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

Under development

This Draft International Standard is in the enquiry phase with ISO members.

Will replace ISO 14622:2000

ISO/DIS 14622

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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
: Full report circulated: DIS approved for registration as FDIS [40.99]
Edition
: 2

Number of pages
: 10
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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