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ISO 27852:2024

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Note: This standard has a new edition: ISO 27852:2024

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Abstract

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 information

  • Standard from ISO
  • Published:
  • Expires:
  • Edition: 3
  • Version: 1
  • Document type: IS
  • ICS 49.140
  • ISO TC ISO/TC 20/SC 14

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