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ISO 27852:2024

Space systems - Estimation of orbit lifetime


This document describes a process for the long-duration orbit lifetime prediction of orbit lifetime for spacecraft, launch vehicles, upper stages and associated debris in LEO-crossing orbits after mission phase (including any mission lifetime extensions).

 

The document also clarifies:

 

a)       modelling approaches and resources for solar and geomagnetic activity modelling;

 

b)       resources for atmosphere model selection;

 

c)        approaches for spacecraft ballistic coefficient estimation.


CONTENT PROVIDER
International Organization for Standardization [iso]

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