (H1025) | 1,310 MPa (190 ksi) minimum |
| Tensile Strength (H1025) | 1,450 MPa (210 ksi) minimum |
| Elongation (H1025) | 10% minimum |
| Density | 7.81 g/cm³ |
| Yield Strength (Annealed) | 480 MPa (70 ksi) |
| Elongation (Annealed) | 25% minimum |
| Modulus of Elasticity | 205 GPa |
| Thermal Conductivity | 9.8 W/m·K at 20°C |
| Coefficient of Linear Expansion | 10.8 × 10⁻⁶ /°C (0-100°C) |
| Hardness Range (H1025) | 40-46 HRC |
Chemical Composition
| Element | Content (%) |
|---|---|
| Chromium (Cr) | 14.0-15.5 |
| Nickel (Ni) | 3.5-5.5 |
| Molybdenum (Mo) | 2.5-4.5 |
| Niobium (Nb) | 0.15-0.45 |
| Aluminum (Al) | 1.0-1.5 |
| Carbon (C) | 0.03 max |
| Manganese (Mn) | 0.10 max |
| Silicon (Si) | 0.10 max |
| Phosphorus (P) | 0.010 max |
| Sulfur (S) | 0.008 max |
Mechanical Properties
| Property | Value |
|---|---|
| Tensile Strength (Annealed) | 860 MPa |
| Reduction of Area (Annealed) | 50% minimum |
| Charpy Impact (V-notch, Annealed) | 70 J at room temperature |
| Charpy Impact (V-notch, H1025) | 50-70 J at room temperature |
| Fatigue Strength (H1025) | 520 MPa at 10⁷ cycles |
| Fracture Toughness (K₁c, H1025) | 60-70 MPa√m |
Key Features & Advantages
Applications
Aerospace Structures
Aircraft fuselage panels, wing skins, stringers, and structural elements where high strength, excellent fatigue performance, and superior corrosion resistance are critical for extended service life.
Engine Components
Combustor liners, shrouds, and casing elements in jet engines requiring high temperature corrosion resistance and mechanical reliability in demanding thermal cycling environments.
Industrial Valve Components
Valve bodies, bonnets, and internal components in high-pressure industrial valves for petrochemical and hydrocarbon processing applications requiring superior strength and sealing integrity.
Pressure Vessels
High-pressure vessel construction, heat exchanger components, and reactor vessels in chemical processing and oil and gas applications requiring both mechanical strength and corrosion resistance.
Marine Applications
Naval components, submarine structures, and offshore equipment exposed to seawater with requirements for high strength, excellent corrosion resistance, and exceptional toughness.
Electronic and Automotive
High-performance automotive components, electronic shielding, and structural reinforcement where weight savings and superior corrosion performance are essential.
Frequently Asked Questions
Can 15-5PH sheet be easily formed before hardening?
What is the recommended aging temperature and time?
How does 15-5PH compare to Inconel or superalloys?
Is 15-5PH suitable for welded structures?
What is the expected service life in seawater applications?
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