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ISO 16679:2015

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

General information
Valid from 21.09.2015
Directives or regulations
None
Standard history
Status
Date
Type
Name
21.09.2015
Main
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.
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