BS 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.Cross References:ISO 14303ISO 10784-1ISO 10784-2ISO 10784-3All current amendments available at time of purchase are included with the purchase of this document.