ISO 24411-2022 PDF

St ISO 24411-2022

Name in English:
St ISO 24411-2022

Name in Russian:
Ст ISO 24411-2022

Description in English:

Original standard ISO 24411-2022 in PDF full version. Additional info + preview on request

Description in Russian:
Оригинальный стандарт ISO 24411-2022 в PDF полная версия. Дополнительная инфо + превью по запросу
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Full title and description

ISO 24411:2022 — Space systems — Micro-vibration testing. This International Standard specifies requirements and guidance for the planning and execution of spacecraft-level micro‑vibration tests intended to characterise the micro‑vibration environment produced by internal disturbance sources and its effect on sensitive payloads (earth observation instruments, space telescopes, optical experiments, telecommunications payloads, etc.).

Abstract

This document sets out requirements for implementation of spacecraft‑level micro‑vibration tests for use by test providers (test designers, test engineers) and provides guidance for spacecraft designers and other interested parties. It covers applicability to space systems containing payload equipment sensitive to micro‑vibrations induced by internal on‑orbit disturbance sources.

General information

  • Status: Published.
  • Publication date: 10 October 2022 (ISO edition published October 2022).
  • Publisher: International Organization for Standardization (ISO).
  • ICS / categories: 49.140 (Space systems and operations).
  • Edition / version: Edition 1 (2022).
  • Number of pages: 22 pages (English original PDF/ePub and paper formats available from ISO).

Key bibliographic and lifecycle information as published by ISO.

Scope

ISO 24411:2022 applies to spacecraft‑level micro‑vibration testing intended to characterise the micro‑vibration environment caused by internal disturbance sources on‑orbit and to measure the resulting responses of the spacecraft and payloads. The standard provides a framework for tailoring tests, identifying disturbance sources, performing preliminary analysis, selecting and configuring test equipment (boundary simulation, excitation, sensors, data acquisition), and executing transfer‑function, modal survey and response measurements. It also addresses laboratory environment and background noise requirements, pre‑conditions, safety and recommended test flow and reporting. The objective is to support reproducible, project‑appropriate micro‑vibration verification for payloads sensitive to very low‑level dynamic excitation.

Key topics and requirements

  • Definition of spacecraft‑level micro‑vibration test purpose and tailoring to mission/payload needs.
  • Identification and characterisation of internal disturbance sources (reaction wheels, cryocoolers, mechanisms, etc.).
  • Preliminary analyses and model‑to‑test correlation requirements (transfer functions and modal surveys).
  • Test equipment requirements and recommended configurations for boundary simulation, excitation systems and measurement chains.
  • Requirements for transfer‑function measurement, modal survey tests and micro‑vibration response measurements.
  • Laboratory environment, background noise limits and conditioning required to obtain valid micro‑vibration data.
  • Data acquisition, processing and reporting conventions; guidance on acceptance criteria and safety precautions.
  • Recommended test flow and sequence (pre‑conditions, configuration control, instrumentation, runs and post‑test verification).

Typical use and users

Primary users are test providers (test houses and laboratories), spacecraft and payload test engineers, systems and payload designers, integrators and verifiers at space agencies and industry contractors. Use cases include qualification and verification of satellite platforms and payloads where on‑orbit micro‑vibration susceptibility could degrade mission performance (high‑resolution imagers, optical instruments, precision pointing payloads, interferometers and sensitive scientific instruments). Research organisations and test facility managers also use the standard to establish consistent micro‑vibration test methods and reporting.

Related standards

ISO 24411 is intended to complement ISO system test guidance such as ISO 15864 (Space systems — General test methods for spacecraft, subsystems and units) and ISO 17566 (Space systems — General test documentation), which address broader test methods and test documentation formats used for space programmes.

Users should also consider applicable ECSS (European Cooperation for Space Standardization) and national standards for environmental and vibration testing (for example ECSS‑E‑ST‑10‑03 series for mechanical and vibration testing and associated ECSS guidance on micro‑vibration).

Keywords

micro‑vibration; microvibration testing; spacecraft testing; transfer function; modal survey; payload susceptibility; reaction wheel disturbances; boundary simulation; data acquisition; ISO/TC 20/SC 14.

FAQ

Q: What is this standard?

A: ISO 24411:2022 is an ISO International Standard titled "Space systems — Micro‑vibration testing" that defines requirements and guidance for spacecraft‑level micro‑vibration tests.

Q: What does it cover?

A: It covers the purpose and tailoring of micro‑vibration tests, identification of disturbance sources, preliminary analysis, test equipment and configurations (boundary simulation, excitation and measurement), transfer‑function and modal survey methods, response measurement, laboratory background noise and environmental requirements, safety, and recommended test flow and documentation.

Q: Who typically uses it?

A: Test providers (laboratories and test engineers), spacecraft and payload designers, system integrators, space agencies, and research facilities that perform or specify spacecraft‑level micro‑vibration testing.

Q: Is it current or superseded?

A: ISO 24411:2022 is a current published International Standard (first edition, published October 2022). Users should check ISO or their national standards body for any amendments, confirmations or future revisions.

Q: Is it part of a series?

A: It sits within the ISO space‑systems test/documentation family managed by ISO/TC 20/SC 14 and is complementary to other ISO space testing standards (for example ISO 15864 and ISO 17566) and to ECSS mechanical/vibration test standards and guidance.

Q: What are the key keywords?

A: Micro‑vibration, microvibration testing, spacecraft testing, modal survey, transfer function, payload susceptibility, boundary simulation, data acquisition, ISO 24411.