ISO/DIS 14622

Under development

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

Will replace ISO 14622:2000

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

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