ISO 16679:2015
Current
The latest, up-to-date edition.
Space systems Relative motion analysis elements after LV/SC separation
Hardcopy , PDF , PDF 3 Users , PDF 5 Users , PDF 9 Users
English
21-09-2015
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ISO 16679:2015 provides relative motion analysis elements after LV/SC separation, including analysis input, analysis principle, analysis method and analysis output. It is applicable to the mission design and verification for the prediction of relative motion after LV/SC separation.
This International Standard focuses on the relative motion between the objects involved in one launch mission. It does not cover the issues about the collision avoidance between newly launched objects and on-orbit ones.
| DevelopmentNote |
Supersedes ISO/DIS 16679. (09/2015)
|
| DocumentType |
Standard
|
| Pages |
10
|
| PublisherName |
International Organization for Standardization
|
| Status |
Current
|
| Standards | Relationship |
| BS ISO 16679:2015 | Identical |
| ISO 14303:2002 | Space systems — Launch-vehicle-to-spacecraft interfaces |
| ISO 10784-1:2011 | Space systems Early operations Part 1: Spacecraft initialization and commissioning |
| ISO 10784-3:2011 | Space systems Early operations Part 3: Commissioning report |
| ISO 10784-2:2011 | Space systems Early operations Part 2: Initialization plan |
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