BS A 359:2000, ISO 12278:1999
Explore BS A 359:2000, ISO 12278:1999. Essential standards for aerospace engineering to ensure compliance and performance excellence.
BS A 359:2000, ISO 12278:1999 - Overview
The British Standard BS A 359:2000, which aligns with the international standard ISO 12278:1999, provides critical guidance for professionals in the field of aircraft and space vehicle engineering. This standard was established on March 15, 2000, and serves as a key reference for the design, testing, and performance evaluation of aerospace materials and components.
Importance of BS A 359:2000
As the aerospace industry evolves with increasing demands for safety, efficiency, and innovation, BS A 359:2000 acts as a comprehensive framework that ensures compliance with international best practices. This standard is particularly relevant for aerospace engineers, manufacturers, and quality control professionals committed to maintaining the highest standards of performance and reliability in their products.
Key Specifications
- ISBN: 0 580 34422 3
- Price: £134.00
- File Format: Available in both PDF and hardcopy formats
- Standard Type: Identical to ISO 12278:1999
Applications
BS A 359:2000 is applicable across various sectors within the aerospace industry, including but not limited to:
- Aircraft manufacturing
- Spacecraft development
- Quality assurance processes
- Performance testing of materials and components
Who Should Use This Standard?
This standard is essential for:
- Aerospace engineers designing new aircraft and spacecraft
- Manufacturers ensuring that their processes adhere to international standards
- Quality assurance auditors aiming to evaluate compliance with industry norms
- Research and development teams focused on innovation and material testing
Conclusion
By investing in the BS A 359:2000, professionals in the aerospace sector can enhance their compliance with safety regulations and best practices, fostering technological advancement and operational excellence within their organizations. The standard serves not just as a guideline but as a fundamental component of the aerospace engineering landscape, ensuring that products not only meet but exceed established benchmarks for performance and reliability.
For purchase or more information, please refer to the standard's official publication details and acquire your copy in PDF or hardcopy format today.
Technical Information
Specification Details
- Nuts, barrel, self-locking, floating, with MJ threads, classifications
- 900 MPa (at ambient temperature)/235°C, 1100 MPa (at ambient temperature)/235°C, 1250 MPa (at ambient temperature)/235°C, 1550 MPa (at ambient temperature)/235°C
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