ISO 14622:2000

Space systems — Structural design — Loads and induced environment

OVERVIEW

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.

COMMENTS

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PRODUCT DETAILS

Status Withdrawn - 06 Jan 2026
Edition 2000
No. of Pages 9
ICS Classification 49.140 Space systems and operations
Committee ISO/TC 20/SC 14
Available for Purchase For sale in Singapore only
Adoption ISO