Summary
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.
Notes
40.20 : Mise au vote du DIS: 12 semaines
Technical characteristics
| Publisher | International Organization for Standardization (ISO) |
| Publication Date | 04/14/2025 |
| Edition | 2 |
| Page Count | 10 |
| EAN | --- |
| ISBN | --- |
| Weight (in grams) | --- |
Replaces
21/12/2000
Superseded
, Confirmed
, Has Draft
Historical
Previous versions
21/12/2000
Superseded
, Confirmed
, Has Draft
Historical