BS EN 16603-60-20:2020 - Space Engineering: Star Sensor Terminology and Performance Specification

Welcome to the world of advanced space engineering with the BS EN 16603-60-20:2020 standard. This comprehensive document is an essential resource for professionals and organizations involved in the design, development, and deployment of star sensors in space missions. Released on August 28, 2020, this standard is a cornerstone in the field of space engineering, providing detailed terminology and performance specifications crucial for the success of space missions.

Key Features of the Standard

• Standard Number: BS EN 16603-60-20:2020
• Pages: 92
• ISBN: 978 0 539 05709 6
• Status: Standard

Comprehensive Coverage

This standard spans 92 pages of in-depth information, meticulously detailing the terminology and performance specifications for star sensors. It is designed to ensure that all stakeholders have a common understanding of the terms and performance criteria, which is vital for the seamless integration and operation of star sensors in space systems.

Why This Standard is Essential

Star sensors are critical components in spacecraft, used for navigation and orientation by detecting and tracking stars. The BS EN 16603-60-20:2020 standard provides a unified framework that helps engineers and scientists to:

• Ensure consistency and reliability in the design and functionality of star sensors.
• Facilitate communication and collaboration across international teams and projects.
• Enhance the accuracy and efficiency of space missions by providing clear performance benchmarks.

Who Can Benefit from This Standard?

This standard is invaluable for a wide range of professionals and organizations, including:

• Space agencies and organizations involved in space exploration and satellite deployment.
• Engineers and designers specializing in spacecraft systems and components.
• Research institutions and universities focusing on space technology and engineering.
• Manufacturers and suppliers of star sensors and related technologies.

Enhancing Space Mission Success

By adhering to the BS EN 16603-60-20:2020 standard, organizations can significantly enhance the success rate of their space missions. The standard provides a robust framework for the development and evaluation of star sensors, ensuring they meet the rigorous demands of space environments. This leads to improved mission outcomes, reduced risk of failure, and optimized performance of spacecraft systems.

Global Recognition and Compliance

As a recognized standard, BS EN 16603-60-20:2020 is widely accepted and implemented across the globe. Compliance with this standard not only demonstrates a commitment to quality and excellence but also facilitates international collaboration and partnerships in the space industry. It serves as a benchmark for best practices, helping organizations to align with global standards and expectations.

Conclusion

The BS EN 16603-60-20:2020 standard is an indispensable tool for anyone involved in the field of space engineering. Its comprehensive coverage of star sensor terminology and performance specifications provides a solid foundation for the development of reliable and efficient space systems. By integrating this standard into your projects, you can ensure that your star sensors meet the highest standards of quality and performance, paving the way for successful space missions.

BS EN 16603-60-20:2020

This standard BS EN 16603-60-20:2020 Space engineering. Star sensor terminology and performance specification is classified in these ICS categories:

• 49.140 Space systems and operations
• 01.040.49 Aircraft and space vehicle engineering (Vocabularies)

This Standard specifies star sensor performances as part of a space project. The Standard covers all aspects of performances, including nomenclature, definitions, and performance requirements for the performance specification of star sensors.

The Standard focuses on:

• performance specifications (including the impact of temperature, radiation and straylight environments);

• robustness (ability to maintain functionalities under non nominal environmental conditions).

Other specification types, for example mass and power, housekeeping data and data structures, are outside the scope of this Standard.

This Standard also proposes a standard core of functional interfaces defined by unit suppliers and avionics primes in the context of Space AVionics Open Interface aRchitecture (SAVOIR) initiative.

When viewed from the perspective of a specific project context, the requirements defined in this Standard should be tailored to match the genuine requirements of a particular profile and circumstances of a project.

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