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

Under development

This draft is in the approval phase.

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

Stage
: Final text received or FDIS registered for formal approval [50.00]
Edition
: 2
Technical Committee :
ISO/TC 20/SC 14

ICS :
49.140
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Life cycle

This standard contributes to the following Sustainable Development Goal

Industry, Innovation and Infrastructure

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