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ISO 16679:2015

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ISO 16679:2015

Space systems — Relative motion analysis elements after LV/SC separation

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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.

Author ISO/TC 20/SC 14 Space systems and operations
Editor ISO
Document type Standard
Format Paper
Edition 1
ICS 49.140 : Space systems and operations
Number of pages 10
Weight(kg.) 0.1170
Year 2015
Country Switzerland