Standard

ISO 27852:2024

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Merknad: Denne standarden har en ny utgave: ISO 27852:2024

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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.

Dokumentinformasjon

  • Standard fra ISO
  • Publisert:
  • products.specs.Expires:
  • Utgave: 3
  • Versjon: 1
  • Varetype: IS
  • ICS 49.140
  • ISO TC ISO/TC 20/SC 14

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