ISO 14954:2005
Current
The latest, up-to-date edition.
Space systems — Dynamic and static analysis — Exchange of mathematical models
Hardcopy , PDF , PDF 3 Users , PDF 5 Users , PDF 9 Users
English, French
26-01-2005
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ISO 14954:2005 normalizes the exchange of mathematical models between spacecraft contractors (SCC) and launch service providers (LSP). It identifies standard methods for modelling the dynamic behaviour of both launch vehicles (LV) and spacecraft (SC) particularly when they are coupled prior to launch and during the early moments of the launch phase.
In standard mode, the delivered models represent dynamic and static behaviour at the launcher interface. The requirements provided in ISO 14954:2005 are the minimum necessary for dynamic coupled analysis. They may be not sufficient for stress analysis.
ISO 14954:2005 does not include the validation of spacecraft models.
| DevelopmentNote |
Supersedes ISO/DIS 14954 (01/2005)
|
| DocumentType |
Standard
|
| Pages |
13
|
| ProductNote |
THIS STANDARD ALSO REFERS TO ISO/CEI 646
|
| PublisherName |
International Organization for Standardization
|
| Status |
Current
|
| Standards | Relationship |
| BS ISO 14954:2005 | Identical |
| ISO 10786:2011 | Space systems — Structural components and assemblies |
| BS ISO 10786:2011 | Space systems. Structural components and assemblies |
| 10/30197714 DC : 0 | BS ISO 10786 - SPACE SYSTEMS - STRUCTURAL COMPONENTS AND ASSEMBLIES |
| ISO/IEC 646:1991 | Information technology ISO 7-bit coded character set for information interchange |
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