Draft International Standard
ISO/DIS 14622
Space systems — Structural design — Loads and induced environment
Reference number
ISO/DIS 14622
Edition 2
© ISO 2024
Draft
International Standard
Read sample
Under development
This Draft International Standard is in the enquiry phase with ISO members.
Will replace ISO 14622:2000

ISO/DIS 14622

Language
Format
CHF 63
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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

    You can help develop this draft international standard by contacting your national member

    Stage
    : DIS ballot initiated: 12 weeks [40.20]
  • Edition
     : 2
    Number of pages
     : 10
  • Technical Committee :
    ISO/TC 20/SC 14
    ICS :
    49.140 
  • RSS updates

Life cycle

Sustainable Development Goals

This standard contributes to the following Sustainable Development Goal

9
Industry, Innovation and Infrastructure

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