ISO 14622:2000

This standard was last reviewed and confirmed in 2016. Therefore this version remains current.

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.

	Format	Language
std 1 61	PDF
std 2 61	Paper

This standard contributes to the following Sustainable Development Goal

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