This standard was last reviewed and confirmed in 2016.
Therefore this version remains current.
Abstract
PreviewThis 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.
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Status: PublishedPublication date: 2000-12
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Edition: 1Number of pages: 9
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- ICS :
- 49.140 Space systems and operations
Buy this standard
en
| Format | Language | |
|---|---|---|
| std 1 61 | ||
| std 2 61 | Paper |
- CHF61
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