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.
General information
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Status: PublishedPublication date: 2000-12Stage: International Standard to be revised [90.92]
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Edition: 1Number of pages: 9
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Technical Committee :ISO/TC 20/SC 14ICS :49.140
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Draft
International StandardISO/DIS 14622
Space systems — Structural design — Loads and induced environment
Reference number
ISO/DIS 14622
ISO/DIS 14622
Edition 1
© ISO 2024
Draft International Standard
ISO/DIS 14622
Space systems — Structural design — Loads and induced environment
Life cycle
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Now
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Will be replaced by
Under developmentISO/DIS 14622
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