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ISO 16679:2015
Space systems — Relative motion analysis elements after LV/SC separation
Automatically translated name:
Space systems -- Relative motion analysis elements after LV/SC separation
STANDARD published on 21.9.2015
The information about the standard:
Designation standards: ISO 16679:2015
Publication date standards: 21.9.2015
SKU: NS-615980
The number of pages: 10
Approximate weight : 30 g (0.07 lbs)
Country: International technical standard
Category: Technical standards ISO
The category - similar standards:
Annotation of standard text ISO 16679:2015 :
Description / Abstract: 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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