Norm

ISO 16679:2015 en

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

48,19

Over deze norm

Status Definitief
Aantal pagina's 10
Commissie Lucht- en ruimtevaart
Gepubliceerd op 01-09-2015
Taal Engels
ISO 16679 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.

Details

ICS-code 49.140
Nederlandse titel Space systems - Relative motion analysis elements after LV/SC separation
Engelse titel Space systems - Relative motion analysis elements after LV/SC separation
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