ISO 14622:2000

Published (Edition 1, 2000)

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

Expected to be replaced by ISO/FDIS 14622 within the coming months.

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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.

This standard contributes to the following Sustainable Development Goal