ISO 27852:2024

Published (Edition 3, 2024)

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.

General information

Status
: Published

Publication date
: 2024-02

Stage
: International Standard published [60.60]
Edition
: 3

Number of pages
: 48
Technical Committee :
ISO/TC 20/SC 14

ICS :
49.140
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