Status : Published (To be revised)

This standard was last reviewed and confirmed in 2016. Therefore this version remains current.
This standard will be replaced by 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.

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General information

  • Status
     : Published
    Publication date
     : 2000-12
    Stage
    : International Standard to be revised [90.92]
  • Edition
     : 1
    Number of pages
     : 9
  • Technical Committee :
    ISO/TC 20/SC 14
    ICS :
    49.140 
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Life cycle

Sustainable Development Goals

This standard contributes to the following Sustainable Development Goal

9
Industry, Innovation and Infrastructure

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