This standard was last reviewed and confirmed in 2016. Therefore this version remains current.
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.
Status: PublishedPublication date: 2000-12
Edition: 1Number of pages: 9
Technical Committee: ISO/TC 20/SC 14 Space systems and operations
- ICS :
- 49.140 Space systems and operations
This standard contributes to the following Sustainable Development Goal:
Buy this standard
|std 1 61|
|std 2 61||Paper|
A standard is reviewed every 5 years
Stage: 90.92 (To be revised)
Will be replaced byUnder development
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