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Full Description

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.
 

Document History

  1. ISO 27852:2024

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    Space systems - Estimation of orbit lifetime

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  2. ISO 27852:2016


    Space systems - Estimation of orbit lifetime

    • Historical Version
  3. ISO 27852:2011


    Space systems - Estimation of orbit lifetime

    • Historical Version