International Standard
ISO 27852:2024
Space systems — Estimation of orbit lifetime
Reference number
ISO 27852:2024
Edition 3
2024-02
Read sample
ISO 27852:2024
85364
Published (Edition 3, 2024)

ISO 27852:2024

ISO 27852:2024
85364
Language
Format
CHF 173
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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.

General information

  •  : Published
     : 2024-02
    : International Standard published [60.60]
  •  : 3
     : 48
  • ISO/TC 20/SC 14
    49.140 
  • RSS updates

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