Norm

ISO 27852:2016 en

Space systems - Estimation of orbit lifetime

131,28

Over deze norm

Status Definitief
Aantal pagina's 43
Commissie Lucht- en ruimtevaart
Gepubliceerd op 01-07-2016
Taal Engels
ISO 27852 describes a process for the estimation of orbit lifetime for spacecraft, launch vehicles, upper stages and associated debris in LEO-crossing orbits. This International Standard also clarifies the following: a) modelling approaches and resources for solar and geomagnetic activity modelling; b) resources for atmosphere model selection; c) approaches for spacecraft ballistic coefficient estimation.

Details

ICS-code 49.140
Nederlandse titel Space systems - Estimation of orbit lifetime
Engelse titel Space systems - Estimation of orbit lifetime
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