ISO 16679:2015

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

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.

Edition	2015
Published Date	2015
Published By	International Standardization Organisation
Page Count	10