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immediate downloadReleased: 2021-09-15
BS ISO 23670:2021 Space systems. Vibration testing

BS ISO 23670:2021

Space systems. Vibration testing

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Standard number:BS ISO 23670:2021
Pages:36
Released:2021-09-15
ISBN:978 0 539 02911 6
Status:Standard
BS ISO 23670:2021 Space systems. Vibration testing

BS ISO 23670:2021 Space Systems. Vibration Testing

Standard Number: BS ISO 23670:2021

Pages: 36

Released: 2021-09-15

ISBN: 978 0 539 02911 6

Name: Space systems. Vibration testing

Status: Standard

Overview

The BS ISO 23670:2021 standard is an essential document for professionals in the aerospace industry, particularly those involved in the design, testing, and validation of space systems. This comprehensive standard provides detailed guidelines and methodologies for vibration testing, ensuring that space systems can withstand the harsh conditions of launch and operation in space.

Why Choose BS ISO 23670:2021?

Space systems are subjected to extreme conditions, including intense vibrations during launch and operation. The BS ISO 23670:2021 standard is designed to help engineers and scientists ensure the reliability and durability of these systems. By adhering to this standard, you can:

  • Ensure the structural integrity of space systems under vibrational stress.
  • Enhance the reliability and performance of space missions.
  • Comply with international best practices and regulatory requirements.
  • Minimize the risk of mission failure due to vibrational damage.

Key Features

The BS ISO 23670:2021 standard includes a range of features designed to provide comprehensive guidance on vibration testing for space systems:

  • Detailed Methodologies: Step-by-step procedures for conducting vibration tests, including pre-test preparations, test execution, and post-test analysis.
  • Test Equipment Specifications: Guidelines on the selection and calibration of vibration testing equipment to ensure accurate and reliable results.
  • Data Analysis Techniques: Methods for analyzing test data to assess the performance and durability of space systems under vibrational stress.
  • Compliance and Certification: Information on how to achieve compliance with international standards and obtain certification for your space systems.

Who Should Use This Standard?

The BS ISO 23670:2021 standard is ideal for a wide range of professionals in the aerospace industry, including:

  • Aerospace Engineers
  • Test Engineers
  • Quality Assurance Specialists
  • Project Managers
  • Regulatory Compliance Officers

Benefits of Using BS ISO 23670:2021

By implementing the guidelines and methodologies outlined in the BS ISO 23670:2021 standard, you can achieve several key benefits:

  • Enhanced Reliability: Ensure that your space systems can withstand the vibrational stresses of launch and operation, reducing the risk of mission failure.
  • Improved Performance: Optimize the performance of your space systems by identifying and addressing potential vibrational issues during the testing phase.
  • Regulatory Compliance: Meet international standards and regulatory requirements, facilitating the certification and approval of your space systems.
  • Cost Savings: Minimize the risk of costly mission failures and rework by identifying and addressing vibrational issues early in the development process.

Conclusion

The BS ISO 23670:2021 standard is an invaluable resource for anyone involved in the design, testing, and validation of space systems. By following the comprehensive guidelines and methodologies outlined in this standard, you can ensure the reliability, performance, and compliance of your space systems, ultimately contributing to the success of your space missions.

DESCRIPTION

BS ISO 23670:2021


This standard BS ISO 23670:2021 Space systems. Vibration testing is classified in these ICS categories:
  • 17.160 Vibrations, shock and vibration measurements
  • 49.140 Space systems and operations

This document provides guidance and requirements for test providers and interested parties to implement vibration testing.

This document specifies methods, including the force limiting approach, to mitigate unnecessary over-testing of spacecraft, subsystems and units for space application.

The technical requirements in this document can be tailored to meet the actual test objectives.