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Normas BSI – AENOR
20/30386448 DC

20/30386448 DC

BS ISO 23670. Space systems. Vibration testing

Fecha:
2020-08-13 /Definitive
Comité:
ACE/68
Equivalencias internacionales:

ISO/DIS 23670

Resumen:

The primary goals of vibration testing are to qualify the design and to detect manufacturing issues of spacecraft, subsystems and units that could result in in-flight failures. This document provides guidance for test providers and interested parties to implement vibration testing.

During vibration test, over-testing can result in unnecessary destruction of the test specimen. Limitation of acceleration input to the test specimen can prevent this. This document provides guidance including 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.

Keywords:
Electrical testing, Spacecraft, Quality assurance systems, Design, Space technology, Electromagnetic compatibility, Mechanical testing, Performance, Space vehicles
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