Draft
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.
Revises
ISO 14622:2000
IN_DEVELOPMENT
ISO/DIS 14622
40.99
Full report circulated: DIS approved for registration as FDIS
Aug 28, 2024
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