ISO 14622:2000
Withdrawn
View Superseded by
Space systems — Structural design — Loads and induced environment
Hardcopy , PDF
English, French
12-21-2000
11-02-2025
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.
| Committee |
ISO/TC 20/SC 14
|
| DocumentType |
Standard
|
| Pages |
9
|
| PublisherName |
International Organization for Standardization
|
| Status |
Withdrawn
|
| SupersededBy | |
| UnderRevision |
| Standards | Relationship |
| IS 19271 : 2025 | Identical |
| NBR ISO 14622 : 2008 | Identical |
| ISO 10786:2011 | Space systems — Structural components and assemblies |
| ISO 16454:2007 | Space systems — Structural design — Stress analysis requirements |
| BS ISO 10786:2011 | Space systems. Structural components and assemblies |
| 10/30197714 DC : 0 | BS ISO 10786 - SPACE SYSTEMS - STRUCTURAL COMPONENTS AND ASSEMBLIES |
| BS ISO 16454:2007 | Space systems. Structural design. Stress analysis requirements |
| 05/30099159 DC : DRAFT FEB 2005 | ISO 16454 - SPACE SYSTEMS - STRUCTURAL DESIGN - STRESS ANALYSIS REQUIREMENTS |
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