ISO 27852:2024

OVERVIEW

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.

COMMENTS

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