ISO 14622 - Space systems — Structural design — Loads and induced environment

Under publication (Edition 2, 2025)

Final production steps (up to seven weeks).

Will replace ISO 14622:2000

Abstract

This International Standard defines the principles used to determine loads and the induced environment during the

service life of a space flight vehicle and its components, taking account of the notions of probability, combined

loads, corresponding safety factors and lifecycle.

General information

Status
: Under development

Publication date
: 2025-04

Stage
: International Standard under publication [60.00]
Edition
: 2
Technical Committee :
ISO/TC 20/SC 14

ICS :
49.140
RSS updates

Life cycle

This standard contributes to the following Sustainable Development Goal

Industry, Innovation and Infrastructure

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