BS EN 3532:2025
Aerospace series. Steel X2NiCoMo18-8-5 (1.6359). Vacuum induction melted and vacuum arc remelted. Solution treated and precipitation treated. Plates. 6 mm < a ≤ 40 mm. 1 750 MPa ≤ Rm ≤ 2 000 MPa
| Standard number: | BS EN 3532:2025 |
| Pages: | 12 |
| Released: | 2025-09-17 |
| ISBN: | 978 0 539 32127 2 |
| Status: | Standard |
BS EN 3532:2025 Aerospace Series Steel X2NiCoMo18-8-5 (1.6359)
Introducing the BS EN 3532:2025, a cutting-edge standard in the aerospace industry, designed to meet the rigorous demands of modern engineering. This standard specifies the properties and requirements for Steel X2NiCoMo18-8-5 (1.6359), a high-performance material that is vacuum induction melted and vacuum arc remelted, ensuring superior quality and consistency.
Key Features
- Material: Steel X2NiCoMo18-8-5 (1.6359)
- Manufacturing Process: Vacuum induction melted and vacuum arc remelted
- Treatment: Solution treated and precipitation treated
- Plate Thickness: 6 mm < a ≤ 40 mm
- Tensile Strength: 1 750 MPa ≤ Rm ≤ 2 000 MPa
Unmatched Performance for Aerospace Applications
The BS EN 3532:2025 standard is meticulously crafted to cater to the aerospace industry's stringent requirements. The steel specified in this standard is known for its exceptional strength and durability, making it an ideal choice for critical aerospace components. With a tensile strength ranging from 1 750 MPa to 2 000 MPa, this material ensures reliability and performance in the most demanding environments.
Advanced Manufacturing Techniques
The steel is produced using advanced vacuum induction melting and vacuum arc remelting processes. These techniques are employed to achieve a high level of purity and homogeneity in the material, which is crucial for maintaining consistent mechanical properties. The solution treatment and precipitation treatment further enhance the material's strength and resistance to wear and tear, ensuring longevity and dependability.
Comprehensive Standard Documentation
The BS EN 3532:2025 standard is a comprehensive document spanning 12 pages, providing detailed specifications and guidelines for the use of Steel X2NiCoMo18-8-5 (1.6359) in aerospace applications. Released on September 17, 2025, this standard is the latest in the series, reflecting the most current advancements and best practices in the industry.
Technical Specifications
| Standard Number | BS EN 3532:2025 |
|---|---|
| Pages | 12 |
| Release Date | 2025-09-17 |
| ISBN | 978 0 539 32127 2 |
| Status | Standard |
Why Choose BS EN 3532:2025?
Choosing the BS EN 3532:2025 standard means opting for a material that is engineered for excellence. Its high tensile strength and robust manufacturing process make it a preferred choice for aerospace engineers and manufacturers who demand the best. Whether you are designing aircraft components or other high-stress applications, this standard provides the assurance of quality and performance.
Applications
The versatility of Steel X2NiCoMo18-8-5 (1.6359) makes it suitable for a wide range of aerospace applications, including:
- Aircraft structural components
- Engine parts
- Landing gear systems
- High-stress fasteners
Conclusion
In the ever-evolving aerospace industry, the BS EN 3532:2025 standard stands out as a benchmark for quality and reliability. Its comprehensive guidelines and specifications ensure that manufacturers and engineers have access to a material that meets the highest standards of performance. Embrace the future of aerospace engineering with Steel X2NiCoMo18-8-5 (1.6359) and the BS EN 3532:2025 standard.
BS EN 3532:2025
This standard BS EN 3532:2025 Aerospace series. Steel X2NiCoMo18-8-5 (1.6359). Vacuum induction melted and vacuum arc remelted. Solution treated and precipitation treated. Plates. 6 mm < a ≤ 40 mm. 1 750 MPa ≤ Rm ≤ 2 000 MPa is classified in these ICS categories:
- 49.025.10 Steels