BS EN 16603-20-01:2020 Space Engineering: Multipactor, Design and Test

Welcome to the world of advanced space engineering with the BS EN 16603-20-01:2020 standard. This comprehensive document is an essential resource for professionals in the aerospace industry, providing detailed guidelines and methodologies for addressing the phenomenon of multipactor effects in space engineering. Released on October 6, 2020, this standard is a cornerstone for ensuring the reliability and safety of space systems.

Overview

The BS EN 16603-20-01:2020 standard is a meticulously crafted document that spans 78 pages, offering in-depth insights into the design and testing processes necessary to mitigate multipactor effects. Multipactor is a critical concern in the design of space systems, as it can lead to significant performance degradation or even failure of electronic components in the harsh environment of space.

Key Features

• Standard Number: BS EN 16603-20-01:2020
• Pages: 78
• Release Date: October 6, 2020
• ISBN: 978 0 580 86644 9
• Status: Standard

Why This Standard is Essential

In the realm of space engineering, the multipactor effect is a phenomenon that can severely impact the performance of RF components. This effect occurs when electrons in a vacuum are accelerated by an RF field, leading to a cascade of secondary electron emissions. If not properly managed, this can result in power loss, signal distortion, and even catastrophic failure of spaceborne systems.

The BS EN 16603-20-01:2020 standard provides a robust framework for understanding and mitigating these effects. It outlines the theoretical foundations of multipactor phenomena, offers design strategies to prevent its occurrence, and details testing procedures to ensure compliance and reliability of space systems.

Comprehensive Design and Testing Guidelines

This standard is not just a theoretical document; it is a practical guide that equips engineers with the tools they need to design and test components that are resistant to multipactor effects. It includes:

• Theoretical Analysis: Detailed explanations of the physics behind multipactor effects, helping engineers understand the root causes and potential solutions.
• Design Strategies: Practical guidelines for designing components and systems that minimize the risk of multipactor effects, including material selection, geometric considerations, and RF power management.
• Testing Procedures: Step-by-step instructions for conducting tests to verify the multipactor resistance of components, ensuring that they meet the rigorous demands of space applications.

Who Should Use This Standard?

The BS EN 16603-20-01:2020 standard is an invaluable resource for a wide range of professionals in the aerospace industry, including:

• Design Engineers: Those involved in the creation of RF components and systems for space applications will find this standard essential for ensuring their designs are robust and reliable.
• Test Engineers: Professionals responsible for verifying the performance and safety of space systems will benefit from the detailed testing methodologies outlined in this document.
• Project Managers: Those overseeing space engineering projects can use this standard to ensure that their teams are adhering to best practices and industry standards.
• Quality Assurance Specialists: Individuals tasked with maintaining the quality and reliability of aerospace components will find this standard a critical tool in their arsenal.

Conclusion

The BS EN 16603-20-01:2020 standard is a vital document for anyone involved in the design, testing, and management of space systems. By providing a comprehensive framework for understanding and mitigating multipactor effects, this standard helps ensure the reliability and safety of spaceborne components. Whether you are an engineer, a project manager, or a quality assurance specialist, this standard is an indispensable resource that will enhance your ability to deliver high-quality, reliable space systems.

Embrace the future of space engineering with the BS EN 16603-20-01:2020 standard, and ensure your projects are built on a foundation of excellence and innovation.

BS EN 16603-20-01:2020

This standard BS EN 16603-20-01:2020 Space engineering. Multipactor, design and test is classified in these ICS categories:

• 49.140 Space systems and operations

This standard defines the requirements and recommendations for the design and test of RF components and equipment to achieve acceptable performance with respect to multipactor-free operation in service in space. The standard includes:

• verification planning requirements,

• definition of a route to conform to the requirements,

• design and test margin requirements,

• design and test requirements, and

• informative annexes that provide guidelines on the design and test processes.

This standard is intended to result in the effective design and verification of the multipactor performance of the equipment and consequently in a high confidence in achieving successful product operation.

This standard covers multipactor events occurring in all classes of RF satellite components and equipment at all frequency bands of interest in high vacuum conditions (pressure lower than 10-5 hPa). Operation in single carrier CW and pulse modulated mode are included, as well as unmodulated multi-carrier operations. A detailed clause on secondary emission yield is also included.

This standard does not include breakdown processes caused by collisional processes, such as plasma formation.

This standard is applicable to all space missions.

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