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ISO/DIS 14622

Space systems — Structural design — Loads and induced environment

General information

40.99     28 gush 2024

ISO

ISO/TC 20/SC 14

International Standard

49.140  

anglisht  

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Draft

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Scope

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.

Life cycle

PREVIOUSLY

Revises
ISO 14622:2000

NOW

IN_DEVELOPMENT
ISO/DIS 14622
40.99 Full report circulated: DIS approved for registration as FDIS
28 gush 2024

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