BS EN 16602-60-14:2020: Space Product Assurance - Relifing Procedure for EEE Components

In the ever-evolving world of space exploration and technology, ensuring the reliability and longevity of electronic, electrical, and electromechanical (EEE) components is paramount. The BS EN 16602-60-14:2020 standard provides a comprehensive framework for the relifing procedure of these critical components, ensuring they meet the rigorous demands of space missions.

Overview of the Standard

The BS EN 16602-60-14:2020 is a crucial document for professionals in the aerospace industry, offering guidelines and procedures to extend the life of EEE components used in space applications. Released on September 24, 2020, this standard is a testament to the ongoing commitment to quality and reliability in space product assurance.

Key Features

• Standard Number: BS EN 16602-60-14:2020
• Pages: 36
• ISBN: 978 0 539 06292 2
• Status: Standard

Importance of Relifing Procedures

Relifing procedures are essential for maintaining the functionality and safety of EEE components in space environments. These procedures help identify potential failures and extend the operational life of components, reducing the risk of mission-critical failures. The BS EN 16602-60-14:2020 standard provides a structured approach to relifing, ensuring that components are thoroughly evaluated and tested before being deemed fit for extended use.

Benefits of Implementing the Standard

By adhering to the guidelines set forth in the BS EN 16602-60-14:2020 standard, organizations can achieve several benefits:

• Enhanced Reliability: Ensure that EEE components meet the highest standards of reliability, reducing the likelihood of failures during critical missions.
• Cost Efficiency: Extend the life of existing components, minimizing the need for costly replacements and reducing overall mission expenses.
• Risk Mitigation: Identify and address potential issues before they become critical, enhancing the safety and success of space missions.
• Compliance: Meet industry standards and regulatory requirements, demonstrating a commitment to quality and safety.

Who Should Use This Standard?

The BS EN 16602-60-14:2020 standard is designed for a wide range of professionals involved in the aerospace industry, including:

• Engineers and Technicians: Responsible for the design, testing, and maintenance of EEE components.
• Quality Assurance Professionals: Ensuring that components meet the necessary standards and specifications.
• Project Managers: Overseeing the implementation of relifing procedures and ensuring compliance with industry standards.
• Regulatory Bodies: Monitoring and enforcing compliance with space product assurance standards.

Conclusion

The BS EN 16602-60-14:2020 standard is an indispensable resource for anyone involved in the design, testing, and maintenance of EEE components for space applications. By providing a clear and structured approach to relifing procedures, this standard helps ensure the reliability, safety, and success of space missions. Embrace the guidelines set forth in this standard to enhance the performance and longevity of your EEE components, and contribute to the advancement of space technology.

BS EN 16602-60-14:2020

This standard BS EN 16602-60-14:2020 Space product assurance. Relifing procedure. EEE components is classified in these ICS categories:

• 49.140 Space systems and operations

This standard specifies the requirements, also known as “relifing requirements”, for the planned, intentional storage, control, and removal from storage of electronic, electrical and electromechanical parts which are intended to be used for space applications.

This standard covers the relifing of all components as defined by ECSS-Q-ST-60 and ECSS-Q-ST-60-13.

The relifing process is a lot quality control activity. The inspections and tests defined do not constitute an up-screening or up-grading of components to a higher level of quality than procured to.

In line with ECSS-Q-ST-60, this standard differentiates between classes of components through different sets of standardization requirements.

The classes provide levels of trade-off between assurance and risk. The highest assurance and lowest risk is provided by Class 1 and the lowest assurance and highest risk by Class 3. Procurement costs are typically highest for Class 1 and lowest for Class 3. Mitigation and other engineering measures can decrease the total cost of ownership differences between the three classes. The project objectives, definition and constraints determine which class or classes of components are appropriate to be utilised within the system and subsystems.

• Class 1 components are described in Clause 4, 5 and 6

• Class 2 components are described in Clause 4, 5 and 6

• Class 3 components are described in Clause 4, 5 and 7

The requirements of this document apply to all parties involved at all levels in the integration of EEE components into space segment hardware and launchers.

This standard is applicable to all EEE parts covered by ECSS-Q-ST-60 and used in space programmes.

This standard is not applicable to dice.

This standard may be tailored for the specific characteristic and constrains of a space project in conformance with ECSS-S-ST-00.